560:
had its first stage damaged in another accident. On 5 February, LC-16 returned to action by hosting
Missile C-4. The second attempt at a Lot C Titan failed at T+52 seconds when the guidance compartment collapsed, causing the RVX-3 reentry vehicle to separate. The missile pitched down and the first stage LOX tank ruptured from aerodynamic loads, blowing the stage to pieces. After the first stage destroyed itself, the second stage separated and began engine ignition, sensing that normal staging had taken place. With no attitude control, it began tumbling end-over-end and quickly lost thrust. The stage plummeted into the Atlantic Ocean some 30–40 miles downrange After the successful flight of Missile G-4 on 24 February, Missile C-1's second stage failed to ignite on 8 March due to a stuck valve preventing the gas generator from starting.The last Lot C missile was C-6 which flew successfully on April 28. The Lot G missiles incorporated several design improvements to correct problems encountered on previous Titan launches. On 1 July, the newly opened LC-20 hosted its first launch when Missile J-2, an operational prototype, was flown. Unfortunately, a broken hydraulic line caused the Titan's engines to gimbal hard left almost as soon as the tower was cleared. The missile pitched over and flew onto a near-horizontal plane when Range Safety sent the destruct command at T+11 seconds. The burning remains of the Titan impacted 300 meters from the pad in an enormous fireball. The piece of plumbing responsible for the missile failure was retrieved—it had popped out of its sleeve resulting in loss of first stage hydraulic pressure. The sleeve was not tight enough to hold the hydraulic line in place, and the pressure being imparted into it at liftoff was enough to pop it loose. Examination of other Titan missiles found more defective hydraulic lines, and the Missile J-2 debacle caused a wholesale review of manufacturing processes and improved parts testing.
656:-minute intervals. Titan I utilized radio-inertial command guidance. The inertial guidance system originally intended for the missile was instead eventually deployed in the Atlas E and F missiles. Less than a year later the Air Force considered deploying the Titan I with an all-inertial guidance system but that change never occurred. (The Atlas series was intended to be the first generation of American ICBMs and Titan II (as opposed to Titan I) was to be the second generation deployed). The Titan 1 was controlled by an autopilot which was informed of the missile's attitude by a rate gyro assembly consisting of 3 gyroscopes. During the first minute or two of the flight a pitch programmer put the missile on the correct path. From that point the AN/GRW-5 guidance radar tracked a transmitter on the missile. The guidance radar fed missile position data to the AN/GSK-1 (Univac Athena) missile guidance computer in the Launch Control Center. The guidance computer used the tracking data to generate instructions which were encoded and transmitted to the missile by the guidance radar. Guidance input/output between the guidance radar and guidance computer occurred 10 times a second. Guidance commands continued for the stage 1 burn, the stage 2 burn and the vernier burn ensuring the missile was on the correct trajectory and terminating the vernier burn at the desired velocity. The last thing the guidance system did was to determine if the missile was on the right trajectory and pre-arm the warhead which then separated from the second stage. In case of the failure of the guidance system at one site, the guidance system at another site could be used to guide the missiles of the site with the failure.
918:
January 1962. There were 59 XSM-68 Titan Is manufactured I in 7 developmental lots. One hundred and one SM-68 Titan I missiles were produced to equip six squadrons of nine missiles each across
Western America. Fifty-four missiles were in silos in total, with one missile as a spare on standby at each squadron, bringing to 60 in service at any one time. Titan was originally planned for a 1 X 10 (one control center with 10 launchers) "soft" site. In mid-1958 it was decided that the American Bosh Arma all-inertial guidance system designed for Titan would, because production was insufficient, be assigned to Atlas and the Titan would switch to radio-inertial guidance. The decision was made to deploy Titan squadrons in a "hardened" 3 X 3 (three sites with one control center and three silos each) to reduce the number of guidance systems required. (Radio-inertial guided Atlas D squadrons were similarly sited).
660:
part, was selected as the contractor because it had "recognized the 'magnitude of the altitude start problem' for the second stage and had a good suggestion for solving it." Titan I's second-stage engines were reliable enough to be ignited at altitude, after separation from the first stage booster. The first stage, besides including heavy fuel tanks and engines, also had launch interface equipment and the launch pad thrust ring with it. When the first stage had finished consuming its propellant, it dropped away, thereby decreasing the mass of the vehicle. Titan I's ability to jettison this mass prior to the ignition of the second stage meant that Titan I had a much greater total range (and a greater range per pound of second-stage fuel) than Atlas, even if the total fuel load of Atlas had been greater. As North
American Aviation's
572:
1204:
raising the launcher and missile out of the silo on an elevator. Before each launch, the guidance radar, which was periodically calibrated by acquiring a special target at a precisely known range and bearing, had to acquire a radio on the missile (missile guidance set AN/DRW-18, AN/DRW-19, AN/DRW-20, AN/DRW-21, or AN/DRW-22). When the missile was launched, the guidance radar tracked the missile and supplied precise velocity range and azimuth data to the guidance computer, which then generated guidance corrections that were transmitted to the missile. Because of this, the complex could only launch and track one missile at a time, although another could be elevated while the first was being guided.
591:
first stage burn, but after second stage separation, the fuel valve to the gas generator failed to open, preventing engine start. Missiles AJ-12 and AJ-15 in March were lost due to turbopump problems. Missile M-1's second stage lost thrust when the hydraulic pump failed. Missile SM-2 experienced early first stage shutdown; although the second stage burn was successful, it had to run to propellant depletion instead of a timed cutoff. The added stress of this operation apparently resulted in a failure of either the gas generator or turbopump, as the vernier solo phase ended prematurely. Missile M-6's second stage failed to start when an electrical relay malfunctioned and reset the ignition timer.
1433:
1255:
Air Force wanted to retain 5 Titan sites and the
General Services Administration had earmarked 1 for possible use. The USAF removed equipment it had uses for, the rest was offered to other government agencies. Eventually no sites were retained and all were salvaged. The chosen method was the Service and Salvage contract, which required the contractor to remove the equipment the government wanted before proceeding with scrapping. This accounts for the varied degree of salvage at the sites today. Most are sealed today, with one in Colorado that is easily entered but also very unsafe. One is open for tours.
1200:
crucial to avoid possible destruction by incoming missiles. Even though Titan complexes were designed to withstand nearby nuclear blasts antenna and missile extended for launch and guidance were quite susceptible to even a relatively distant miss. The missiles sites of a squadron were placed at least 17 (usually 20 to 30) miles apart so that a single nuclear weapon could not take out two sites. The sites also had to be close enough that if a site's guidance system failed it could "handover" its missiles to another site of the squadron.
1273:(AKA "Star Wars" program), a scrapped Titan I Second Stage was used in a Missile Defense test. The MIRACL Near Infrared Laser, at White Sands Missile Range, NM was fired at a stationary Titan I second stage that was fixed to the ground. The second stage burst and was destroyed by the laser blast. The second stage was pressurized with nitrogen gas to 60-psi and did not contain any fuel or oxidizer. A follow-up test 6 days later was conducted on a scrapped Thor IRBM, its remnants reside at the SLC-10 Museum at Vandenberg AFB.
3037:
968:
471:
the
Western Development Division and Brigadier General Bernard Schriever was detailed to command it. Schriever devised an entirely new organization for program management. The Air Force was to act as "prime contractor," the Ramo-Woolridge Corporation was contracted to provide systems engineering and technical direction of all ballistic missiles. The airframe contractor also would assemble the sub-systems provided by other Air Force contractors. At the time, this new organization was very controversial.
1304:
1292:
1280:
496:
Despite counterarguments that the Titan offered greater performance and growth potential than the Atlas as a missile and space launch vehicle, the Titan program was under constant budgetary pressure. In the summer of 1957 budget cuts led
Secretary of Defense Wilson to reduce the Titan production rate from the proposed seven per month to two a month, which left the Titan as a research and development program only. However, the
1251:. It did not make economic sense to refurbish them as SM-65 Atlas missiles with similar payload capacities had already been converted to satellite launchers. About 33 were distributed to museums, parks and schools as static displays (see list below). The remaining 50 missiles were scrapped at Mira Loma AFS near San Bernardino, CA; the last was broken up in 1972, in accordance with the SALT-I Treaty of 1 February 1972.
1320:
1481:
1196:
there was a site commander, site maintenance officer, site chief, job controller/expediter, tool crib operator, power house chief, three pad chiefs, three assistant pad chiefs, another cook and more air police. There could be a number of electricians, plumbers, power production technicians, air conditioning technicians, and other specialist when maintenance was being performed.
38:
587:. The plan was to load the missile with propellant, raise it up to firing position, and then lower it back into the silo. Unfortunately, the silo elevator collapsed, causing the Titan to fall back down and explode. The blast was so violent that it ejected a service tower from inside the silo and launched it some distance into the air before coming back down.
544:
feet before the engines shut down and it fell back onto LC-19 in a fiery explosion. Postflight investigation found that the hold-down bolts released prematurely, causing B-5 to lift before full thrust rise had been achieved. A still-attached umbilical sent a shutdown command to the engines. LC-19 was badly damaged and would not be used again for six months.
1045:
1031:
1017:
1003:
989:
975:
607:. The launch pads at Cape Canaveral were quickly converted for the new vehicle. Vandenberg Launch Complex 395 continued to provide for operational test launches. The last Titan I launch was from LC 395A silo A-2 in March 1965. After a brief period as an operational ICBM, it was retired from service in 1965 when Defense Secretary
556:
relay into a vibration-prone area during repair work on the missile and testing confirmed that the shock from the pad hold-down bolts firing was enough to set off the relay. The pad was not as badly damaged as LC-19 had been from the B-5 mishap as C-3 had not actually lifted and it was repaired in only two months.
1254:
By
November 1965 the Air Force Logistics Command had determined that the cost of modifying the widely dispersed sites to support other ballistic missiles was prohibitive, and attempts were made to find new uses. By Spring 1966 a number of possible uses and users had been identified. By 6 May 1966 the
1199:
These early complexes while safe from a nearby nuclear detonation, however, had certain drawbacks. First, the missiles took about 15 minutes to fuel, and then, one at a time, had to be lifted to the surface on elevators for launching and guidance, which slowed their reaction time. Rapid launching was
1191:
guidance radar antennas, and three launchers each composed of: three equipment terminals, three propellant terminals, and three missile silos. All connected by an extensive network of tunnels. Both antenna terminals and all three launchers were isolated with double door blast locks the doors of which
838:
toward the target. On-board Titan attitude control rolled the missile to maintain the missile antenna aligned to the ground antenna. Computer commands were transmitted to the missile from a ground transmitter a "quarter mile out" (400 m). Completed in 1957, the Athena weighed 21,000 pounds (11
833:
missile guidance system. The Athena was the "first transistorized digital computer to be produced in numbers." It consisted of ten cabinets plus console on a 13.5 by 20 foot (4.1 by 6 m) floor plan. It used radar tracking of the missile to compute Titan flight data to the necessary burn-out point to
641:
had to be loaded onto the missile just before launch from an underground storage tank, and the missile raised above ground on the enormous elevator system, exposing the missile for some time before launch. The complexity of the system combined with its relatively slow reaction time – fifteen minutes
539:
The four A-type missile launches with dummy second stages all occurred in 1959 and were carried out on 6 February, 25 February, 3 April, and 4 May. The guidance system and stage separation all performed well, and aerodynamic drag was lower than anticipated. Titan I was the first program to have a new
433:
The reduction in the mass of nuclear warheads allowed full coverage of the entire Sino-Soviet land mass, and the missile control capabilities were also upgraded. The Titan I would be fully independent in controlled flight from launch to the ballistic release of the warhead, which would descend to its
1186:
Weapon System 107A-2 was a weapon system. It encompassed all of the equipment and even the bases for the Titan I strategic missile. The Titan I was first
American ICBM designed to be based in underground silos, and it gave USAF managers, contractors and missile crews valuable experience building and
598:
Twelve more Titan Is were flown in 1963–65, with the finale being
Missile SM-33, flown on 5 March 1965. The only total failure in this last stretch of flights was when Missile V-4 (1 May 1963) suffered a stuck gas generator valve and loss of engine thrust at liftoff. The Titan fell over and exploded
559:
On 2 February 1960, LC-19 returned to action as
Missile B-7A marked the first successful flight of a Titan with a live upper stage--this was a composite missile as B-7's original upper stage was damaged months earlier in an accident and it was replaced with the upper stage from Missile B-6 which had
555:
At 1:11 PM EST on December 12, Missile C-3 launched from LC-16. The engines started, but the missile almost immediately disappeared in a fireball. The mishap was quickly traced to the Range Safety destruct charges on the first stage inadvertently going off. Martin technicians had moved the activator
551:
sent Martin an angry letter calling their handling of the Titan program "inexcusable." Ritland's disciplinary blast had little effect for the time being. On December 10, the first attempt was made to launch a Lot C missile, which would be a complete Titan I with all systems and a detachable warhead.
1195:
The launch crew was composed of a missile combat crew commander, missile launch officer (MLO), guidance electronics officer (GEO), ballistic missile analyst technician (BMAT), and two electrical power production technicians (EPPT). There were also a cook and two Air Police. During normal duty hours
928:
oxidizer had to be pumped aboard the missile just before launch, and complex equipment was required to store and move this liquid. In its brief career, a total of six USAF squadrons were equipped with the Titan I missile. Each squadron was deployed in a 3x3 configuration, which meant each squadron
543:
Missile B-5 was intended to launch from LC-19 as the first flight article Lot B missile, incorporating most Titan I missile systems but with a dummy warhead. A planned launch on July 31 was scrubbed due to fuel system problems. At about noon on August 5, B-5 was launched. The missile rose about ten
478:
oxidizer could not be stored for long periods of time, increasing the response time as the missile had to be raised out of its silo and loaded with oxidizer before a launch could occur. The main improvements of the Titan I over the first Atlas's deployed were vertical storage in a fully underground
611:
made the decision to phase out all first generation cryogenically fueled missiles in favor of newer hypergolic and solid-fueled models. While decommissioned Atlas (and later Titan II) missiles were recycled and utilized for space launches, the Titan I inventory were stored and eventually scrapped.
552:
Missile C-3 was prepared for launch but much like with B-5, a premature shutdown command was sent due to failure of an umbilical to detach, fortunately the missile had not been released from the pad. The umbilical was quickly repaired but any relief at having avoided near-disaster was short-lived.
495:
The Titan, proposed as a fallback in case the Atlas failed, was by December 1956 accepted by some as a "principal ingredient of the national ballistic missile force." At the same time, others pushed for the cancellation of the Titan program almost from the beginning, arguing that it was redundant.
470:
missiles had slipped an average of 5 years and had cost overruns of 300 per cent or more. In response, the Teapot Committee was tasked with evaluating requirements for ballistic missiles and methods of accelerating their development. As a result of the ensuing recommendations, the USAF established
659:
Titan I also was the first true multi-stage (two or more stages) design. The Atlas missile had all three of its main rocket engines ignited at launch (two were jettisoned during flight) due to concerns about igniting rocket engines at high altitude and maintaining combustion stability. Martin, in
590:
A total of 21 Titan I launches took place during 1961, with five failures. On 20 January 1961, Missile AJ-10 launched from LC-19 at CCAS. The flight ended in failure when an improper disconnect of a pad umbilical caused an electrical short in the second stage. The Titan performed well through the
567:
The string of failures during 1959–60 led to complaints from the Air Force that Martin–Marietta weren't taking the Titan project seriously (since it was just a backup to the primary Atlas ICBM program) and displayed an indifferent, careless attitude that resulted in easily avoidable failure modes
594:
With attention shifting to the Titan II, there were only six Titan I flights during 1962, with one failure, when Missile SM-4 (21 January) experienced an electrical short in the second stage hydraulic actuator, which gimbaled hard left at T+98 seconds. Staging was performed successfully, but the
917:
The production of operational missiles began during the final stages of the flight test program. An operational specification SM-2 missile was launched from Vandenberg AFB LC-395-A3 on 21 January 1962, with the M7 missile launched on the last development flight from Cape Canaveral's LC-19 on 29
511:
A total of 62 flight test missiles were constructed in various numbers. The first successful launch was on 5 February 1959 with Titan I A3, and the last test flight was on 29 January 1962 with Titan I M7. Of the missiles produced, 49 launched and two exploded: six A-types (four launched), seven
1203:
The distance between the antenna silos and the most distant missile silo was between 1,000 and 1,300 feet (400 m). These were by far the most complex, extensive and expensive missile launch facilities ever deployed by the USAF. Launching a missile required fueling it in its silo, and then
563:
The next launch at the end of the month (Missile J-4) suffered premature first stage shutdown and landed far short of its planned impact point. Cause of the failure was a LOX valve closing prematurely, which resulted in the rupture of a propellant duct and thrust termination. Missile J-6 on 24
540:
missile succeed on the initial attempt, which left launch crews unprepared for the series of failures that followed. Missile B-4 exploded from a LOX pump failure during a static firing at Martin's Denver test stand in May and assorted other mishaps occurred in the following two months.
442:(SM-65/HGM-16) ICBM, serving as a backup with potentially greater capabilities and an incentive for the Atlas contractor to work harder. Martin was selected as the contractor due to its proposed organization and method of igniting a liquid fueled engine at high altitude.
628:
with an effective range of 6,101 nautical miles (11,300 km). The first stage delivered 300,000 pounds (1,330 kN) of thrust, the second stage 80,000 pounds (356 kN). The fact that Titan I, like Atlas, burned Rocket Propellant 1
457:
The previous strategic missile programs of the Air Force had been administered using the "single prime contractor concept" (later called the weapon system concept). This had resulted in three badly botched programs; the programs of the
1690:
Spirres, David 2012, On Alert An Operational History of the United States Air Force Intercontinental Ballistic Missile (ICBM) Program, 1945-2011, Air Force Space Command, United States Air Force, Colorado Springs, Colorado, 2012, p.
434:
target by the combination of gravity and air resistance alone. In May 1955 the Air Materiel Command invited contractors to submit proposals and bids for the two stage Titan I ICBM, formally beginning the program. In September 1955,
421:
By January 1955, the size of nuclear weapons had been shrinking dramatically, allowing the possibility of building a bomb that could be carried by a missile of reasonable size. The Titan I program began on the recommendation of the
3561:
2882:
Spirers, David N., “On Alert An Operational History of the United States Air Force Intercontinental Ballistic Missile (ICBM) Program, 1945-2011,” Air Force Space Command, United States Air Force, Colorado Springs, Colorado,
2599:
On Alert An Operational History of the United States Air Force Intercontinental Ballistic Missile (ICBM) Program, 1945-2011, Spires, David, p 147, Air Force Space Command, United States Air Force, Colorado Springs, Colorado
1187:
working in vast complexes containing everything the missiles and crews needed for operation and survival. The complexes were composed of an entry portal, control center, powerhouse, terminal room, two antenna silos for the
2854:
Lonnquest, John C and Winkler, David F., “To Defend and Deter: the Legacy of the Cold War Missile program,” U.S. Army Construction Engineering Research Laboratories, Champaign, IL Defense Publishing Service, Rock Island,
602:
Although most of the Titan I's teething problems were worked out by 1961, the missile was already eclipsed not only by the Atlas, but by its own design successor, the Titan II, a bigger, more powerful ICBM with storable
512:
B-types (two launched), six C-types (five launched), ten G-types (seven launched), 22 J-types (22 launched), four V-types (four launched), and seven M-types (seven launched). Missiles were tested and launched in
5193:
430:(USAF) their findings of the technical feasibility to develop weapons (bombs) and their delivery systems (intercontinental range ballistic missiles) that were completely invulnerable to "surprise" attack.
397:
missile development ran into problems, the Titan was ultimately beaten into service by Atlas. Deployment went ahead anyway to more rapidly increase the number of missiles on alert and because the Titan's
374:
was operational for only three years, it spawned numerous follow-on models that were a part of the U.S. arsenal and space launch capability. The Titan I was unique among the Titan models in that it used
1192:
could not be open at the same time. This was to ensure that if there was an explosion in a missile launcher or the site was under attack, only the exposed antenna and/or missile silo would be damaged.
1519:
The Titan I was considered for use as the first missile to put a man in space. Two of the firms responding to an Air Force "Request for Proposal" for "Project 7969," an early USAF project to "Put a
2563:
Kaplan, Albert B. and Keyes, Lt. Colonel George W.1962 Lowry Area History 29 September 1958 – December 1961, U.S. Army Corps of Engineers Ballistic Missile Construction Office (CEBMCO), 1962, pg. 4.
2019:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, paragraph 1-159 - 6-1 - 6-4
672:-AJ-3 (booster) and LR91-AJ-3 (sustainer). George P. Sutton wrote "Aerojet's most successful set of large LPRE was that for the booster and sustainer stages of the versions of the Titan vehicle".
2058:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, paragraph 1-159 - 1-161
2010:
Clemmer, Wilbur E..1966, Phase-Out of the Atlas E and F and Titan I Weapon Systems, Wright-Patterson Air Force Base: Historical Research Division Air Force Logistics Command, 1966, p. 22-23.
2669:
Clemmer, Wilbur E..1966, Phase-Out of the Atlas E and F and Titan I Weapon Systems, Wright-Patterson Air Force Base: Historical Research Division Air Force Logistics Command, 1962, p. 49.
2660:
Clemmer, Wilbur E..1966, Phase-Out of the Atlas E and F and Titan I Weapon Systems, Wright-Patterson Air Force Base: Historical Research Division Air Force Logistics Command, 1962, p. 31.
2651:
Clemmer, Wilbur E..1966, Phase-Out of the Atlas E and F and Titan I Weapon Systems, Wright-Patterson Air Force Base: Historical Research Division Air Force Logistics Command, 1962, p. 28.
2411:
Clemmer, Wilbur E..1966, Phase-Out of the Atlas E and F and Titan I Weapon Systems, Wright-Patterson Air Force Base: Historical Research Division Air Force Logistics Command, 1962, p. 25.
3239:
3234:
438:
was declared the contractor for the Titan missile. In early October the Air Force's Western Development Division was ordered to start work. The Titan was developed in parallel with the
2590:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, paragraph 1-159
2101:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, paragraph 1-173
5183:
2322:
United States Air Force The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, paragraph 1-159
2488:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, Pg 7-1 - 7-3
571:
2536:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, page 3-100
2313:
United States Air Force The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, Figure 1-43
1262:
was used as an undergraduate project until 1971, when the former electrical engineering undergraduate students (Athena Systems Development Group) orchestrated its donation to the
2509:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, page 6-1
2554:
Green Warren E., 1962, The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 77.
2479:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, Pg 1-52
2518:
Green Warren E..1962, The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 85.
2470:
United States Air Force, The T.O. 21M-HGM25A-1-1 Technical Manual Operation and Organizational Maintenance HGM-25A Missile Weapon System, United States Air Force, 1964, Pg 1-9
5203:
1878:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 128.
1575:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. vi.
3229:
3224:
3219:
3214:
2420:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 54.
1859:"NASA Technical Reports Server (NTRS) 19730015128: Long life assurance study for manned spacecraft long life hardware. Volume 3: Long life assurance studies of components"
1847:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 96.
1835:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 95.
1815:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 94.
1801:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 93.
1750:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 91.
1721:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 41.
1712:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 37.
1700:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 36.
1672:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 23.
1605:
Green, Warren E.. The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 17.
1596:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 17.
1584:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 11.
1566:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. vi.
1327:
Of the 33 Titan I Strategic Missiles and two (plus five possible) Research and Development Missiles that were not launched, destroyed, or scrapped, several survive today:
165:
161:
157:
152:
1681:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 24
1645:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 4.
1636:
Green, Warren E., The Development of the SM-68 Titan, Wright-Patterson Air Force Base: Air Force Systems Command, 1962, AFSC Historical Publications Series 62-23-1, p. 3.
1303:
1291:
1279:
500:, which started 5 October 1957, ended any talk of canceling Titan. Priority was restored, and 1958 saw increases in funding and plans for additional Titan squadrons.
664:
Division was the only manufacturer of large liquid propellent rocket engines the Air Force Western Development Division decided to develop a second source for them.
642:
to load, followed by the time required to raise and launch the first missile. Following the launch of the first missile the other two could reportedly be fired at
4667:
1542:
1411:
921:
Although Titan I's two stages gave it true intercontinental range and foreshadowed future multistage rockets, its propellants were dangerous and hard to handle.
3257:
564:
October set a record by flying 6100 miles. The J series resulted in minor changes to alleviate the second stage shutting down prematurely or failing to ignite.
1404:. It has been restored to correct external appearance and is now vertically displayed on the grounds. Its upper stage engine was also restored and on display.
1366:
2461:
Simpson, Col. Charlie, LOX and RP-1 – Fire Waiting to Happen, Brekenridge, Colorado: Association of Air Force Missileers, Volume 14, Number 3 2006, p. 1.
2225:
1789:
Cleary, Mark, The 6555th Missile and Space Launches Through 1970, 45th Space Wing History Office, Patrick Air Force Base, Florida, Chapter III Section 6
967:
4712:
1912:
Marsh, Lt. Col.Robert E., Launch of The Blue Gander Door, Brekenridge, Colorado: Association of Air Force Missileers, Volume 4, Number 1 1996, p. 8.
2907:
United States Air Force, “T.O. 21M-HGM25A-1-1, “Technical Manual, Operation and Organizational Maintenance USAF Model HGM-25A Missile Weapon System
4810:
4191:
2995:
2844:
Green, Warren E., “The Development of The SM-68 Titan”, Historical Office Deputy Commander for Aerospace Systems, Air Force Systems Command, 1962
2749:
2348:
2092:
Hoselton, Gary A., Titan I Guidance System, Brekenridge, Colorado: Association of Air Force Missileers, Volume 6, Number 1, March, 1998, p. 6.
2083:
Hoselton, Gary A., Titan I Guidance System, Brekenridge, Colorado: Association of Air Force Missileers, Volume 6, Number 1, March, 1998, p. 5.
2031:
Hoselton, Gary A., Titan I Guidance System, Brekenridge, Colorado: Association of Air Force Missileers, Volume 6, Number 1, March, 1998, p. 4.
4717:
4501:
3552:
3277:
3272:
2863:
2736:
2581:
Hoselton, Gary A., Titan I Guidance System, Brekenridge, Colorado: Association of Air Force Missileers, Volume 6, Number 1, March 1998, p. 5.
2572:
Hoselton, Gary A., Titan I Guidance System, Brekenridge, Colorado: Association of Air Force Missileers, Volume 6, Number 1, March 1998, p. 7.
2072:
1058:
4036:
2876:
2868:
Rosenberg, Max, “The Air Force and The National Guided Missile Program 1944-1949,” USAF Historical Division Liaison Office, Ann Arbor, 1964
474:
The Titan I represented an evolution of technology when compared to the Atlas missile program, but shared many of the Atlas' problems. The
2136:
Sutton, George P, History of Liquid Propellent Rocket Engines, Reston Virginia: American Institute of Aeronautics and Astronautics, 2006,
1943:
1258:
The 26 ATHENA guidance computers, when declared surplus by the federal government, went to various United States universities. The one at
508:
The Titan I flight testing consisted of the first stage only Series I, the cancelled Series II, and Series III with the complete missile.
547:
Further problems occurred over the next several months. Missiles continued to be damaged through careless personnel mistakes and General
4752:
4626:
2946:
1332:
4747:
3293:
2193:
1663:
Sheehan, Neil 2009, A Fiery Peace in a Cold War Bernard Schriever and the Ultimate Weapon, New York: Vintage Books, 2009, pp. 255–257.
1654:
Sheehan, Neil 2009, A Fiery Peace in a Cold War Bernard Schriever and the Ultimate Weapon, New York: Vintage Books, 2009, pp. 233–234.
885:
radars in silos each with "20 foot (6 m) tall antenna" raised prior to launch and locked to the raised Titan's "missileborne antenna".
367:
3267:
2901:
2891:
2614:
2527:
Hoselton, Gary A., Titan I Guidance System, Brekenridge, Colorado: Association of Air Force Missileers, Volume 6, Number 1998, p. 6.
2449:
2141:
2115:
1972:
1931:
1892:
1735:
1472:
1380:
SM-61 60-3706 Gotte Park, Kimball, NE (only first stage standing, damaged by winds in '96?) Vertical (damaged by winds 7/94 ?)
3318:
1903:
See, Earl , Titan Missile Memoirs, Huntington Beach, California: American Aviation Historical Society Journal, Summer 2014, p. 118.
2896:
Sutton, George P., “History of Liquid Propellant Rocket Engines,” American Institute of Aeronautics and Astronautics, Reston, VA,
1858:
1432:
714:
Total production missiles built: 163 Titan 1s; 62 R&D Missiles – 49 launched & 101 Strategic Missiles (SMs) – 17 launched.
4672:
4516:
4228:
3206:
2930:
1163:
1144:
1125:
1106:
1087:
1068:
517:
149:
45:
2386:
5139:
2920:
1266:. One remained in use at Vandenberg AFB until it guided a last Thor-Agena launch in May 1972. It had guided over 400 missiles.
1220:
were deployed in 1963, the Titan I and Atlas missiles became obsolete. They were retired from service as ICBMs in early 1965.
5198:
4707:
2815:
3262:
1501:
SM-?? (stg. 1 only) Science Museum, Bayamon, Puerto Rico (top half from Bell's Junkyard) Vert. (stg 1 mated to stg 1 above)
2789:
1985:
4777:
4521:
4429:
4414:
1492:
SM-?? (stg. 1 only) former Spaceport USA Rocket Garden, Kennedy Space Center, Florida. Vert. (stg 1 mated to stg 1 below)
684:
2683:
2617:
United States Cold War Missile Program,U.S. Army Construction Engineering Research Laboratories, Champaign, IL., page 137
1495:
SM-?? (stg. 1 only) former Spaceport USA Rocket Garden, Kennedy Space Center, Florida. Vert. (stg 1 mated to stg 1 above)
1462:
SM-92 61-4519 (st. 1) Kansas Cosmosphere, Hutchinson, Kansas. (acq. 11/93 from MCDD) Vertical (st 1 mate to SM-94 st 1)
5155:
4770:
4697:
4692:
4511:
4378:
3298:
2500:
Simpson, Charles G, The Titan I part 2, Breckenridge, Colorado: Association of Air Force Missileers, October 1993, p. 5.
2293:
1270:
4600:
1761:
1468:
SM-94 61-4521 (st. 1) Kansas Cosmosphere, Hutchinson, Kansas. (acq. 6/93 from MCDD) Vertical (st 1 mate to SM-92 st 1)
929:
controlled a total of nine missiles divided among three launch sites, with the six operational units spread across the
4803:
4176:
2988:
1248:
580:
169:
2545:
Simpson, Charles G, The Titan I part 1, Breckenridge, Colorado: Association of Air Force Missileers, July 1993, p. 3.
2153:
Hansen, Chuck, Swords of Armageddon, 1995, Chukelea Publications, Sunnyvale, California, page Volume VII Page 290-293
4788:
3530:
1227:(VAFB) occurred on 5 March 1965. At that time, the disposition of the 101 total production missiles was as follows:
483:
models were equipped with what would have been the Titan I's guidance system The Titan I would be deployed with the
4687:
4471:
4151:
3916:
3911:
3790:
3370:
3328:
1453:
1259:
938:
1615:
4338:
4253:
4186:
4016:
3780:
3545:
3249:
2871:
Sheehan, Neil, “A Fiery Peace in a Cold War: Bernard Schriever and the Ultimate Weapon.” New York: Random House.
2164:
2067:
Achieving Accuracy a Legacy of Computers and Missiles, by Marshall W. McMurran, p 141, Xlibris Corporation, 2008
1437:
1418:
1397:
1387:
1224:
906:
5188:
5114:
4727:
4662:
3323:
3308:
2731:
McMurran, Marshall W., Achieving Accuracy a Legacy of Computers and Missiles, p 141, Xlibris Corporation, 2008
679:
with a yield of 3.75 megatons which was fuzed for either air burst or contact burst. The Mk 4 RV also deployed
4820:
4560:
4166:
3484:
3036:
1263:
621:
435:
427:
391:
70:
4796:
3981:
3391:
3026:
2981:
2858:
Mc Murran, Marshall W, “Achieving Accuracy a Legacy of Computers and Missiles,” Xlibris Corporation, 2008
1537:
1511:
Note: Two stacked Titan-1 first stages created a perfect illusion of a Titan-2 Missile for museums above.
568:
such as Missile C-3's range safety command destruct system relays being placed in a vibration-prone area.
5073:
5068:
4536:
4328:
3901:
3805:
3016:
1532:
1523:(MISS)". Two of the four firms which responded, Martin and Avco, proposed using Titan I as the booster.
1441:
1407:
SM-70 61-4497 Veterans Home, Quincy, IL Vertical (removed and sent to DMAFB for destruction in May 2010)
1401:
930:
676:
604:
4203:
4171:
1504:
SM-?? (full missile) former Outside main gate of White Sands Missile Range, N.M. false report? Vertical
5160:
4732:
4682:
4590:
4100:
3538:
3406:
3396:
3313:
3303:
3170:
3119:
1520:
843:
835:
88:
4398:
4393:
3145:
1887:
Stumpf, David K., Titan II, p 22-26, The University of Arkansas Press, Fayetteville, Arkansas, 2000
548:
5063:
4278:
4238:
4233:
4078:
4001:
2938:
2127:
Widnal Perair S., Lecture L14 - Variable Mass Systems The: Rocket Equation, 2008, MIT OpenCourseWar
384:
4570:
4531:
4363:
1967:
Stumpf, David K., Titan II, p 277, The University of Arkansas Press, Fayetteville, Arkansas, 2000
1926:
Stumpf, David K., Titan II, p 276, The University of Arkansas Press, Fayetteville, Arkansas, 2000
5058:
4313:
4263:
4198:
4120:
4088:
3795:
3653:
2679:
2609:
Stumpf, David K., Titan II, p 31, The University of Arkansas Press, Fayetteville, Arkansas, 2000
1393:
SM-67 61-4494 Titusville High School, Titusville, Florida (on Route US-1) removed, was horizontal
1080:
954:
851:
3510:
3175:
668:-General was selected to design and manufacture the engines for the Titan. Aerojet produced the
3165:
3160:
3155:
1244:(three at VAFB, one at each of five bases, one at Lowry, and 20 in storage at SBAMA elsewhere)
5104:
4968:
4742:
4722:
4373:
4318:
4273:
4243:
4041:
4031:
3866:
3611:
3442:
2942:
2897:
2887:
2872:
2859:
2732:
2610:
2445:
2219:
2137:
2111:
2068:
1968:
1927:
1888:
1731:
1459:
SM-89 61-4516 (st. 2) Pima Air Museum, outside DM AFB, Tucson, Arizona, now WPAFB Horizontal
1370:
1217:
1095:
625:
410:
364:
4545:
4368:
4130:
3437:
3150:
1824:
575:
Titan I missile emerges from its silo at Vandenberg Operational System Test Facility in 1960.
5129:
5013:
4998:
4877:
4737:
4642:
4358:
4343:
4223:
4218:
4125:
4110:
3971:
3961:
3735:
3725:
3708:
3623:
3063:
1547:
1465:
SM-93 61-4520 (st. 2) SLC-10 Museum, Vandenberg AFB, Lompoc, Ca. Horizontal (only stage 2)
1348:
1213:
961:. Each missile complex had three Titan I ICBM missiles ready to launch at any given time.
942:
882:
830:
826:
423:
406:
312:
252:
2886:
Stumpf, David K., Titan II, The University of Arkansas Press, Fayetteville, Arkansas, 2000
2200:
1498:
SM-?? (stg. 1 only) Science Museum, Bayamon, Puerto Rico Vert. (stg 1 mated to stg 1 below)
1427:
SM-79 61-4506 former Oklahoma State Fair Grounds, Oklahoma City, Oklahoma. 1960s Horizontal
445:
The Titan I was initially designated as a bomber aircraft (B-68), but was later designated
5124:
4948:
4595:
4580:
4550:
4491:
4439:
4434:
4388:
4303:
4258:
4161:
4006:
3976:
3946:
3941:
3936:
3785:
3770:
3765:
3740:
3730:
3668:
3633:
3601:
3586:
3489:
3432:
2933:
by Kristin Alexander about Titan 1 complexes in Washington State. Published 22 March 1998.
2924:
1188:
875:
680:
608:
439:
413:
until 1987 and had increased capacity and range in addition to the different propellants.
357:
2261:
1362:
SM-53 60-3698 Site 395-C Museum, Vandenberg AFB, Lompoc, Ca. (from March AFB) Horizontal
5048:
5028:
5008:
5003:
4657:
4555:
4481:
4454:
4383:
4248:
4156:
4115:
4083:
4068:
4026:
3921:
3896:
3881:
3845:
3835:
3800:
3775:
3755:
3720:
3673:
3638:
3596:
3140:
1478:
SM-101 61-4528 Estrella Warbirds Museum, Paso Robles, CA (2nd stage damaged) Horizontal
1356:
1338:
R&D (57–2743) Colorado State Capitol display 1959 (SN belongs to a Bomarc) Vertical
497:
5177:
5078:
5053:
5023:
4958:
4933:
4923:
4903:
4887:
4496:
4461:
4449:
4444:
4333:
4181:
3991:
3931:
3906:
3886:
3876:
3850:
3830:
3825:
3820:
3815:
3810:
3715:
3698:
3648:
3628:
3606:
3581:
3576:
2950:
2775:
2431:
2390:
1352:
1152:
925:
475:
467:
376:
237:
624:(which became "The Martin Company" in 1957), Titan I was a two-stage, liquid-fueled
5134:
4978:
4973:
4938:
4882:
4872:
4867:
4862:
4857:
4852:
4847:
4621:
4605:
4585:
4575:
4565:
4526:
4476:
4466:
4419:
4353:
4323:
4283:
4268:
4105:
4058:
4011:
3986:
3951:
3871:
3760:
3678:
3591:
3079:
2917:
1730:
Divine, Robert A., The Sputnik Challenge, New York: Oxford University Press, 1990,
1424:
SM-73 61-4500 former Holiday Motor Lodge, San Bernardino (now missing?). Horizontal
1319:
1156:
958:
868:
864:
847:
463:
399:
2819:
2630:
1449:
SM-86 61-4513 Beale AFB (not on display, was horizontal, removed 1994) Horizontal
5094:
5018:
4993:
4988:
4963:
4943:
4928:
4842:
4293:
4063:
4053:
3956:
3744:
3693:
3663:
3658:
3643:
3618:
3386:
3021:
2444:
Walker, Chuck Atlas The Ultimate Weapon, Burlington Canada: Apogee Books, 2005,
2110:
Walker,Chuck, Atlas The Ultimate Weapon, Burlington Canada: Apogee Books, 2005,
1989:
890:
459:
446:
394:
371:
241:
1309:
Titan-I ICBM SM vehicles being destroyed at Mira Loma AFS for the SALT-1 Treaty
1297:
Titan-I ICBM SM vehicles being destroyed at Mira Loma AFS for the SALT-1 Treaty
1285:
Titan-I ICBM SM vehicles being destroyed at Mira Loma AFS for the SALT-1 Treaty
5119:
5109:
5099:
5043:
5038:
4095:
3996:
3966:
3180:
3104:
3099:
3094:
3089:
3084:
2688:
1175:
1076:
950:
922:
902:
661:
584:
17:
579:
In December, Missile V-2 was undergoing a flight readiness test in a silo at
4677:
3891:
3840:
3411:
3114:
3109:
2963:
2793:
2333:
2242:
1765:
1480:
1171:
1133:
1114:
894:
878:
set with 440 volt 3 phase AC input weighed over 2 tons" at remote locations
484:
480:
1341:
R&D G-type Science and Technology Museum, Chicago 21 June 1963 Vertical
2040:
Guidance Changes Made on Atlas, Titan, Aviation Week 28 July 1958, page 22
675:
The warhead of the Titan I was an AVCO Mk 4 re-entry vehicle containing a
37:
4540:
3124:
2968:
1374:
1137:
1118:
934:
638:
5033:
4424:
4298:
4288:
4213:
4146:
3515:
3505:
3401:
3185:
2365:
909:
in California, the last of over 400 missile flights using the Athena.
807:
761:
665:
513:
49:
2168:
346:
4983:
4506:
4486:
4348:
4308:
4208:
4073:
4048:
4021:
3926:
2957:
2937:
Information on "Northern California Triad" of Titan missile bases in
2773:”Missile Destroyed in First Sdi Test At High-energy Laser Facility”,
1234:
one was destroyed in Beale AFB Site 851-C1 silo explosion 24 May 1962
822:
479:
silo and an improved fully internal inertial guidance system. Later
2279:
901:, during a missile launch. The last Athena-controlled launch was a
5161:
United States tri-service missile and drone designations post-1962
4702:
4652:
4647:
3750:
3688:
3683:
3452:
3447:
3427:
3365:
3360:
3355:
2389:. Johnathan's Space Report Launch Vehicle Database. Archived from
2268:. A Third Survey of Domestic Electronic Digital Computing Systems.
1479:
1431:
1383:
SM-63 60-3708 In storage at Edwards AFB (still there?) Horizontal
1318:
1099:
946:
570:
2710:
3457:
2973:
1430:
SM-81 61-4508 Kansas Cosmosphere, Hutchinson, Kansas. In storage
810:
764:
669:
630:
533:
529:
525:
521:
380:
333:
293:
273:
226:
60:
4792:
3534:
2977:
1489:
SM-?? (stg. 2 only) former SDI laser test target (whereabouts?)
687:
balloons which replicated the radar signature of the Mk 4 RV.
634:
337:
277:
2631:"Mira Loma Quartermaster. Depot (Mira Loma Air Force Station"
1231:
17 were test launched from VAFB (September 1961 – March 1965)
1825:
https://nsarchive2.gwu.edu/nukevault/ebb249/doc02-vol1.pdf
1421:
Air and Space Museum, Florence, South Carolina. Horizontal
2851:
USAF Historical Division Liaison Office: Ann Arbor, 1967.
2349:"Letter Concerning the Last Athena guided Missile Launch"
2049:
Titan Guidance Switch, Aviation Week 6 April 195, page 31
5194:
Intercontinental ballistic missiles of the United States
4772:
United States tri-service rocket designations post-1963
1456:, outside DM AFB, Tucson, Arizona, now WPAFB Horizontal
2964:
A site for the Univac Athena Missile Guidance Computer
846:
design with separate data and instruction memories by
1475:, Ellsworth AFB, Rapid City, South Dakota. Horizontal
897:
circuits such as fuses from deactivating the machine
5087:
4916:
4896:
4835:
4828:
4635:
4614:
4407:
4139:
3859:
3569:
3562:
1963 United States Tri-Service missile designations
3498:
3477:
3470:
3420:
3379:
3348:
3341:
3286:
3248:
3205:
3198:
3133:
3072:
3051:
3044:
3009:
2301:
Carnegie Institute of Technology Computation Center
720:
Titan base cost: $ 170,000,000 (US$ 1.75B in 2024)
329:
321:
311:
299:
288:
283:
269:
261:
251:
232:
221:
216:
208:
200:
192:
184:
176:
145:
137:
132:
124:
116:
108:
100:
95:
84:
76:
66:
56:
708:Development cost: $ 1,643,300,000 in 1960 dollars.
1247:The 83 surplus missiles remained in inventory at
27:Early American intercontinental ballistic missile
2849:The Air Force and Strategic Deterrence 1951-1960
1944:"Titan I Captive and Flight Test Firing History"
711:Flyaway cost: $ 1,500,000 each, in 1962 dollars.
370:(ICBM), in use from 1959 until 1962. Though the
2969:The most comprehensive site about Titan I bases
2927:by Earl See Titan Missile Memoirs. Summer 2014.
5184:Cold War nuclear missiles of the United States
1857:Martin Marietta Corporation (September 1972).
1543:List of military aircraft of the United States
1507:SM-?? (full missile) Spacetec CCAFS Horizontal
4804:
3546:
2989:
383:as propellants; all subsequent versions used
8:
2918:American Aviation Historical Society Journal
2818:. Encyclopedia Astronautica=. Archived from
2792:. Encyclopedia Astronautica=. Archived from
1367:Strategic Air Command & Aerospace Museum
1237:54 were deployed in silos on 20 January 1965
1062:Map Of HGM-25A Titan I Operational Squadrons
829:to transmit to the Titan missile as part of
390:Originally designed as a backup in case the
30:
2188:
2186:
1414:, now AMARC (to go to PIMA Mus.) Horizontal
5204:Military equipment introduced in the 1950s
4832:
4811:
4797:
4789:
3553:
3539:
3531:
3474:
3345:
3202:
3048:
2996:
2982:
2974:
2237:
2235:
1323:Titan I in Cordele, Georgia, I-75 exit 101
803:Propellants: liquid oxygen (LOX), kerosene
788:Isp (sea level): 210 s (2.06 kN·s/kg)
757:Propellants: liquid oxygen (LOX), kerosene
742:Isp (sea level): 256 s (2.51 kN·s/kg)
29:
2711:"The Hotchkiss Titan I ICBM Missile Base"
2429:"Guidance Changes Made on Atlas, Titan",
2334:"Univac Athena Missile Guidance Computer"
2243:"Univac Athena Missile Guidance Computer"
1797:
1795:
2625:
2623:
2496:
2494:
2027:
2025:
1843:
1841:
1811:
1809:
1807:
1785:
1783:
1746:
1744:
1708:
1706:
1922:
1920:
1918:
1592:
1590:
1559:
1390:, Mountain View, California. Horizontal
1275:
861:AN/GSK-1 Computer Set Console (OA-2654)
402:basing was more survivable than Atlas.
2224:: CS1 maint: archived copy as title (
2217:
1984:Air Force Space & Missile Museum.
1760:Air Force Space & Missile Museum.
893:" mode ("melt-before-fail") prevented
717:Total deployed strategic missiles: 54.
2689:"Abandoned Titan I Missile Base – CO"
881:input from one of two large AN/GRW-5
739:Isp (vac): 290 s (2.84 kN·s/kg)
595:second stage engine failed to start.
7:
1333:Air Force Space & Missile Museum
785:Isp (vac): 308 s (3.02 kN·s/kg)
42:Launch of a Titan I SM/567.8-90 ICBM
2947:Live Oak, Sutter County, California
2748:Shufelt, Wayne (17 October 1972).
2280:"UNIVAC 24-bit computer genealogy"
2167:. missilebases.com. Archived from
368:intercontinental ballistic missile
25:
5156:USAF missile designations 1947–51
4778:Drones designated in UAV sequence
2366:"Information Technology Pioneers"
1473:South Dakota Air and Space Museum
1044:
1030:
1016:
1002:
988:
974:
857:Used with the computer were the:
426:. The committee presented to the
120:105,140 kg (231,790 lb)
3035:
2633:. California Military Department
1302:
1290:
1278:
1164:851st Strategic Missile Squadron
1145:850th Strategic Missile Squadron
1126:725th Strategic Missile Squadron
1107:724th Strategic Missile Squadron
1088:569th Strategic Missile Squadron
1069:568th Strategic Missile Squadron
1043:
1029:
1015:
1001:
987:
973:
966:
518:Cape Canaveral Air Force Station
487:radio-inertial guidance system.
36:
5140:Supersonic Low Altitude Missile
4823:rocket and missile designations
4187:BGM-109/AGM-109/RGM-109/UGM-109
1396:SM-69 61-4496 (full missile)
1344:SM-5 60-3650 Lompoc? Horizontal
2260:Weik, Martin H. (March 1961).
905:missile launched in 1972 from
1:
854:and cost about $ 1,800,000.
696:Liftoff thrust: 1,296 kN
449:and finally HGM-25A in 1962.
424:Scientific Advisory Committee
363:was the United States' first
2779:, 23 September 1985, page 17
2755:. Letter to Dr. Uta Merzbach
1315:Static displays and articles
1271:Strategic Defense Initiative
1618:. Strategic-Air-Command.com
1454:Pima Air & Space Museum
1240:29 were in storage at SBAMA
842:The Athena computer used a
825:Athena computer calculated
736:Thrust (vac): 1,467 kN
699:Total mass: 105,142 kg
599:on impact with the ground.
5220:
2691:. YouTube. 15 October 2014
2165:"History of Missile Bases"
1515:Prospective manned flights
1331:B2 57-2691 Cape Canaveral
1166:February 1961 – March 1965
776:Gross mass: 28,939 kg
730:Gross mass: 76,203 kg
112:3.05 m (10.0 ft)
5148:
4761:
3033:
2163:missilebases.com (2011).
1438:Discovery Park of America
1419:Florence Regional Airport
1398:Discovery Park of America
1388:NASA Ames Research Center
1225:Vandenberg Air Force Base
1212:When the storable-fueled
907:Vandenberg Air Force Base
839:short tons; 9.5 t).
779:Empty mass: 1,725 kg
733:Empty mass: 4,000 kg
677:W38 thermonuclear warhead
581:Vandenberg Air Force Base
343:
35:
2750:"Univac Athena computer"
2387:"List of Titan Launches"
2294:"Athena Reference guide"
817:Athena guidance computer
782:Thrust (vac):356 kN
4821:United States Air Force
2958:Titan 1 Upgrade Project
2931:Tri-City Herald article
2923:4 December 2021 at the
2435:, 28 July 1958, page 22
1452:SM-88 61-4515 (st. 1)
1264:Smithsonian Institution
1071:April 1961 – March 1965
852:Sperry Rand Corporation
806:Number of engines: one
760:Number of engines: two
622:Glenn L. Martin Company
428:United States Air Force
104:31 m (102 ft)
2816:"Martin Project 7969s"
1538:List of Titan launches
1485:
1445:
1324:
1223:The final launch from
1147:June 1960 – March 1965
1128:April 1961 – June 1965
1109:April 1961 – June 1965
1090:June 1961 – March 1965
605:hypergolic propellants
576:
520:from Launch Complexes
361:SM-68A/HGM-25A Titan I
5199:Titan (rocket family)
4748:M30 GMLRS/M31 GMLRS-U
2960:at NASA Moffett Field
1483:
1435:
1412:U.S. Air Force Museum
1402:Union City, Tennessee
1322:
1216:and the solid-fueled
931:western United States
633:) and liquid oxygen (
574:
4032:AGM-84/RGM-84/UGM-84
3120:Commercial Titan III
2790:"Avco Project 7969s"
2206:on 16 September 2012
1521:Man in Space Soonest
1335:, Florida Horizontal
1269:On 6 September 1985
1059:class=notpageimage|
844:Harvard architecture
836:ballistic trajectory
705:Total length: 31.0 m
702:Core diameter: 3.1 m
385:storable propellants
4829:Air-to-air missiles
3511:Pratt & Whitney
2939:Lincoln, California
2847:Lemmer, George F.,
2822:on 28 December 2016
2393:on 23 February 2016
1992:on 12 November 2019
1533:Titan rocket family
409:served in the U.S.
32:
5088:Undesignated types
4897:1961–1963 sequence
4836:1955–1961 sequence
2303:. 22 October 1968.
2249:. 26 January 2018.
1486:
1446:
1325:
831:Western Electric's
577:
491:Budgetary problems
453:Program management
436:The Martin Company
5169:
5168:
4912:
4911:
4786:
4785:
3528:
3527:
3524:
3523:
3466:
3465:
3337:
3336:
3194:
3193:
2943:Chico, California
2864:978-1-4363-8106-2
2737:978-1-4363-8106-2
2332:DiVecchio, Mark.
2073:978-1-4363-8106-2
1436:SM-69 61-4496 at
1096:Mountain Home AFB
637:) meant that the
626:ballistic missile
411:nuclear deterrent
354:
353:
303:356 kN (80,000 lb
77:Country of origin
16:(Redirected from
5211:
4833:
4813:
4806:
4799:
4790:
4773:
3555:
3548:
3541:
3532:
3475:
3346:
3203:
3064:LGM-25C Titan II
3049:
3039:
2998:
2991:
2984:
2975:
2877:978-0679-42284-6
2832:
2831:
2829:
2827:
2812:
2806:
2805:
2803:
2801:
2786:
2780:
2771:
2765:
2764:
2762:
2760:
2754:
2745:
2739:
2729:
2723:
2722:
2720:
2718:
2713:. Bari Hotchkiss
2707:
2701:
2700:
2698:
2696:
2676:
2670:
2667:
2661:
2658:
2652:
2649:
2643:
2642:
2640:
2638:
2627:
2618:
2607:
2601:
2597:
2591:
2588:
2582:
2579:
2573:
2570:
2564:
2561:
2555:
2552:
2546:
2543:
2537:
2534:
2528:
2525:
2519:
2516:
2510:
2507:
2501:
2498:
2489:
2486:
2480:
2477:
2471:
2468:
2462:
2459:
2453:
2442:
2436:
2427:
2421:
2418:
2412:
2409:
2403:
2402:
2400:
2398:
2383:
2377:
2376:
2374:
2372:
2362:
2356:
2355:
2353:
2347:Shufelt, Wayne.
2344:
2338:
2337:
2329:
2323:
2320:
2314:
2311:
2305:
2304:
2298:
2290:
2284:
2283:
2276:
2270:
2269:
2257:
2251:
2250:
2239:
2230:
2229:
2223:
2215:
2213:
2211:
2205:
2199:. Archived from
2198:
2190:
2181:
2180:
2178:
2176:
2160:
2154:
2151:
2145:
2134:
2128:
2125:
2119:
2108:
2102:
2099:
2093:
2090:
2084:
2081:
2075:
2065:
2059:
2056:
2050:
2047:
2041:
2038:
2032:
2029:
2020:
2017:
2011:
2008:
2002:
2001:
1999:
1997:
1988:. Archived from
1981:
1975:
1965:
1959:
1958:
1956:
1954:
1948:
1940:
1934:
1924:
1913:
1910:
1904:
1901:
1895:
1885:
1879:
1876:
1870:
1869:
1867:
1865:
1854:
1848:
1845:
1836:
1833:
1827:
1822:
1816:
1813:
1802:
1799:
1790:
1787:
1778:
1777:
1775:
1773:
1768:on 29 March 2020
1764:. Archived from
1757:
1751:
1748:
1739:
1728:
1722:
1719:
1713:
1710:
1701:
1698:
1692:
1688:
1682:
1679:
1673:
1670:
1664:
1661:
1655:
1652:
1646:
1643:
1637:
1634:
1628:
1627:
1625:
1623:
1612:
1606:
1603:
1597:
1594:
1585:
1582:
1576:
1573:
1567:
1564:
1548:List of missiles
1349:Cordele, Georgia
1306:
1294:
1282:
1047:
1046:
1033:
1032:
1019:
1018:
1005:
1004:
991:
990:
977:
976:
970:
933:in five states:
883:Western Electric
791:Burn time: 225 s
745:Burn time: 138 s
681:penetration aids
655:
654:
650:
647:
620:Produced by the
407:LGM-25C Titan II
392:U.S. Air Force's
347:edit on Wikidata
313:Specific impulse
253:Specific impulse
172:OSTF SLTF LC-395
40:
33:
21:
5219:
5218:
5214:
5213:
5212:
5210:
5209:
5208:
5189:Lockheed Martin
5174:
5173:
5170:
5165:
5144:
5083:
4908:
4892:
4824:
4817:
4787:
4782:
4771:
4757:
4631:
4610:
4403:
4274:RUM-125/UUM-125
4254:CQM-121/CGM-121
4135:
3855:
3565:
3559:
3529:
3520:
3494:
3490:Lockheed Martin
3462:
3416:
3375:
3333:
3282:
3244:
3190:
3129:
3068:
3059:HGM-25A Titan I
3040:
3031:
3005:
3002:
2925:Wayback Machine
2914:
2841:
2836:
2835:
2825:
2823:
2814:
2813:
2809:
2799:
2797:
2796:on 4 March 2016
2788:
2787:
2783:
2772:
2768:
2758:
2756:
2752:
2747:
2746:
2742:
2730:
2726:
2716:
2714:
2709:
2708:
2704:
2694:
2692:
2687:
2684:Wayback Machine
2677:
2673:
2668:
2664:
2659:
2655:
2650:
2646:
2636:
2634:
2629:
2628:
2621:
2608:
2604:
2598:
2594:
2589:
2585:
2580:
2576:
2571:
2567:
2562:
2558:
2553:
2549:
2544:
2540:
2535:
2531:
2526:
2522:
2517:
2513:
2508:
2504:
2499:
2492:
2487:
2483:
2478:
2474:
2469:
2465:
2460:
2456:
2443:
2439:
2428:
2424:
2419:
2415:
2410:
2406:
2396:
2394:
2385:
2384:
2380:
2370:
2368:
2364:
2363:
2359:
2351:
2346:
2345:
2341:
2331:
2330:
2326:
2321:
2317:
2312:
2308:
2296:
2292:
2291:
2287:
2278:
2277:
2273:
2259:
2258:
2254:
2241:
2240:
2233:
2216:
2209:
2207:
2203:
2196:
2194:"Archived copy"
2192:
2191:
2184:
2174:
2172:
2171:on 2 March 2009
2162:
2161:
2157:
2152:
2148:
2135:
2131:
2126:
2122:
2109:
2105:
2100:
2096:
2091:
2087:
2082:
2078:
2066:
2062:
2057:
2053:
2048:
2044:
2039:
2035:
2030:
2023:
2018:
2014:
2009:
2005:
1995:
1993:
1983:
1982:
1978:
1966:
1962:
1952:
1950:
1949:. February 1962
1946:
1942:
1941:
1937:
1925:
1916:
1911:
1907:
1902:
1898:
1886:
1882:
1877:
1873:
1863:
1861:
1856:
1855:
1851:
1846:
1839:
1834:
1830:
1823:
1819:
1814:
1805:
1800:
1793:
1788:
1781:
1771:
1769:
1759:
1758:
1754:
1749:
1742:
1729:
1725:
1720:
1716:
1711:
1704:
1699:
1695:
1689:
1685:
1680:
1676:
1671:
1667:
1662:
1658:
1653:
1649:
1644:
1640:
1635:
1631:
1621:
1619:
1616:"Titan Missile"
1614:
1613:
1609:
1604:
1600:
1595:
1588:
1583:
1579:
1574:
1570:
1565:
1561:
1556:
1529:
1517:
1317:
1310:
1307:
1298:
1295:
1286:
1283:
1210:
1184:
1065:
1064:
1063:
1061:
1055:
1054:
1053:
1052:
1048:
1040:
1039:
1038:
1034:
1026:
1025:
1024:
1020:
1012:
1011:
1010:
1006:
998:
997:
996:
992:
984:
983:
982:
978:
941:, both east of
915:
913:Service history
876:motor-generator
827:ground commands
819:
794:Diameter: 2.3 m
748:Diameter: 3.1 m
693:
683:in the form of
652:
648:
645:
643:
618:
616:Characteristics
609:Robert McNamara
506:
493:
455:
419:
405:The succeeding
358:Martin Marietta
350:
306:
245:
204:6 February 1959
196:17 (suborbital)
188:53 (suborbital)
180:70 (suborbital)
168:
156:
85:Cost per launch
52:
43:
28:
23:
22:
15:
12:
11:
5:
5217:
5215:
5207:
5206:
5201:
5196:
5191:
5186:
5176:
5175:
5167:
5166:
5164:
5163:
5158:
5149:
5146:
5145:
5143:
5142:
5137:
5132:
5127:
5122:
5117:
5112:
5107:
5102:
5097:
5091:
5089:
5085:
5084:
5082:
5081:
5076:
5071:
5066:
5061:
5056:
5051:
5046:
5041:
5036:
5031:
5026:
5021:
5016:
5011:
5006:
5001:
4996:
4991:
4986:
4981:
4976:
4971:
4966:
4961:
4956:
4951:
4946:
4941:
4936:
4931:
4926:
4920:
4918:
4914:
4913:
4910:
4909:
4907:
4906:
4900:
4898:
4894:
4893:
4891:
4890:
4885:
4880:
4875:
4870:
4865:
4860:
4855:
4850:
4845:
4839:
4837:
4830:
4826:
4825:
4818:
4816:
4815:
4808:
4801:
4793:
4784:
4783:
4781:
4780:
4775:
4768:
4762:
4759:
4758:
4756:
4755:
4750:
4745:
4740:
4735:
4730:
4725:
4720:
4715:
4710:
4705:
4700:
4695:
4690:
4685:
4680:
4675:
4670:
4665:
4660:
4658:Common Missile
4655:
4650:
4645:
4639:
4637:
4633:
4632:
4630:
4629:
4624:
4618:
4616:
4612:
4611:
4609:
4608:
4603:
4598:
4593:
4588:
4583:
4578:
4573:
4568:
4563:
4558:
4553:
4548:
4543:
4534:
4529:
4524:
4519:
4514:
4509:
4504:
4499:
4494:
4489:
4484:
4479:
4474:
4469:
4464:
4459:
4458:
4457:
4447:
4442:
4437:
4432:
4427:
4422:
4417:
4411:
4409:
4405:
4404:
4402:
4401:
4396:
4391:
4386:
4381:
4376:
4371:
4366:
4361:
4356:
4351:
4346:
4341:
4336:
4331:
4326:
4321:
4316:
4311:
4306:
4301:
4296:
4291:
4286:
4281:
4276:
4271:
4266:
4261:
4256:
4251:
4246:
4241:
4236:
4231:
4226:
4221:
4216:
4211:
4206:
4201:
4196:
4195:
4194:
4184:
4179:
4174:
4169:
4164:
4159:
4154:
4149:
4143:
4141:
4137:
4136:
4134:
4133:
4128:
4123:
4118:
4113:
4108:
4103:
4098:
4093:
4092:
4091:
4081:
4076:
4071:
4066:
4061:
4056:
4051:
4046:
4045:
4044:
4039:
4029:
4024:
4019:
4014:
4009:
4004:
3999:
3994:
3989:
3984:
3979:
3974:
3969:
3964:
3959:
3954:
3949:
3944:
3939:
3934:
3929:
3924:
3919:
3914:
3909:
3904:
3899:
3894:
3889:
3884:
3879:
3874:
3869:
3863:
3861:
3857:
3856:
3854:
3853:
3848:
3843:
3838:
3833:
3828:
3823:
3818:
3813:
3808:
3803:
3798:
3793:
3788:
3783:
3778:
3773:
3768:
3763:
3758:
3753:
3748:
3738:
3733:
3728:
3723:
3718:
3713:
3712:
3711:
3701:
3696:
3691:
3686:
3681:
3676:
3671:
3666:
3661:
3656:
3651:
3646:
3641:
3636:
3631:
3626:
3621:
3616:
3615:
3614:
3604:
3599:
3594:
3589:
3584:
3579:
3573:
3571:
3567:
3566:
3564:, 1963–present
3560:
3558:
3557:
3550:
3543:
3535:
3526:
3525:
3522:
3521:
3519:
3518:
3513:
3508:
3502:
3500:
3496:
3495:
3493:
3492:
3487:
3481:
3479:
3472:
3468:
3467:
3464:
3463:
3461:
3460:
3455:
3450:
3445:
3440:
3435:
3430:
3424:
3422:
3418:
3417:
3415:
3414:
3409:
3404:
3399:
3394:
3389:
3383:
3381:
3377:
3376:
3374:
3373:
3368:
3363:
3358:
3352:
3350:
3343:
3339:
3338:
3335:
3334:
3332:
3331:
3326:
3321:
3316:
3311:
3306:
3301:
3296:
3290:
3288:
3284:
3283:
3281:
3280:
3275:
3270:
3265:
3260:
3254:
3252:
3246:
3245:
3243:
3242:
3237:
3232:
3227:
3222:
3217:
3211:
3209:
3207:Cape Canaveral
3200:
3196:
3195:
3192:
3191:
3189:
3188:
3183:
3178:
3173:
3168:
3163:
3158:
3153:
3148:
3146:Titan-Vanguard
3143:
3137:
3135:
3131:
3130:
3128:
3127:
3122:
3117:
3112:
3107:
3102:
3097:
3092:
3087:
3082:
3076:
3074:
3073:Launch Systems
3070:
3069:
3067:
3066:
3061:
3055:
3053:
3046:
3042:
3041:
3034:
3032:
3030:
3029:
3024:
3019:
3013:
3011:
3007:
3006:
3003:
3001:
3000:
2993:
2986:
2978:
2972:
2971:
2966:
2961:
2955:
2934:
2928:
2913:
2912:External links
2910:
2909:
2908:
2905:
2894:
2884:
2880:
2869:
2866:
2856:
2852:
2845:
2840:
2837:
2834:
2833:
2807:
2781:
2766:
2740:
2724:
2702:
2671:
2662:
2653:
2644:
2619:
2602:
2592:
2583:
2574:
2565:
2556:
2547:
2538:
2529:
2520:
2511:
2502:
2490:
2481:
2472:
2463:
2454:
2437:
2422:
2413:
2404:
2378:
2357:
2339:
2324:
2315:
2306:
2285:
2271:
2252:
2247:Mark DiVecchio
2231:
2182:
2155:
2146:
2129:
2120:
2103:
2094:
2085:
2076:
2060:
2051:
2042:
2033:
2021:
2012:
2003:
1986:"Complex 395A"
1976:
1960:
1935:
1914:
1905:
1896:
1880:
1871:
1849:
1837:
1828:
1817:
1803:
1791:
1779:
1752:
1740:
1723:
1714:
1702:
1693:
1683:
1674:
1665:
1656:
1647:
1638:
1629:
1607:
1598:
1586:
1577:
1568:
1558:
1557:
1555:
1552:
1551:
1550:
1545:
1540:
1535:
1528:
1525:
1516:
1513:
1509:
1508:
1505:
1502:
1499:
1496:
1493:
1490:
1487:
1476:
1471:SM-96 61-4523
1469:
1466:
1463:
1460:
1457:
1450:
1447:
1442:Union City, TN
1428:
1425:
1422:
1417:SM-72 61-4499
1415:
1410:SM-71 61-4498
1408:
1405:
1394:
1391:
1386:SM-65 61-4492
1384:
1381:
1378:
1365:SM-54 60-3699
1363:
1360:
1357:U.S. Route 280
1355:, exit 101 at
1351:(west side of
1347:SM-49 60-3694
1345:
1342:
1339:
1336:
1316:
1313:
1312:
1311:
1308:
1301:
1299:
1296:
1289:
1287:
1284:
1277:
1242:
1241:
1238:
1235:
1232:
1209:
1206:
1183:
1180:
1179:
1178:
1168:
1167:
1160:
1159:
1149:
1148:
1141:
1140:
1130:
1129:
1122:
1121:
1111:
1110:
1103:
1102:
1092:
1091:
1084:
1083:
1073:
1072:
1057:
1056:
1050:
1049:
1042:
1041:
1036:
1035:
1028:
1027:
1022:
1021:
1014:
1013:
1008:
1007:
1000:
999:
994:
993:
986:
985:
980:
979:
972:
971:
965:
964:
963:
914:
911:
887:
886:
879:
872:
867:terminal with
862:
818:
815:
814:
813:
804:
801:
798:
795:
792:
789:
786:
783:
780:
777:
768:
767:
758:
755:
754:Length: 16.0 m
752:
749:
746:
743:
740:
737:
734:
731:
722:
721:
718:
715:
712:
709:
706:
703:
700:
697:
692:
691:Specifications
689:
617:
614:
549:Osmond Ritland
505:
504:Flight testing
502:
498:Sputnik crisis
492:
489:
454:
451:
418:
415:
352:
351:
344:
341:
340:
331:
327:
326:
323:
319:
318:
315:
309:
308:
304:
301:
297:
296:
290:
286:
285:
281:
280:
271:
267:
266:
263:
259:
258:
255:
249:
248:
243:
234:
230:
229:
223:
219:
218:
214:
213:
210:
206:
205:
202:
198:
197:
194:
190:
189:
186:
182:
181:
178:
177:Total launches
174:
173:
170:Vandenberg AFB
150:Cape Canaveral
147:
143:
142:
139:
135:
134:
133:Launch history
130:
129:
126:
122:
121:
118:
114:
113:
110:
106:
105:
102:
98:
97:
93:
92:
86:
82:
81:
78:
74:
73:
71:Martin Company
68:
64:
63:
58:
54:
53:
46:Cape Canaveral
41:
26:
24:
18:LGM-25 Titan I
14:
13:
10:
9:
6:
4:
3:
2:
5216:
5205:
5202:
5200:
5197:
5195:
5192:
5190:
5187:
5185:
5182:
5181:
5179:
5172:
5162:
5159:
5157:
5154:
5151:
5150:
5147:
5141:
5138:
5136:
5133:
5131:
5128:
5126:
5123:
5121:
5118:
5116:
5113:
5111:
5108:
5106:
5103:
5101:
5098:
5096:
5093:
5092:
5090:
5086:
5080:
5077:
5075:
5072:
5070:
5067:
5065:
5062:
5060:
5057:
5055:
5052:
5050:
5047:
5045:
5042:
5040:
5037:
5035:
5032:
5030:
5027:
5025:
5022:
5020:
5017:
5015:
5012:
5010:
5007:
5005:
5002:
5000:
4997:
4995:
4992:
4990:
4987:
4985:
4982:
4980:
4977:
4975:
4972:
4970:
4967:
4965:
4962:
4960:
4957:
4955:
4952:
4950:
4947:
4945:
4942:
4940:
4937:
4935:
4932:
4930:
4927:
4925:
4922:
4921:
4919:
4915:
4905:
4902:
4901:
4899:
4895:
4889:
4886:
4884:
4881:
4879:
4876:
4874:
4871:
4869:
4866:
4864:
4861:
4859:
4856:
4854:
4851:
4849:
4846:
4844:
4841:
4840:
4838:
4834:
4831:
4827:
4822:
4814:
4809:
4807:
4802:
4800:
4795:
4794:
4791:
4779:
4776:
4774:
4769:
4767:
4764:
4763:
4760:
4754:
4751:
4749:
4746:
4744:
4741:
4739:
4736:
4734:
4731:
4729:
4726:
4724:
4721:
4719:
4716:
4714:
4711:
4709:
4706:
4704:
4701:
4699:
4696:
4694:
4691:
4689:
4686:
4684:
4681:
4679:
4676:
4674:
4671:
4669:
4666:
4664:
4661:
4659:
4656:
4654:
4651:
4649:
4646:
4644:
4641:
4640:
4638:
4634:
4628:
4625:
4623:
4620:
4619:
4617:
4613:
4607:
4604:
4602:
4599:
4597:
4594:
4592:
4589:
4587:
4584:
4582:
4579:
4577:
4574:
4572:
4569:
4567:
4564:
4562:
4559:
4557:
4554:
4552:
4549:
4547:
4544:
4542:
4538:
4535:
4533:
4530:
4528:
4525:
4523:
4520:
4518:
4515:
4513:
4510:
4508:
4505:
4503:
4500:
4498:
4495:
4493:
4490:
4488:
4485:
4483:
4480:
4478:
4475:
4473:
4470:
4468:
4465:
4463:
4460:
4456:
4453:
4452:
4451:
4448:
4446:
4443:
4441:
4438:
4436:
4433:
4431:
4428:
4426:
4423:
4421:
4418:
4416:
4413:
4412:
4410:
4406:
4400:
4397:
4395:
4392:
4390:
4387:
4385:
4382:
4380:
4377:
4375:
4372:
4370:
4367:
4365:
4362:
4360:
4357:
4355:
4352:
4350:
4347:
4345:
4342:
4340:
4337:
4335:
4332:
4330:
4327:
4325:
4322:
4320:
4317:
4315:
4312:
4310:
4307:
4305:
4302:
4300:
4297:
4295:
4292:
4290:
4287:
4285:
4282:
4280:
4277:
4275:
4272:
4270:
4267:
4265:
4262:
4260:
4257:
4255:
4252:
4250:
4247:
4245:
4242:
4240:
4237:
4235:
4232:
4230:
4227:
4225:
4222:
4220:
4217:
4215:
4212:
4210:
4207:
4205:
4202:
4200:
4197:
4193:
4190:
4189:
4188:
4185:
4183:
4180:
4178:
4175:
4173:
4170:
4168:
4165:
4163:
4160:
4158:
4155:
4153:
4150:
4148:
4145:
4144:
4142:
4138:
4132:
4129:
4127:
4124:
4122:
4119:
4117:
4114:
4112:
4109:
4107:
4104:
4102:
4099:
4097:
4094:
4090:
4087:
4086:
4085:
4082:
4080:
4077:
4075:
4072:
4070:
4067:
4065:
4062:
4060:
4057:
4055:
4052:
4050:
4047:
4043:
4040:
4038:
4035:
4034:
4033:
4030:
4028:
4025:
4023:
4020:
4018:
4015:
4013:
4010:
4008:
4005:
4003:
4000:
3998:
3995:
3993:
3990:
3988:
3985:
3983:
3980:
3978:
3975:
3973:
3970:
3968:
3965:
3963:
3960:
3958:
3955:
3953:
3950:
3948:
3945:
3943:
3940:
3938:
3935:
3933:
3930:
3928:
3925:
3923:
3920:
3918:
3915:
3913:
3910:
3908:
3905:
3903:
3900:
3898:
3895:
3893:
3890:
3888:
3885:
3883:
3880:
3878:
3875:
3873:
3870:
3868:
3865:
3864:
3862:
3858:
3852:
3849:
3847:
3844:
3842:
3839:
3837:
3834:
3832:
3829:
3827:
3824:
3822:
3819:
3817:
3814:
3812:
3809:
3807:
3804:
3802:
3799:
3797:
3794:
3792:
3789:
3787:
3784:
3782:
3779:
3777:
3774:
3772:
3769:
3767:
3764:
3762:
3759:
3757:
3754:
3752:
3749:
3746:
3742:
3739:
3737:
3734:
3732:
3729:
3727:
3724:
3722:
3719:
3717:
3714:
3710:
3707:
3706:
3705:
3702:
3700:
3697:
3695:
3692:
3690:
3687:
3685:
3682:
3680:
3677:
3675:
3672:
3670:
3667:
3665:
3662:
3660:
3657:
3655:
3652:
3650:
3647:
3645:
3644:CGM-13/MGM-13
3642:
3640:
3637:
3635:
3632:
3630:
3627:
3625:
3622:
3620:
3617:
3613:
3610:
3609:
3608:
3605:
3603:
3600:
3598:
3595:
3593:
3590:
3588:
3585:
3583:
3580:
3578:
3575:
3574:
3572:
3568:
3563:
3556:
3551:
3549:
3544:
3542:
3537:
3536:
3533:
3517:
3514:
3512:
3509:
3507:
3504:
3503:
3501:
3497:
3491:
3488:
3486:
3483:
3482:
3480:
3476:
3473:
3471:Manufacturers
3469:
3459:
3456:
3454:
3451:
3449:
3446:
3444:
3441:
3439:
3436:
3434:
3431:
3429:
3426:
3425:
3423:
3419:
3413:
3410:
3408:
3405:
3403:
3400:
3398:
3395:
3393:
3390:
3388:
3385:
3384:
3382:
3378:
3372:
3369:
3367:
3364:
3362:
3359:
3357:
3354:
3353:
3351:
3347:
3344:
3340:
3330:
3327:
3325:
3322:
3320:
3319:Davis-Monthan
3317:
3315:
3312:
3310:
3307:
3305:
3302:
3300:
3299:Mountain Home
3297:
3295:
3292:
3291:
3289:
3285:
3279:
3276:
3274:
3271:
3269:
3266:
3264:
3261:
3259:
3256:
3255:
3253:
3251:
3247:
3241:
3238:
3236:
3233:
3231:
3228:
3226:
3223:
3221:
3218:
3216:
3213:
3212:
3210:
3208:
3204:
3201:
3197:
3187:
3184:
3182:
3179:
3177:
3174:
3172:
3169:
3167:
3164:
3162:
3159:
3157:
3154:
3152:
3149:
3147:
3144:
3142:
3139:
3138:
3136:
3132:
3126:
3123:
3121:
3118:
3116:
3113:
3111:
3108:
3106:
3103:
3101:
3098:
3096:
3093:
3091:
3088:
3086:
3083:
3081:
3078:
3077:
3075:
3071:
3065:
3062:
3060:
3057:
3056:
3054:
3050:
3047:
3043:
3038:
3028:
3025:
3023:
3020:
3018:
3015:
3014:
3012:
3010:Main articles
3008:
3004:Titan rockets
2999:
2994:
2992:
2987:
2985:
2980:
2979:
2976:
2970:
2967:
2965:
2962:
2959:
2956:
2954:
2952:
2951:Sutter Buttes
2948:
2944:
2940:
2935:
2932:
2929:
2926:
2922:
2919:
2916:
2915:
2911:
2906:
2903:
2902:1-56347-649-5
2899:
2895:
2893:
2892:1-55728-601-9
2889:
2885:
2881:
2878:
2874:
2870:
2867:
2865:
2861:
2857:
2853:
2850:
2846:
2843:
2842:
2838:
2821:
2817:
2811:
2808:
2795:
2791:
2785:
2782:
2778:
2777:
2776:Aviation Week
2770:
2767:
2751:
2744:
2741:
2738:
2734:
2728:
2725:
2712:
2706:
2703:
2690:
2685:
2681:
2675:
2672:
2666:
2663:
2657:
2654:
2648:
2645:
2632:
2626:
2624:
2620:
2616:
2615:1-55728-601-9
2612:
2606:
2603:
2596:
2593:
2587:
2584:
2578:
2575:
2569:
2566:
2560:
2557:
2551:
2548:
2542:
2539:
2533:
2530:
2524:
2521:
2515:
2512:
2506:
2503:
2497:
2495:
2491:
2485:
2482:
2476:
2473:
2467:
2464:
2458:
2455:
2451:
2450:0-517-56904-3
2447:
2441:
2438:
2434:
2433:
2432:Aviation Week
2426:
2423:
2417:
2414:
2408:
2405:
2392:
2388:
2382:
2379:
2367:
2361:
2358:
2350:
2343:
2340:
2335:
2328:
2325:
2319:
2316:
2310:
2307:
2302:
2295:
2289:
2286:
2281:
2275:
2272:
2267:
2266:ed-thelen.org
2263:
2256:
2253:
2248:
2244:
2238:
2236:
2232:
2227:
2221:
2202:
2195:
2189:
2187:
2183:
2170:
2166:
2159:
2156:
2150:
2147:
2143:
2142:1-56347-649-5
2139:
2133:
2130:
2124:
2121:
2117:
2116:0-517-56904-3
2113:
2107:
2104:
2098:
2095:
2089:
2086:
2080:
2077:
2074:
2070:
2064:
2061:
2055:
2052:
2046:
2043:
2037:
2034:
2028:
2026:
2022:
2016:
2013:
2007:
2004:
1991:
1987:
1980:
1977:
1974:
1973:1-55728-601-9
1970:
1964:
1961:
1945:
1939:
1936:
1933:
1932:1-55728-601-9
1929:
1923:
1921:
1919:
1915:
1909:
1906:
1900:
1897:
1894:
1893:1-55728-601-9
1890:
1884:
1881:
1875:
1872:
1860:
1853:
1850:
1844:
1842:
1838:
1832:
1829:
1826:
1821:
1818:
1812:
1810:
1808:
1804:
1798:
1796:
1792:
1786:
1784:
1780:
1767:
1763:
1756:
1753:
1747:
1745:
1741:
1737:
1736:0-19-505008-8
1733:
1727:
1724:
1718:
1715:
1709:
1707:
1703:
1697:
1694:
1687:
1684:
1678:
1675:
1669:
1666:
1660:
1657:
1651:
1648:
1642:
1639:
1633:
1630:
1617:
1611:
1608:
1602:
1599:
1593:
1591:
1587:
1581:
1578:
1572:
1569:
1563:
1560:
1553:
1549:
1546:
1544:
1541:
1539:
1536:
1534:
1531:
1530:
1526:
1524:
1522:
1514:
1512:
1506:
1503:
1500:
1497:
1494:
1491:
1488:
1482:
1477:
1474:
1470:
1467:
1464:
1461:
1458:
1455:
1451:
1448:
1443:
1439:
1434:
1429:
1426:
1423:
1420:
1416:
1413:
1409:
1406:
1403:
1399:
1395:
1392:
1389:
1385:
1382:
1379:
1376:
1372:
1368:
1364:
1361:
1358:
1354:
1350:
1346:
1343:
1340:
1337:
1334:
1330:
1329:
1328:
1321:
1314:
1305:
1300:
1293:
1288:
1281:
1276:
1274:
1272:
1267:
1265:
1261:
1256:
1252:
1250:
1249:Mira Loma AFS
1245:
1239:
1236:
1233:
1230:
1229:
1228:
1226:
1221:
1219:
1215:
1207:
1205:
1201:
1197:
1193:
1190:
1181:
1177:
1173:
1170:
1169:
1165:
1162:
1161:
1158:
1154:
1153:Ellsworth AFB
1151:
1150:
1146:
1143:
1142:
1139:
1135:
1132:
1131:
1127:
1124:
1123:
1120:
1116:
1113:
1112:
1108:
1105:
1104:
1101:
1097:
1094:
1093:
1089:
1086:
1085:
1082:
1078:
1075:
1074:
1070:
1067:
1066:
1060:
969:
962:
960:
956:
952:
948:
944:
940:
939:two squadrons
936:
932:
927:
926:liquid oxygen
924:
919:
912:
910:
908:
904:
900:
896:
892:
884:
880:
877:
873:
870:
866:
863:
860:
859:
858:
855:
853:
849:
845:
840:
837:
832:
828:
824:
816:
812:
809:
805:
802:
800:Length: 9.8 m
799:
796:
793:
790:
787:
784:
781:
778:
775:
774:
773:
772:
771:Second Stage:
766:
763:
759:
756:
753:
750:
747:
744:
741:
738:
735:
732:
729:
728:
727:
726:
719:
716:
713:
710:
707:
704:
701:
698:
695:
694:
690:
688:
686:
682:
678:
673:
671:
667:
663:
657:
640:
636:
632:
627:
623:
615:
613:
610:
606:
600:
596:
592:
588:
586:
582:
573:
569:
565:
561:
557:
553:
550:
545:
541:
537:
535:
531:
527:
523:
519:
515:
509:
503:
501:
499:
490:
488:
486:
482:
477:
476:liquid oxygen
472:
469:
465:
461:
452:
450:
448:
443:
441:
437:
431:
429:
425:
416:
414:
412:
408:
403:
401:
396:
393:
388:
386:
382:
378:
377:liquid oxygen
373:
369:
366:
362:
359:
348:
342:
339:
335:
332:
328:
324:
320:
316:
314:
310:
302:
298:
295:
291:
287:
282:
279:
275:
272:
268:
264:
260:
256:
254:
250:
246:
239:
235:
231:
228:
224:
220:
215:
211:
207:
203:
199:
195:
191:
187:
183:
179:
175:
171:
167:
163:
159:
154:
151:
148:
144:
140:
136:
131:
127:
123:
119:
115:
111:
107:
103:
99:
94:
90:
87:
83:
80:United States
79:
75:
72:
69:
65:
62:
59:
55:
51:
47:
39:
34:
19:
5171:
5152:
5135:Sky Scorcher
4953:
4765:
4636:Undesignated
3703:
3380:Upper stages
3199:Launch sites
3080:Titan II GLV
3058:
3017:Titan family
2936:
2848:
2824:. Retrieved
2820:the original
2810:
2798:. Retrieved
2794:the original
2784:
2774:
2769:
2757:. Retrieved
2743:
2727:
2715:. Retrieved
2705:
2693:. Retrieved
2680:Ghostarchive
2678:Archived at
2674:
2665:
2656:
2647:
2635:. Retrieved
2605:
2595:
2586:
2577:
2568:
2559:
2550:
2541:
2532:
2523:
2514:
2505:
2484:
2475:
2466:
2457:
2440:
2430:
2425:
2416:
2407:
2395:. Retrieved
2391:the original
2381:
2369:. Retrieved
2360:
2342:
2327:
2318:
2309:
2300:
2288:
2274:
2265:
2255:
2246:
2208:. Retrieved
2201:the original
2173:. Retrieved
2169:the original
2158:
2149:
2132:
2123:
2106:
2097:
2088:
2079:
2063:
2054:
2045:
2036:
2015:
2006:
1994:. Retrieved
1990:the original
1979:
1963:
1951:. Retrieved
1938:
1908:
1899:
1883:
1874:
1862:. Retrieved
1852:
1831:
1820:
1770:. Retrieved
1766:the original
1755:
1726:
1717:
1696:
1686:
1677:
1668:
1659:
1650:
1641:
1632:
1620:. Retrieved
1610:
1601:
1580:
1571:
1562:
1518:
1510:
1326:
1268:
1257:
1253:
1246:
1243:
1222:
1211:
1202:
1198:
1194:
1185:
1157:South Dakota
959:South Dakota
920:
916:
898:
888:
865:Friden, Inc.
856:
848:Seymour Cray
841:
820:
770:
769:
725:First Stage:
724:
723:
674:
658:
619:
601:
597:
593:
589:
578:
566:
562:
558:
554:
546:
542:
538:
510:
507:
494:
473:
456:
444:
432:
420:
404:
400:missile silo
389:
360:
355:
284:Second stage
212:5 March 1965
201:First flight
146:Launch sites
67:Manufacturer
5095:Alpha Draco
4917:Other types
4733:Senior Prom
3771:LGM-35 (II)
3329:Little Rock
3022:SM-68 Titan
2826:11 November
2800:11 November
2759:14 February
2717:14 February
2695:14 February
2637:11 November
2397:13 February
2371:11 February
2175:4 September
1996:11 November
1953:12 November
1772:11 November
1484:LR87 engine
1359:). Vertical
1218:Minuteman I
891:battleshort
797:Span: 2.3 m
751:Span: 3.1 m
447:SM-68 Titan
395:SM-65 Atlas
325:155 seconds
317:308 seconds
265:140 seconds
257:290 seconds
217:First stage
209:Last flight
185:Success(es)
91:1.5 million
5178:Categories
5120:Pye Wacket
5110:High Virgo
5100:Bold Orion
4819:1955–1962
4450:AGM-158A/B
3766:AQM-35 (I)
3342:Components
3250:Vandenberg
3181:Titan IIIM
3176:Titan IIIL
3105:Titan IIIE
3100:Titan IIID
3095:Titan IIIC
3090:Titan IIIB
3085:Titan IIIA
2839:References
1622:6 February
1554:References
1377:. Vertical
1208:Retirement
1176:California
1081:Washington
1077:Larson AFB
955:Washington
951:California
903:Thor-Agena
869:paper tape
662:Rocketdyne
585:California
365:multistage
330:Propellant
270:Propellant
193:Failure(s)
5153:See also:
4766:See also:
4678:Have Dash
4042:AGM-84H/K
3741:MGM-31A/B
3412:Transtage
3324:McConnell
3309:Ellsworth
3166:Titan IIS
3161:Titan IIL
3156:Titan IIB
3115:Titan 23G
3110:Titan 34D
2210:22 August
1762:"Titan I"
1172:Beale AFB
1134:Lowry AFB
1115:Lowry AFB
1051:851st SMS
1037:850th SMS
1023:725th SMS
1009:724th SMS
995:569th SMS
981:568th SMS
923:Cryogenic
895:fail-safe
874:"massive
871:equipment
485:Bell Labs
481:Atlas E/F
387:instead.
322:Burn time
294:LR91-AJ-3
262:Burn time
240:(430,000
227:LR87-AJ-3
5105:Cherokee
4541:AIM-174B
4455:AGM-158C
4192:BGM-109G
4089:"AIM-92"
3443:Orbus 21
3349:Boosters
3240:(S)LC-41
3235:(S)LC-40
3125:Titan IV
3052:Missiles
3027:Launches
2921:Archived
2879:, (2009)
2682:and the
2452:, p. 154
2262:"ATHENA"
2220:cite web
2144:, p. 380
1738:, p. xv.
1527:See also
1375:Nebraska
1260:Carnegie
1214:Titan II
1138:Colorado
1119:Colorado
935:Colorado
834:start a
639:oxidizer
109:Diameter
57:Function
5130:Skydart
4904:AIM-101
4743:Wagtail
4723:OpFires
4643:Aequare
4627:MIM-401
4622:AIM-260
4606:AGM-187
4601:MQM-186
4596:MQM-185
4591:RGM-184
4586:AGM-183
4581:LGM-182
4576:AGM-181
4571:AGM-180
4566:AGM-179
4561:MQM-178
4556:BQM-177
4551:AGM-176
4546:MQM-175
4537:RIM-174
4532:GQM-173
4527:FGM-172
4522:MQM-171
4517:MQM-170
4512:AGM-169
4507:MGM-168
4502:BQM-167
4497:MGM-166
4492:RGM-165
4487:MGM-164
4482:GQM-163
4477:RIM-162
4472:RIM-161
4467:ADM-160
4462:AGM-159
4445:MGM-157
4440:RIM-156
4435:BQM-155
4430:AGM-154
4425:AGM-153
4420:AIM-152
4415:FQM-151
4408:151–200
4399:PQM-150
4394:PQM-149
4389:FGM-148
4384:BQM-147
4379:MIM-146
4374:BQM-145
4369:ADM-144
4364:MQM-143
4359:AGM-142
4354:ADM-141
4349:MGM-140
4344:RUM-139
4339:CEM-138
4334:AGM-137
4329:AGM-136
4324:ASM-135
4319:MGM-134
4314:UGM-133
4309:AIM-132
4304:AGM-131
4299:AGM-130
4294:AGM-129
4289:AQM-128
4284:AQM-127
4279:BQM-126
4269:AGM-124
4264:AGM-123
4259:AGM-122
4249:AIM-120
4244:AGM-119
4239:LGM-118
4234:FQM-117
4229:RIM-116
4224:MIM-115
4219:AGM-114
4214:RIM-113
4209:AGM-112
4204:BQM-111
4199:BGM-110
4182:BQM-108
4177:MQM-107
4172:BQM-106
4167:MQM-105
4162:MIM-104
4157:AQM-103
4152:PQM-102
4147:RIM-101
4140:101–150
4131:LIM-100
4037:AGM-84E
3841:XLIM-49
3745:MGM-31C
3709:LGM-25C
3704:HGM-25A
3516:Thiokol
3506:Aerojet
3499:Engines
3438:Orbus 6
3421:Engines
3402:Star-37
3392:Centaur
3186:Titan V
3151:Titan-C
3134:Unbuilt
3045:Rockets
2855:IL,1996
2118:, p. 11
1864:16 June
1371:Ashland
808:Aerojet
762:Aerojet
666:Aerojet
651:⁄
514:Florida
417:History
289:Engines
222:Engines
141:Retired
50:Florida
31:Titan I
5125:Skokie
5115:Jaguar
5054:SRM-88
5049:GAM-87
5029:GAM-83
5009:GAM-79
4999:GAM-77
4974:GAM-72
4969:GAM-71
4949:GAM-67
4934:GAM-63
4888:GAR-11
4738:Sprint
4126:LIM-99
4121:YQM-98
4116:AIM-97
4111:UGM-96
4106:AIM-95
4101:YQM-94
4096:XQM-93
4084:FIM-92
4079:AQM-91
4074:BQM-90
4069:UGM-89
4064:AGM-88
4059:AGM-87
4054:AGM-86
4049:RIM-85
4027:AGM-83
4022:AIM-82
4017:AQM-81
4012:AGM-80
4007:AGM-79
4002:AGM-78
3997:FGM-77
3992:AGM-76
3987:BGM-75
3982:BQM-74
3977:UGM-73
3972:MIM-72
3967:BGM-71
3962:LEM-70
3957:AGM-69
3952:AIM-68
3947:RIM-67
3942:RIM-66
3937:AGM-65
3932:AGM-64
3927:AGM-63
3922:AGM-62
3917:MQM-61
3912:AQM-60
3907:RGM-59
3902:MQM-58
3897:MQM-57
3892:PQM-56
3887:RIM-55
3882:AIM-54
3877:AGM-53
3872:MGM-52
3867:MGM-51
3860:51–100
3851:RIM-50
3846:LIM-49
3836:AGM-48
3831:AIM-47
3826:MIM-46
3821:AGM-45
3816:UUM-44
3811:FIM-43
3806:MQM-42
3801:AQM-41
3796:MQM-40
3791:MQM-39
3786:AQM-38
3781:AQM-37
3776:MQM-36
3761:AQM-34
3756:MQM-33
3751:MGM-32
3736:LGM-30
3731:MGM-29
3726:AGM-28
3721:UGM-27
3716:AIM-26
3699:RIM-24
3694:MIM-23
3689:AGM-22
3684:MGM-21
3679:ADM-20
3674:PGM-19
3669:MGM-18
3664:PGM-17
3659:CGM-16
3654:RGM-15
3649:MIM-14
3639:AGM-12
3634:PGM-11
3629:CIM-10
3485:Martin
3478:Rocket
3433:B-8096
3366:UA1207
3361:UA1206
3356:UA1205
3294:Larson
3268:LC-395
3171:Soltan
2904:, 2006
2900:
2890:
2875:
2862:
2735:
2613:
2448:
2140:
2114:
2071:
1971:
1930:
1891:
1734:
1189:ATHENA
957:, and
943:Denver
937:(with
823:UNIVAC
811:LR91-3
765:LR87-3
532:, and
468:RASCAL
464:Navaho
372:SM-68A
300:Thrust
236:1,900
233:Thrust
138:Status
125:Stages
101:Height
5079:IM-99
5074:RM-92
5069:RM-91
5064:RM-90
5059:RM-89
5044:RM-86
5039:RM-85
5034:RM-84
5024:RM-82
5019:RM-81
5014:SM-80
5004:SM-78
4994:TM-76
4989:SM-75
4984:SM-74
4979:SM-73
4964:IM-70
4959:IM-69
4954:SM-68
4944:SM-65
4939:SM-64
4929:SM-62
4924:TM-61
4883:GAR-9
4878:GAR-8
4873:GAR-6
4868:GAR-5
4863:GAR-4
4858:GAR-3
4853:GAR-2
4848:GAR-1
4753:GLSDB
4713:NCADE
4703:MA-31
4653:Brazo
4648:ASALM
3624:AIM-9
3619:RIM-8
3612:RIM-7
3607:AIM-7
3602:RGM-6
3597:MGM-5
3592:AIM-4
3587:MIM-3
3582:RIM-2
3577:MGM-1
3453:LR-91
3448:LR-87
3428:AJ-10
3387:Agena
3314:Lowry
3304:Beale
3287:Bases
3278:SLC-6
3273:SLC-4
3230:LC-20
3225:LC-19
3220:LC-16
3215:LC-15
2753:(PDF)
2352:(PDF)
2297:(PDF)
2204:(PDF)
2197:(PDF)
1947:(PDF)
1182:Silos
1100:Idaho
947:Idaho
889:The "
685:mylar
460:Snark
440:Atlas
345:[
166:LC-20
162:LC-19
158:LC-16
153:LC-15
44:from
4843:MB-1
4728:PrSM
4718:NLOS
4708:MSDM
4698:LRHW
4693:LREW
4673:HACM
4668:HALO
4615:201–
3570:1–50
3458:RL10
3371:SRMU
3263:SLTF
3258:OSTF
3141:Ares
2945:and
2898:ISBN
2888:ISBN
2883:2012
2873:ISBN
2860:ISBN
2828:2019
2802:2019
2761:2016
2733:ISBN
2719:2016
2697:2016
2639:2019
2611:ISBN
2600:2012
2446:ISBN
2399:2015
2373:2016
2226:link
2212:2013
2177:2011
2138:ISBN
2112:ISBN
2069:ISBN
1998:2019
1969:ISBN
1955:2022
1928:ISBN
1889:ISBN
1866:2018
1774:2019
1732:ISBN
1624:2016
1353:I-75
899:e.g.
821:The
670:LR87
631:RP-1
534:LC20
530:LC19
526:LC16
522:LC15
466:and
381:RP-1
379:and
356:The
334:RP-1
274:RP-1
117:Mass
96:Size
61:ICBM
4688:KEI
4683:JSM
4663:GBI
3407:TOS
3397:IUS
1440:in
1400:in
945:),
850:at
635:LOX
516:at
338:LOX
278:LOX
5180::
2941:;
2686::
2622:^
2493:^
2299:.
2264:.
2245:.
2234:^
2222:}}
2218:{{
2185:^
2024:^
1917:^
1840:^
1806:^
1794:^
1782:^
1743:^
1705:^
1691:97
1589:^
1373:,
1369:,
1174:,
1155:,
1136:,
1117:,
1098:,
1079:,
953:,
949:,
583:,
536:.
528:,
524:,
462:,
292:1
242:lb
238:kN
225:1
164:,
160:,
89:$
48:,
4812:e
4805:t
4798:v
4539:/
3747:)
3743:(
3554:e
3547:t
3540:v
2997:e
2990:t
2983:v
2953:)
2949:(
2830:.
2804:.
2763:.
2721:.
2699:.
2641:.
2401:.
2375:.
2354:.
2336:.
2282:.
2228:)
2214:.
2179:.
2000:.
1957:.
1868:.
1776:.
1626:.
1444:.
653:2
649:1
646:+
644:7
629:(
349:]
336:/
307:)
305:f
276:/
247:)
244:f
155:,
128:2
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.