Knowledge (XXG)

Supersonic transport

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1084:. The speed limit of rail transport had been pushed so hard to enable it to effectively compete with road and air transport. But this achievement was not done for different rail operating companies to compete among themselves. This phenomenon also reduces the airline desirability of SSTs, because, for very long-distance transportation (a couple of thousand kilometers), competition between different modes of transport is rather like a single-horse race: air transport does not have a significant competitor. The only competition is between the airline companies, and they would rather pay moderately to reduce cost and increase service quality than pay much more for a speed increase. Also, for-profit companies generally prefer low risk business plans with high probabilities of appreciable profit, but an expensive leading-edge technological research and development program is a high-risk enterprise, as it is possible that the program will fail for unforeseeable technical reasons or will meet cost overruns so great as to force the company, due to financial resource limits, to abandon the effort before it yields any marketable SST technology, causing potentially all investment to be lost. 1068:
competitive advantage, even to the extent that many customers will willingly pay higher fares for the benefit of saving time and/or arriving sooner. However, Concorde's high noise levels around airports, time zone issues, and insufficient speed meant that only a single return trip could be made per day, so the extra speed was not an advantage to the airline other than as a selling feature to its customers. The proposed American SSTs were intended to fly at Mach 3, partly for this reason. However, allowing for acceleration and deceleration time, a trans-Atlantic trip on a Mach 3 SST would be less than three times as fast as a Mach 1 trip.
1050: 1285: 537: 1270: 1850: 1188: 604: 661:. The efficiency curve of the fan design means that the amount of bypass that maximizes overall engine efficiency is a function of forward speed, which decreases from propellers, to fans, to no bypass at all as speed increases. Additionally, the large frontal area taken up by the low-pressure fan at the front of the engine increases drag, especially at supersonic speeds, and means the bypass ratios are much more limited than on subsonic aircraft. 78: 796:, where the specific thrust (and therefore jet velocity and noise) is low at take-off, but is forced high during supersonic cruise. Transition between the two modes would occur at some point during the climb and back again during the descent (to minimize jet noise upon approach). The difficulty is devising a variable cycle engine configuration that meets the requirement for a low cross-sectional area during supersonic cruise. 1310: 202: 4259: 1235: 261:, stated to various magazines that an SST constructed of steel weighing 250,000 pounds (110,000 kg) could be developed for $ 160 million and in production lots of 200 or more sold for around $ 9 million. But it was the Anglo-French development of the Concorde that set off panic in the US industry, where it was thought that Concorde would soon replace all other long range designs, especially after 533:), to the square of the airspeed and to the air density. Since drag rises rapidly with speed, a key priority of supersonic aircraft design is to minimize this force by lowering the coefficient of drag. This gives rise to the highly streamlined shapes of SSTs. To some extent, supersonic aircraft also manage drag by flying at higher altitudes than subsonic aircraft, where the air density is lower. 4503: 2924: 993: 1993: 556:). Around Mach 1, the peak coefficient of drag is four times that of subsonic drag. Above the transonic range, the coefficient drops drastically again, although remains 20% higher by Mach 2.5 than at subsonic speeds. Supersonic aircraft must have considerably more power than subsonic aircraft require to overcome this wave drag, and although cruising performance above 36: 2932: 649:, it would have been much more competitive, though the 707 and DC-8 still carried more passengers. When these high bypass jet engines reached commercial service in the 1960s, subsonic jet engines immediately became much more efficient, closer to the efficiency of turbojets at supersonic speeds. One major advantage of the SST disappeared. 378:, and others, suggest that the drop in ozone would be at most, "no more" than 1 to 2% if a fleet of 500 supersonic aircraft operated. Fahey expressed that this would not be a fatal obstacle for an advanced SST development – while "a big caution flag... should not be a showstopper for advanced SST development" because "removing the 101: 2901: 1209:(registration N9604Z) exceeded Mach 1 in a controlled dive during a test flight at Edwards Air Force Base. The crew were William Magruder (pilot), Paul Patten (copilot), Joseph Tomich (flight engineer), and Richard H. Edwards (flight test engineer). This is the first supersonic flight by a civilian airliner. 1698:
Design goals are a 4,200–5,300 nmi (7,800–9,800 km) range and a 9,500–10,500 ft (2,900–3,200 m) takeoff field length, a 75-80 PLdB sonic boom and a cruise of Mach 1.6–1.7 over land and Mach 1.7-1.8 over water. Twin tail-mounted nonafterburning 40,000 lbf (180 kN) engines
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in Moscow a scale model of its Supersonic Business Jet / Commercial Jet which should produce a low sonic boom permitting supersonic flight over land, optimised for 2,100 km/h (1,300 mph) cruise and 7,400–8,600 km (4,600–5,300 mi) range. The scientific research aims to optimise for
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In total, 20 Concordes were built: two prototypes, two development aircraft and 16 production aircraft. Of the sixteen production aircraft, two did not enter commercial service and eight remained in service as of April 2003. All but two of these aircraft are preserved; the two that are not are F-BVFD
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Supersonic aircraft have higher per-passenger fuel consumption than subsonic aircraft; this makes the ticket price necessarily higher, all other factors being equal, as well as making that price more sensitive to the price of oil. (It also makes supersonic flights less friendly to the environment and
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If the intensity of the boom can be reduced, then this may make even very large designs of supersonic aircraft acceptable for overland flight. Research suggests that changes to the nose cone and tail can reduce the intensity of the sonic boom below that needed to cause complaints. During the original
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For example, the early Tu-144S was fitted with a low bypass turbofan engine which was much less efficient than Concorde's turbojets in supersonic flight. The later TU-144D featured turbojet engines with comparable efficiency. These limitations meant that SST designs were not able to take advantage of
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transports using wings), would use a very large amount of propellant and operate best at speeds between about Mach 8 and orbital speeds. Rockets compete best with air-breathing jet engines on cost at very long range; however, even for antipodal travel, costs would be only somewhat lower than orbital
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is a self-funded twinjet design aiming to cruise at Mach 1.6 over water for 6,200 nmi (11,500 km; 7,100 mi) with 22 passengers in a windowless cabin, with unspecified 20,000 lbf (89 kN) engines. A SX-1.2-scale model should have made its maiden flight in September 2017 before
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revealed that it is in the development phases of building a 40-passenger supersonic jet capable of flying Mach 1.7, claiming that the design simulation shows that it will be quieter and 30% more efficient than the Concorde and will be able to fly Los Angeles to Sydney in 6 hours. It is planned to go
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Concorde only sold to British Airways and Air France, with subsidized purchases that were to return 80% of the profits to the government. In practice for almost all of the length of the arrangement, there was no profit to be shared. After Concorde was privatized, cost reduction measures (notably the
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rates of the aircraft, at least on medium and long-range flights where the aircraft spends a considerable amount of time in cruise. SST designs flying at least three times as fast as existing subsonic transports were possible, and would thus be able to replace as many as three planes in service, and
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was founded with the goal of developing a 70-passenger supersonic jet capable of flying Mach 1.8 and with a range of 5,000 nmi (9,300 km; 5,800 mi). The company aims to introduce the jet commercially in the 2030s. In April 2021, Exosonic was awarded a contract to develop a supersonic
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Since SSTs produce sonic booms at supersonic speeds they are rarely permitted to fly supersonic over land, and must fly supersonic over sea instead. Since they are inefficient at subsonic speeds compared to subsonic aircraft, range is deteriorated and the number of routes that the aircraft can fly
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Airlines potentially value very fast aircraft, because it enables the aircraft to make more flights per day, providing a higher return on investment. Also, passengers generally prefer faster, shorter-duration trips to slower, longer-duration trips, so operating faster aircraft can give an airline a
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Nevertheless, fuel costs are not the bulk of the price for most subsonic aircraft passenger tickets. For the transatlantic business market that SST aircraft were utilized for, Concorde was actually very successful, and was able to sustain a higher ticket price. Now that commercial SST aircraft have
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Along with shifting political considerations, the flying public continued to show interest in high-speed ocean crossings. This started additional design studies in the US, under the name "AST" (Advanced Supersonic Transport). Lockheed's SCV was a new design for this category, while Boeing continued
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of explosive energy being released in 1962, so therefore the equivalent amount of NOx from "1047" Concordes flying "10 hours a day", would likewise, not be unprecedented. In 1981 models and observations were still irreconcilable. More recent computer models in 1995 by David W. Fahey, an atmospheric
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was proposed as a 12-seat trijet, with a range of 4,750 nmi (8,800 km; 5,470 mi) at Mach 1.4 over water or 5,300 nmi (9,800 km; 6,100 mi) at Mach 0.95 over land, although "boomless" Mach 1.1 flight was claimed to be possible. Backed by Airbus and with 20 launch orders
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Investing in research and development work to design a new SST can be considered as an effort to push the speed limit of air transport. Generally, other than an urge for new technological achievement, the major driving force for such an effort is competitive pressure from other modes of transport.
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The aerodynamic design of a supersonic aircraft needs to change with its speed for optimal performance. Thus, an SST would ideally change shape during flight to maintain optimal performance at both subsonic and supersonic speeds. Such a design would introduce complexity which increases maintenance
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Higher fuel costs and lower passenger capacities due to the aerodynamic requirement for a narrow fuselage make SSTs an expensive form of commercial civil transportation compared with subsonic aircraft. For example, the Boeing 747 can carry more than three times as many passengers as Concorde while
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third-scale testbed should fly in 2018 as the powerplant is selected for a 45/55-seat trijet airliner reaching Mach 2.2 over water for 9,000 nmi (17,000 km; 10,000 mi) with one stop for a business-class fare. Aiming for 2023 deliveries, it received 10 commitments from Virgin and 15
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of subsonic aircraft. This implies that for any given required amount of lift, the aircraft will have to supply about twice the thrust, leading to considerably greater fuel use. This effect is pronounced at speeds close to the speed of sound, as the aircraft is using twice the thrust to travel at
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Subsonic aircraft are usually made of aluminium. However aluminium, while being light and strong, is not able to withstand temperatures much over 127 °C; above 127 °C the aluminium gradually loses its properties that were brought about by age hardening. For aircraft that fly at Mach 3,
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While conventional turbo and ramjet engines are able to remain reasonably efficient up to Mach 5.5, some ideas for very high-speed flight above Mach 6 are also sometimes discussed, with the aim of reducing travel times down to one or two hours anywhere in the world. These vehicle proposals very
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The high per-passenger takeoff weight makes it difficult to obtain a good fuel fraction. This issue, along with the challenge presented by supersonic lift/drag ratios, greatly limits the range of supersonic transports. Because long-distance routes were not a viable option, airlines had little
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The annoyance of a sonic boom can be avoided by waiting until the aircraft is at high altitude over water before reaching supersonic speeds; this was the technique used by Concorde. However, it precludes supersonic flight over populated areas. Supersonic aircraft have poor lift/drag ratios at
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Extreme jet velocities used during take-off caused Concorde and Tu-144s to produce significant take-off noise. Communities near the airport were affected by high engine noise levels, which prompted some regulators to disfavor the practice. SST engines need a fairly high specific thrust (net
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are much stronger for their weight (important to deal with stresses) as well as being more rigid. As per-seat weight of the structure is much higher in an SST design, structural improvements would have led to a greater proportional improvement than the same changes in a subsonic aircraft.
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Competition between different service providers within a mode of transport does not typically lead to such technological investments to increase the speed. Instead, the service providers prefer to compete in service quality and cost. An example of this phenomenon is
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Since Concorde stopped flying, it has been revealed that over the life of Concorde, the plane did prove profitable, at least to British Airways. Concorde operating costs over nearly 28 years of operation were approximately £1 billion, with revenues of £1.75 billion.
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When it comes to public policy, for example, the FAA prohibits commercial airplanes from flying at supersonic speeds above sovereign land governed by the United States because of the negative impact the sonic boom brings to humans and animal populations below.
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during flight), high development costs, expensive construction materials, high fuel consumption, extremely high emissions, and an increased cost per seat over subsonic airliners. However, despite these challenges, Concorde claimed it operated profitably.
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warned that a fleet of 500 SSTs flying at 65,000 ft (20 km) for a period of years could raise stratospheric water content by as much as 50% to 100%. According to Train, this could lead to greater ground-level heat and hamper the formation of
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aircraft was flown which proved the soundness of the design and demonstrated the capability of reducing the boom by about half. Even lengthening the vehicle (without significantly increasing the weight) would seem to reduce the boom intensity (see
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to a greater differential than subsonic aircraft, which do not operate at the high altitudes necessary for supersonic flight. These factors together meant that the empty weight per seat of Concorde is more than three times that of a Boeing 747.
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Turbofan engines improve efficiency by increasing the amount of cold low-pressure air they accelerate, using some of the energy normally used to accelerate hot air in the classic non-bypass turbojet. The ultimate expression of this design is the
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designs, to produce an even more advanced, larger, faster and longer ranged design. The Boeing 2707 design was eventually selected for continued work, with design goals of ferrying around 300 passengers and having a cruising speed near to
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of about 4) at slow speed, but it travelled at high speed for most of the flight. Designers of Concorde spent 5000 hours optimizing the vehicle shape in wind tunnel tests to maximize the overall performance over the entire flightplan.
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are jet engines with a heat exchanger at the inlet that cools the air at very high speeds. These engines may be practical and efficient at up to about Mach 5.5, and this is an area of research in Europe and Japan. The British company
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2018 conference a Mach 6 (6,500 km/h; 3,500 kn) passenger airliner. Crossing the Atlantic in 2 hours or the Pacific in 3 at 100,000 ft (30 km) would enable same-day return flights, increasing airlines' asset
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Another problem was that the wide range of speeds over which an SST operates makes it difficult to improve engines. While subsonic engines had made great strides in increased efficiency through the 1960s with the introduction of the
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A total of sixteen airworthy Tupolev Tu-144s were built; a seventeenth Tu-144 (reg. 77116) was never completed. There was also at least one ground test airframe for static testing in parallel with the prototype 68001 development.
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In the early 1960s, various executives of US aerospace companies were telling the US public and Congress that there were no technical reasons an SST could not be produced. In April 1960, Burt C Monesmith, a vice president with
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has an L/D ratio of 17). Because an aircraft's design must provide enough lift to overcome its own weight, a reduction of its L/D ratio at supersonic speeds requires additional thrust to maintain its airspeed and altitude.
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was the first SST to enter service and the first to leave it. Only 55 passenger flights were carried out before service ended due to safety concerns. A small number of cargo and test flights were also carried out after its
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Despite the model-observation discrepancy surrounding the ozone concern, in the mid-1970s, six years after its first supersonic test flight, Concorde was now ready for service. The US political outcry was so high that
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is greater at higher speeds. Because their speed over the ground is greater, this decrease in efficiency is less than proportional to speed until well above Mach 2, and the consumption per unit distance is lower.
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In practice all supersonic transports have used essentially the same shape for subsonic and supersonic flight, and a compromise in performance is chosen, often to the detriment of low speed flight. For example,
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SST efforts in the 1960s, it was suggested that careful shaping of the fuselage of the aircraft could reduce the intensity of the sonic boom's shock waves that reach the ground. One design caused the
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By this time, the economics of past SST concepts were no longer reasonable. When first designed, the SSTs were envisioned to compete with long-range aircraft seating 80 to 100 passengers such as the
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convention in Las Vegas, with NASA supporting only research, various companies faced engineering challenges to propose aircraft with no engine available, variable top speeds and operating models:
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that included Mach 1.6 double-ogee wing and Mach 1.2 delta-wing with separate tail and four under-wing engine configurations. Avro's team moved to the UK where its design formed the basis of
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The desire for a second-generation supersonic aircraft has remained within some elements of the aviation industry, and several concepts have emerged since the retirement of Concorde.
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closing of the metallurgical wing testing site which had done enough temperature cycles to validate the aircraft through to 2010) and ticket price raises led to substantial profits.
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by early 2019. The FAA should make a proposition for landing-and-takeoff noise before March 31, 2020, for a rule after 2022; and for overland sonic boom from the end of 2020, while
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the dramatic improvements in fuel economy that high bypass engines brought to the subsonic market, but they were already more efficient than their subsonic turbofan counterparts.
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banned the plane. This threatened the aircraft's economic prospects — it had been built with the London–New York route in mind. The plane was allowed into Washington, D.C. (at
1418:. NASA should fly a low-boom demonstrator in 2019, reduced from double bangs to soft thumps by airframe shaping, to inquire community response, in support of a prospective 1096:(ICCT) estimates a SST would burn 5 to 7 times as much fuel per passenger. The ICCT shows that a New York to London supersonic flight would consume more than twice as much 162:
Supersonic airliners have been the objects of numerous recent ongoing design studies. Drawbacks and design challenges are excessive noise generation (at takeoff and due to
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In April 2024, Boom received FAA licensure for Mach 1 and beyond tests of its XB-1 to be conducted at the Black Mountain Supersonic Corridor, in Mojave, California.
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If there were 2,000 SSTs in 2035, there would be 5,000 flights per day at 160 airports and the SST fleet would emit ~96 million metric tons of CO₂ per year (like
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Throughout the 1950s an SST looked possible from a technical standpoint, but it was not clear if it could be made economically viable. Because of differences in
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planned noise standards for supersonic transports, giving developers a regulatory certainty for their designs, mostly their engine choice. Rules for supersonic
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to give higher efficiency at low speeds, but the increased space required for such a feature produced capacity problems that proved ultimately insurmountable.
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was selected in May 2017 for a joint engine study. In May 2021 the company announced that they would be ceasing operations due to inability to raise capital.
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would be heard in Canada, Germany, Iraq, Ireland, Israel, Romania, Turkey, and parts of the United States, up to 150–200 per day or one every five minutes.
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Following the permanent cessation of flying by Concorde, there are no remaining SSTs in commercial service. However, several companies have each proposed a
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problems, which require heavier structures to minimize unwanted flexing. SSTs also require a much stronger (and therefore heavier) structure because their
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was not thought to be a serious issue due to the high altitudes at which the planes flew, but experiments in the mid-1960s such as the controversial
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of 1.94 lb/sq ft (93 Pa) (133 dBA SPL). Overpressures over 1.5 lb/sq ft (72 Pa) (131 dBA SPL) often cause complaints.
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concept, cruising at Mach 4 (4,400 km/h; 2,400 kn) at 105,000 ft (32,000 m) and attracting Japanese interest. The German
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X-plane will mimic the shockwave signature of a Mach 1.6 to 1.8, 80- to 100-seat airliner for 75 PNLdB compared with 105 PNLdB for Concorde.
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exposed area around airports could double compared to existing subsonic aircraft of the same size, with more than 300 operations per day at
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drag. Unfortunately this implies a high jet velocity, which makes the engines noisy, particularly at low speeds/altitudes and at take-off.
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effect is reduced as the aircraft accelerates to higher speeds. Offsetting this increase in fuel use was the potential to greatly increase
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Supersonic vehicle speeds demand narrower wing and fuselage designs, and are subject to greater stresses and temperatures. This leads to
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to interfere with each other, greatly reducing the sonic boom. This was difficult to test at the time, but the increasing power of
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are employed), and hence burn more fuel, which results in their use being economically disadvantageous on such flight paths.
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to serve as a guide and means of comparison, observing that no detectable ozone loss was evident from approximately 213
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Yi Zeng; Dini Wang; Xiang Xiong; Xun Zhang; Philip J. Withers; Wei Sun; Matthew Smith; Mingwen Bai; Ping Xiao (2017).
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combined in 2017), 1.6 to 2.4 gigatonnes of CO₂ over their 25-year lifetime: one-fifth of the international aviation
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design shifts significantly between supersonic and subsonic aircraft. Jet engines, as a class, can supply increased
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crashed shortly after take-off with all 109 occupants and four on ground killed; the only fatal incident involving
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to allow supersonic flight over land. In 2016, NASA announced it had signed a contract for the design of a modern
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took out purchase options on the Concorde. Congress was soon funding an SST design effort, selecting the existing
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supersonic business jet. In late 2010, the project continued with a testbed flight of a section of the wing. The
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NASA is working with 2 teams led by Boeing and Northrop Grumman on developing concepts for a Mach 4 airliner.
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that is to cruise at Mach 1.6, and is to create a sonic boom only 1% as strong as that generated by Concorde.
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for sustained supersonic cruise. At about Mach 2, a typical wing design will cut its L/D ratio in half (e.g.,
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carrying four times that, the speed and fuel advantages of the SST concept were taken away by sheer size.
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were entering service. In Britain and France, government-subsidized SST programs quickly settled on the
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300-passenger airliner capable to fly at about 10,000 km/h (Mach 8) above 30 km of altitude.
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have also been proposed. There are many difficulties with such flight, both technical and economic.
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outside Paris on July 25, 2000, killing 100 passengers, 9 crew members, and 4 people on the ground.
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stopped flying, it has become clearer that Concorde made substantial profit for British Airways.
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thrust/airflow) during supersonic cruise, to minimize engine cross-sectional area and, thereby,
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of the " would essentially eliminate the hypothesized 1%–2% ozone-destruction-reaction-pathway.
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10%, with Susan Solomon of NOAA calculating that it is this change which is responsible for the
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is a suborbital hypersonic winged passenger spaceplane project under preliminary development.
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Serious work on SST designs started in the mid-1950s, when the first generation of supersonic
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non-stop is reduced. This also reduces the desirability of such aircraft for most airlines.
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compresses the air in front of it. The increased temperature of the air heats the aircraft.
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from an undisclosed European airline in 2016, totalling 76 from five airlines by June 2017;
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and all overland commercial supersonic flight was banned over the US. Presidential advisor
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https://www.nasa.gov/sites/default/files/atoms/files/supersonic-flight-recommendations.pdf
1998: 1918: 1723: 1625: 1396: 1384: 1373: 1273: 1252:. Please help update this article to reflect recent events or newly available information. 1148: 1120: 1081: 923: 607: 592: 320: 266: 242: 1811:, which examined a design for a hydrogen-fueled plane carrying 300 passengers called the 1195:
in Germany is the only location where both Concorde and the Tu-144 are displayed together
626: 3038: 2727: 4473: 4391: 4346: 4144: 4101: 4026: 3993: 3650:"Swiss Hypersonic Startup Destinus Appears Destined For Same Path As U.S. Counterparts" 3138: 2746: 2711: 1958: 1950: 1902: 1833: 1783: 1637: 1610: 1525: 1380: 1288:
Boeing concept presented to NASA Aeronautics Research Mission Directorate in April 2010
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Later, an additional threat to the ozone was hypothesized as a result of the exhaust's
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a manned testbed in 2019 and the prototype in 2021, with market availability for 2023.
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sustainability, two growing concerns of the general public, including air travelers.)
201: 4525: 4173: 4091: 3905: 3108:"Aerion Supersonic shuts down, ending plans to build silent high speed business jets" 1775: 1704: 1505: 1438: 1297: 1128: 1105: 479: 689:
Concorde and the TU-144 were both constructed of conventional aluminum: Concorde of
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generation, aircraft operating at supersonic speeds have approximately one-half the
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between 2,000 and 7,000 miles (3,200 and 11,300 km), including 72 million in
148:. Concorde's last commercial flight was in October 2003, with a November 26, 2003 3899:. The trials and tribulations of trying to resurrect supersonic passenger travel. 3795: 2925:"Partnership gears up for Concorde sequel; British, French firms sign plane pact" 2498: 1403:
For its economic viability, NASA research since 2006 has focused on reducing the
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1/10-scale model of a McDonnell Douglas Mach 2.2 transport in 1992, part of NASA
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A Technique for Integrating Engine Cycle and Aircraft Configuration Optimization
2011: 1942: 1906: 1700: 1687:(XVS). The 225 ft (69 m) long design is significantly longer than the 1660: 1633: 1618: 1482: 1447: 1362: 1309: 957: 885: 839: 634: 553: 295: 275: 270: 234: 2456: 2031: 4376: 4351: 4129: 4124: 3839: 3084:"More details emerge on the $ 80 million Aerion Supersonic Business Jet." 2597: 1988: 1970: 1874: 1791: 1727: 1699:
are located between V-tails. Integrated low-noise propulsion include advanced
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subsonic speeds as compared to subsonic aircraft (unless technologies such as
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speed is more efficient, it is still less efficient than flying subsonically.
419: 415: 291: 214: 163: 89: 2850:"Noise and climate impacts of an unconstrained commercial supersonic network" 2535: 956:
coating material was discovered which could resist temperatures occurring at
657:, where almost all of the jet thrust is used to power a very large fan – the 4421: 4236: 3701: 3484: 2521: 2330: 2305: 2249:"Nitrogen Oxides, Nuclear Weapon Testing, Concorde and Stratospheric Ozone. 1886: 1708: 1606: 1602: 1443: 1411: 1361:
from Flexjet, first deliveries were pushed back from 2023 by two years when
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on the underside of the aircraft. This improved the L/D ratio by about 30%.
694: 658: 654: 557: 549: 545: 370: 3718:"A passenger aircraft that flies around the world at Mach 9? Sure, why not" 3066:"Orders for Aerion's Concorde executive jet are more than $ 3 billion" 2755: 478:, and a third which had taken off from Heathrow on a loop flight over the 35: 3697:"Venus Aerospace unveils its new dart-like Mach 9 hypersonic plane design" 4465: 4425: 4371: 4361: 4328: 4021: 3633: 3012: 2481: 1978: 1962: 1910: 1870: 1839: 1760: 1715: 1688: 1550: 1109: 1053: 935: 873: 678: 638: 610: 572: 460: 427: 400: 137: 82: 4273: 3500:"Is a Mach 4 Passenger Jet Possible? NASA, Industry Explore Idea – NASA" 3480:"Virgin Galactic unveils Mach 3 design for supersonic passenger flights" 2736: 1969:
a higher risk. Mach 6 was chosen as the limit achievable with available
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has a 73 ft (22 m) span, slightly narrower than the Concorde.
4193: 3951: 3883: 3414: 3157:"This Aerospace Company Wants to Bring Supersonic Civilian Travel Back" 1946: 1926: 1843: 1679:
design; integrated low-noise propulsion; swept-wing supersonic natural
953: 950: 786: 618: 3930: 3872:"Supersonic jets can fly from New York to L.A. in 2.5 hours (or less)" 3761:"Hypersonic airliner "may not be as hard as people think": Boeing CTO" 3271: 1621:
projects 13 million would be interested in supersonic transport then.
4430: 4076: 3858: 2797:"Environmental performance of emerging supersonic transport aircraft" 2795:
Kharina, Anastasia; MacDonald, Tim; Rutherford, Dan (July 17, 2018).
2310:. AAAS Sy~posium, Toronto, January 1981 – via escholarship.org. 2267: 2124:. (Spokane, Washington). Associated Press. March 26, 1971. p. 1. 1938: 1934: 1914: 1857: 1807: 1805:, with 50% EU money, has been engaged in a research programme called 1756: 1349: 1326: 931: 702: 621:, England shows the slender fuselage necessary for supersonic flight. 323:
levels in the 1980s and 1990s were higher than that in the 2000s, by
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at slower speeds, and avoiding afterburners on takeoff would reduce
1846:, and Venus Aerospace are developing hypersonic passenger aircraft. 1667:, a Mach 1.8, transpacific airliner concept for 40 passenger. Lower 1446:
and Mach 1.5–2.0 supersonic speeds, a similar design is tested in a
1021:. Statements consisting only of original research should be removed. 544:
As speeds approach the speed of sound, the additional phenomenon of
3676:"Why a Mach 5 passenger plane is a crazy idea that might just work" 3523:"Boom's XB-1 test plane gets FAA green light for supersonic flight" 2812:"NBAA: Supersonic flight may be feasible – but can Earth stand it?" 2118:"Boeing will lay off 7,000 workers with disbandment of SST program" 1659:
In June 2019, inspired by the NASA quiet supersonic initiative and
298:. Both problems impacted the thinking of lawmakers, and eventually 3941:"U.S. and Europe clash over global supersonic jet noise standards" 1848: 1829: 1726:
with Rolls-Royce unveiled the concept of a Mach 3 capable twinjet
1434: 1308: 1283: 1268: 1186: 1048: 939: 602: 535: 312: 200: 100: 99: 86: 76: 2902:"French transport chief speculates about new-generation Concorde" 3389: 2354:"24 Will commercial supersonic aircraft damage the ozone layer?" 1770:
Rocket-engined vehicles, while technically practical (either as
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Qualitative variation in Cd factor with Mach number for aircraft
145: 4277: 3955: 3838:. National Aeronautics and Space Administration. Archived from 1965:. Cruising at 90,000–100,000 feet (27,000–30,000 m) makes 1941:, and a bypass duct around the turbine engine to a combination 3680: 3441:"Exclusive look at designs for US supersonic presidential jet" 3212:"NASA Begins Work to Build a Quieter Supersonic Passenger Jet" 2848:
Dan Rutherford; Brandon Graver; Chen Chen (January 30, 2019).
2197:""Environment: SST: Boon or Boom-Doggie?", Time, June 1, 1970" 1917:
at Mach 6 would avoid the need for a scramjet, similar to the
1641: 1629: 1419: 1228: 986: 355: 238: 29: 253:
eventually merged their efforts in 1962 to produce Concorde.
2983:
https://www.nasa.gov/langley/100/designing-a-plane-for-speed
2947:"Potential Mach 2.2 Airliner Market Pegged At $ 260 Billion" 132:
designed to transport passengers at speeds greater than the
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Corporation had $ 3 billion of pre-order sales on its
968:
The range of supersonic aircraft can be estimated with the
3336:"Noise Standards One Key To Comeback Of Supersonic Flight" 278:. The Soviet Union set out to produce its own design, the 198:
thereby lower costs in terms of manpower and maintenance.
136:. To date, the only SSTs to see regular service have been 2215:"Stratospheric Water Vapor is a Global Warming Wild Card" 548:
appears. This is a powerful form of drag that begins at
2142:. (Oregon). Associated Press. March 25, 1971. p. 1. 2106:. (Oregon). Associated Press. March 24, 1971. p. 1. 2054:
Cold War Tech War: The Politics of America's Air Defense
346:, a threat that was, in 1974, seemingly validated by an 3906:"Review and prospect of supersonic business jet design" 3829:"Fundamental Aeronautics Program – Supersonics Project" 3549:"Paris: EADS details near-hypersonic transport concept" 1905:. The Boeing hypersonic airliner would be powered by a 1010: 294:
and the potential for its engine exhaust to damage the
3317:"FAA Rulemakings Will Pave Way for New Supersonic Era" 2831:"Supersonic Future Remains Uncertain, Says New Report" 2253:
244, 545 – 551 (31 August 1973); doi:10.1038/244545a0"
290:
The SST was seen as particularly offensive due to its
282:, which the western press nicknamed the "Concordski". 3354:"Lockheed Martin adds momentum for supersonic travel" 518:
For all vehicles traveling through air, the force of
3372:"Lockheed Martin Floats Supersonic Airliner Concept" 846:
has since made this considerably easier. In 2003, a
4464: 4390: 4327: 4318: 4311: 4229: 4202: 4166: 4157: 4115: 4044: 4035: 4014: 3893:"11 Outlandish Attempts To Build The Next Concorde" 2136:"SST supporters see little chance of reviving plan" 3735: 3733: 3365: 3363: 3298:"Spike: Supersonic Market To Draw 13M Pax by 2025" 2966:"The dream of resuming supersonic flight ramps up" 1112:policymakers to establish new standards for SSTs. 792:Therefore, a future SST might well benefit from a 485:By the end of the 20th century, projects like the 3172: 3170: 2457:"Did Concorde make a profit for British Airways?" 2160:. (Bend, Oregon). UPI. March 25, 1971. p. 1. 2088:. (Bend, Oregon). UPI. March 24, 1971. p. 1. 898:had an unusual approach to this problem with the 3939:Lampert, Allison; Freed, Jamie (July 12, 2018). 2799:. International Council on Clean Transportation. 2082:"Senators reject more funds for transport plane" 1832:and universities) with the goal of developing a 2865: 2863: 1929:at higher speeds. It would be integrated in an 1873:airframe, its capacity would be smaller than a 376:National Oceanic and Atmospheric Administration 317:National Oceanic and Atmospheric Administration 3139:"Supersonic jet promises to fly nearly silent" 868:needs, operations costs, and safety concerns. 575:managed a ratio of 7.14, whereas the subsonic 4289: 3967: 3904:Sun, Yicheng; Smith, Howard (December 2016). 3863:National Aeronautics and Space Administration 3013:"Japan, France working on new supersonic jet" 2687:. April 23, 1964. p. 649. Archived from 2056:, pp. 226–9. Burlington: Apogee Books, 2008. 1730:aircraft that can carry up to 19 passengers. 1094:International Council on Clean Transportation 772:using approximately the same amount of fuel. 466:The last regular passenger flights landed at 229:proposed a more radical design, the Mach 1.2 8: 3742:"Boeing Unveils Hypersonic Airliner Concept" 3235:"TsAGI Plans ICAO Chapter 14-compliant SSBJ" 2872:"I Was There: When the DC-8 Went Supersonic" 1945:/ramjet at the rear. It would need advanced 1450:while the engines are conceptualised at the 365:" turned to historical ozone monitoring and 2495:"Aerodynamic Database: Lift-to-Drag Ratios" 1652:low-boom flight demonstrator from 2021 for 960:or above, perhaps as high as 3000 °C. 4502: 4324: 4315: 4296: 4282: 4274: 4163: 4041: 3974: 3960: 3952: 3563:"LAPCAT aims at supersonic civil aviation" 2066:"Here's A Peek At Tomorrow's Huge Planes." 1821:began in 2008 and was to last four years. 1719:jet which could be used as Air Force One. 713: 563:Another issue in supersonic flight is the 352:United States Department of Transportation 302:dropped funding for the US SST program in 3929: 3096:, July 26, 2010. Retrieved July 28, 2010. 2745: 2735: 2451: 2449: 2427:Geiselhart, Karl A. (February 21, 1994). 1824:STRATOFLY MR3 is an EU research program ( 1037:Learn how and when to remove this message 335:by about 25 percent when compared to the 92:, a slender fuselage and four underslung 3547:Kaminski-Morrow, David (June 19, 2011). 2514:NASA SP-472 Supersonic Cruise Technology 1592:200–270 kN (45,000–60,000 lbf) 1489: 1278:Aeronautics Research Mission Directorate 1248:Relevant discussion may be found on the 595:at supersonic speeds, even though their 60:of all important aspects of the article. 3870:Hargreaves, Steve (November 26, 2014). 3179:"Problems Aerospace Still Has To Solve" 2323:"SST Emissions Cut Stratospheric Ozone" 2304:Johnston, Harold S. (January 2, 1981). 2023: 361:Nitrogen Oxides, Nuclear Weapon Testing 27:Airliner faster than the speed of sound 3206: 3204: 2652:"NASA Dryden Fact Sheet – Sonic Booms" 2401:O'Ceallaigh, John (January 21, 2016). 2176:Electronic Code of Federal Regulations 2172:"FAR 91.817 Civil aircraft sonic boom" 1640:certification will be proposed by the 418:, but with newer aircraft such as the 56:Please consider expanding the lead to 2621:globalsecurity.org, November 12, 2008 2596:Wendover Productions (May 10, 2016), 1452:Central Institute for Aviation Motors 411:studies with the 2707 as a baseline. 7: 4179:Next Generation Supersonic Transport 3759:Trimble, Stephen (August 10, 2018). 3746:Aviation Week & Space Technology 3674:Prisco, Jacopo (December 29, 2021). 3376:Aviation Week & Space Technology 3340:Aviation Week & Space Technology 3233:Karnazov, Vladimir (July 25, 2017). 3183:Aviation Week & Space Technology 3137:Hagerman, Eric (February 16, 2007). 2232:"Environment: Pre-Mortem on the SST" 2154:"Boeing workers hardest hit by vote" 1885:experience, riding the leading edge 1665:Quiet Supersonic Technology Airliner 1335:Next Generation Supersonic Transport 625:When Concorde was being designed by 152:being its last airborne operation. 4189:Zero Emission Hyper Sonic Transport 3891:Clarke, Chris (November 24, 2015). 3797:U.S. Supersonic Commercial Aircraft 3334:Warwick, Graham (October 4, 2018). 3064:O'Connell, Dominic (May 18, 2008). 2904:. Associated Press. August 17, 2000 2321:Lipkin, Richard (October 7, 1995). 1853:Boeing hypersonic transport concept 1343:Zero Emission Hyper Sonic Transport 3794:National Research Council (1997). 3783:"The United States SST Contenders" 3272:"Boom Overture – official website" 3039:"Japan tests supersonic jet model" 2995:"Firm considers 'son of Concorde'" 2870:Wasserzieher, Bill (August 2011). 2810:Thisdell, Dan (October 15, 2018). 1348:In May 2008, it was reported that 1193:Sinsheim Auto & Technik Museum 363:, Concorde and Stratospheric Ozone 358:), other scientists in the paper " 25: 3439:O'Hare, Maureen (April 2, 2021). 3252:Jackson, Paul (October 8, 2017). 3118:from the original on May 21, 2021 2964:Trimble, Stephen (May 16, 2017). 2650:Gibbs, Yvonne (August 15, 2017). 2378:. October 8, 1995. Archived from 1707:concepts and distortion-tolerant 1426:ban lift in the early 2020s. The 914:At supersonic speeds an aircraft 4501: 4258: 4257: 3884:"The Rise & Fall of The SST" 3827:Peter Coen (March 15–17, 2011). 3254:"Emerging Aircraft: Supersonics" 3106:Sheetz, Michael (May 21, 2021). 2478:2003: End of an era for Concorde 2403:"Concorde: 40 fascinating facts" 1991: 1617:, reaching 128 million by 2025; 1233: 991: 737:Passenger miles/imperial gallon 34: 4456:Vehicular communication systems 3589:"LAPCAT II – Facts and figures" 3177:Warwick, Graham (May 6, 2016). 2307:The Nitrogen Oxides Controversy 1663:, Lockheed Martin unveiled the 1605:in 2017, over 650 million flew 1542:960 kN (216,000 lbf) 1414:. The designing team is led by 848:Shaped Sonic Boom Demonstration 217:in most studies, including the 48:may be too short to adequately 4135:SAI Quiet Supersonic Transport 3922:10.1016/j.paerosci.2016.12.003 3910:Progress in Aerospace Sciences 3716:Berger, Eric (April 3, 2023). 2829:Phelps, Mark (July 18, 2018). 1636:authorization in the U.S. and 1586:4,250 nmi (7,870 km) 1567:676 kN (152,000 lbf) 1561:3,900 nmi (7,200 km) 1372:is a 12-passenger design from 1370:SAI Quiet Supersonic Transport 805:Oklahoma City sonic boom tests 505:, etc. had not been realized. 495:SAI Quiet Supersonic Transport 94:Rolls-Royce/Snecma Olympus 593 58:provide an accessible overview 1: 3886:. AirVectors. August 1, 2015. 3740:Norris, Guy (June 26, 2018). 3315:Lynch, Kerry (May 17, 2018). 3296:Lynch, Kerry (May 18, 2018). 2923:Cody, Edward (May 10, 1990). 1933:annular layout with a single 1877:but larger than a long-range 1589:77.1 t (170,000 lb) 979:interest in buying the jets. 759:Litres/passenger 100 km 331:in surface temperatures from 4097:Sud Aviation Super-Caravelle 3800:. National Academies Press. 3695:Spry, Jeff (June 28, 2022). 3521:Jeff Spry (April 17, 2024). 3370:Guy Norris (June 19, 2019). 1564:185 t (408,000 lb) 1135:to stay under a 1.5 °C 430:engine with ever-increasing 237:proposed several designs to 219:Sud Aviation Super-Caravelle 85:supersonic transport had an 4479:Automated vacuum collection 4242:Lockheed Martin X-59 QueSST 3239:Aviation International News 2007:List of supersonic aircraft 1650:Lockheed Martin X-59 QueSST 1454:and designs are studied by 1428:Lockheed Martin X-59 QueSST 1416:Lockheed Martin Aeronautics 1201:Concorde aircraft histories 1104:, six times as much as for 1017:the claims made and adding 718:fuel efficiency comparison 367:atmospheric nuclear testing 4563: 4184:Reaction Engines LAPCAT A2 4072:High Speed Civil Transport 2599:Why Flying is So Expensive 2562:"Technical Specifications" 2512:McLean, F. Edward (1985). 1743: 1536:3,500 nmi (6,500 km) 1276:concept presented to NASA 1198: 1131:if aviation maintains its 748:Passenger miles/US gallon 503:High Speed Civil Transport 470:on October 24, 2003, from 189:about the same speed. The 4497: 4255: 4022:Aérospatiale/BAC Concorde 3989: 3816:"Overview: Civil Engines" 3214:. NASA. February 29, 2016 3001:. BBC. November 23, 2003. 2497:. Aerodyn. Archived from 1387:have also been proposed. 1242:This section needs to be 597:specific fuel consumption 350:team commissioned by the 337:warming rate in the 1990s 321:Stratospheric Water Vapor 247:Bristol Aeroplane Company 4405:Alternative fuel vehicle 2876:Air & Space Magazine 2635:. For Your Information. 2633:"Anyone Else for Space?" 2631:Ley, Willy (June 1964). 1803:Reaction Engines Limited 1765:pulse detonation engines 1601:Of the four billion air 1576:Boom Technology Overture 1539:207 t (456,000 lb) 4367:Pulse detonation engine 4337:Adaptive compliant wing 3045:. BBC. October 10, 2005 1973:. It would have a high 1925:, but shutting off the 1923:Pratt & Whitney J58 1826:German Aerospace Center 1325:—the parent company of 983:Commercial practicality 896:North American Aviation 522:is proportional to the 474:, a second flight from 157:supersonic business jet 4436:Personal rapid transit 4357:High-altitude platform 4140:Sukhoi-Gulfstream S-21 3089:March 5, 2012, at the 2637:Galaxy Science Fiction 1913:that transitions to a 1854: 1685:external vision system 1437:exhibited at the 2017 1400:into service in 2029. 1318: 1289: 1281: 1205:On August 21, 1961, a 1196: 1064: 876:had very high drag (a 853:Sonic boom § Abatement 817:Sonic boom § Abatement 815:proved otherwise (see 622: 541: 499:Sukhoi-Gulfstream S-21 457:Air France Flight 4590 286:Environmental concerns 206: 110: 97: 4532:Supersonic transports 4305:Emerging technologies 4230:Experimental programs 4087:North American NAC-60 3593:European Space Agency 3258:Aviation Week Network 2716:Nature Communications 2681:"Design for Mach 2.2" 2619:Concord Airport Noise 2501:on February 20, 2008. 2140:Eugene Register-Guard 2104:Eugene Register-Guard 1883:Boeing X-51 Waverider 1852: 1798:Precooled jet engines 1755:typically either use 1624:In October 2018, the 1312: 1287: 1272: 1190: 1052: 844:computer-aided design 794:variable cycle engine 606: 539: 329:slow down in the rise 204: 103: 80: 4451:Transit Elevated Bus 4382:Supersonic transport 3983:Supersonic transport 3789:. February 13, 1964. 3787:Flight International 3551:. Flight Daily News. 2816:Flight International 2685:Flight International 2382:on September 1, 2016 2071:, April 1960, p. 86. 1975:capacity utilization 1949:technology like the 1786:, EADS unveiled its 1740:Hypersonic transport 1465:At the October 2017 1088:Environmental impact 825:variable-sweep wings 115:supersonic transport 18:Suborbital transport 4474:Pneumatic transport 4417:Ground-effect train 4342:Backpack helicopter 4107:HyperMach SonicStar 3999:Supersonic aircraft 3845:on January 21, 2022 3822:on August 21, 2006. 3595:. November 17, 2009 2953:. October 12, 2016. 2935:on January 3, 2014. 2929:The Washington Post 2737:10.1038/ncomms15836 2728:2017NatCo...815836Z 2639:. pp. 110–128. 2459:(FAQ). Concorde SST 2285:on December 8, 2016 2238:, September 9, 1974 2052:Whitcomb, Randall. 1656:standards in 2025. 1475:Boom XB-1 Baby Boom 1315:High-Speed Research 807:and studies of the 719: 524:coefficient of drag 227:Armstrong-Whitworth 130:supersonic aircraft 123:supersonic airliner 4537:British inventions 4062:Convair Model 58-9 4015:Historic airliners 3637:. August 23, 2019. 3189:on January 2, 2018 3161:Bloomberg Business 3155:(March 21, 2016). 2691:on January 3, 2017 2333:on January 7, 2023 2100:"SST funds denied" 1855: 1683:; and the cockpit 1442:both Mach 0.8–0.9 1321:In November 2003, 1319: 1290: 1282: 1225:Future development 1197: 1183:Completed projects 1151:, and over 100 in 1137:climate trajectory 1098:fuel per passenger 1065: 1002:possibly contains 922:materials such as 878:lift to drag ratio 811:'s North American 714: 647:de Havilland Comet 623: 565:lift to drag ratio 542: 380:sulfur in the fuel 207: 186:lift-to-drag ratio 111: 98: 4547:French inventions 4542:Soviet inventions 4517: 4516: 4493: 4492: 4489: 4488: 4271: 4270: 4225: 4224: 4153: 4152: 3897:Popular Mechanics 3569:. August 30, 2007 3502:. August 22, 2023 3488:. August 3, 2020. 3468:. August 3, 2020. 2376:The Baltimore Sun 2069:Popular Mechanics 1782:At the June 2011 1774:transports or as 1750:Hypersonic flight 1648:plans to fly the 1599: 1598: 1305:Previous concepts 1267: 1266: 1100:than in subsonic 1047: 1046: 1039: 1004:original research 769: 768: 455:On 25 July 2000, 374:scientist at the 75: 74: 16:(Redirected from 4554: 4505: 4504: 4446:Self-driving car 4410:Hydrogen vehicle 4325: 4316: 4298: 4291: 4284: 4275: 4261: 4260: 4164: 4057:Bristol Type 223 4042: 3976: 3969: 3962: 3953: 3948: 3935: 3933: 3900: 3887: 3879: 3866: 3865:. February 2013. 3854: 3852: 3850: 3844: 3836:Project Overview 3833: 3823: 3811: 3790: 3769: 3768: 3756: 3750: 3749: 3737: 3728: 3727: 3713: 3707: 3706: 3692: 3686: 3685: 3671: 3665: 3664: 3662: 3660: 3645: 3639: 3638: 3625: 3619: 3618: 3617:. July 19, 2018. 3611: 3605: 3604: 3602: 3600: 3585: 3579: 3578: 3576: 3574: 3559: 3553: 3552: 3544: 3538: 3537: 3535: 3533: 3518: 3512: 3511: 3509: 3507: 3496: 3490: 3489: 3476: 3470: 3469: 3462: 3456: 3455: 3453: 3451: 3436: 3430: 3429: 3427: 3425: 3415:"Supersonic Jet" 3411: 3405: 3404: 3402: 3400: 3386: 3380: 3379: 3367: 3358: 3357: 3350: 3344: 3343: 3331: 3325: 3324: 3312: 3306: 3305: 3293: 3287: 3286: 3284: 3282: 3268: 3262: 3261: 3249: 3243: 3242: 3230: 3224: 3223: 3221: 3219: 3208: 3199: 3198: 3196: 3194: 3185:. Archived from 3174: 3165: 3164: 3149: 3143: 3142: 3134: 3128: 3127: 3125: 3123: 3103: 3097: 3080: 3074: 3073: 3061: 3055: 3054: 3052: 3050: 3035: 3029: 3028: 3026: 3024: 3009: 3003: 3002: 2991: 2985: 2980: 2974: 2973: 2961: 2955: 2954: 2943: 2937: 2936: 2931:. Archived from 2920: 2914: 2913: 2911: 2909: 2898: 2892: 2891: 2889: 2887: 2878:. Archived from 2867: 2858: 2857: 2845: 2839: 2838: 2826: 2820: 2819: 2807: 2801: 2800: 2792: 2786: 2785: 2783: 2781: 2766: 2760: 2759: 2749: 2739: 2707: 2701: 2700: 2698: 2696: 2677: 2671: 2666: 2660: 2659: 2647: 2641: 2640: 2628: 2622: 2616: 2610: 2609: 2608: 2606: 2584: 2578: 2577: 2575: 2573: 2558: 2552: 2550: 2548: 2546: 2532: 2526: 2525: 2522:2060/19850020600 2509: 2503: 2502: 2491: 2485: 2475: 2469: 2468: 2466: 2464: 2453: 2444: 2443: 2441: 2439: 2433: 2424: 2418: 2417: 2415: 2413: 2398: 2392: 2391: 2389: 2387: 2368: 2362: 2361: 2349: 2343: 2342: 2340: 2338: 2329:. Archived from 2318: 2312: 2311: 2301: 2295: 2294: 2292: 2290: 2284: 2278:. Archived from 2268:10.1038/244545a0 2257: 2245: 2239: 2229: 2223: 2222: 2211: 2205: 2204: 2193: 2187: 2186: 2184: 2182: 2168: 2162: 2161: 2150: 2144: 2143: 2132: 2126: 2125: 2122:Spokesman-Review 2114: 2108: 2107: 2096: 2090: 2089: 2078: 2072: 2063: 2057: 2050: 2044: 2043: 2041: 2039: 2032:"Retirement FAQ" 2028: 2001: 1996: 1995: 1994: 1967:depressurization 1955:Reaction Engines 1860:unveiled at the 1746:Hypersonic speed 1722:In August 2020, 1509: 1490: 1262: 1259: 1253: 1237: 1236: 1229: 1042: 1035: 1031: 1028: 1022: 1019:inline citations 995: 994: 987: 910:Skin temperature 904:compression lift 830:Concorde had an 720: 615:Filton Aerodrome 305: 223:Bristol Type 223 211:fighter aircraft 205:Concorde landing 70: 67: 61: 38: 30: 21: 4562: 4561: 4557: 4556: 4555: 4553: 4552: 4551: 4522: 4521: 4518: 4513: 4485: 4460: 4386: 4307: 4302: 4272: 4267: 4251: 4221: 4212:Gulfstream X-54 4198: 4194:Hermeus Halcyon 4159: 4149: 4111: 4082:Lockheed L-2000 4037: 4031: 4010: 3985: 3980: 3938: 3903: 3890: 3882: 3869: 3857: 3848: 3846: 3842: 3831: 3826: 3814: 3808: 3793: 3781: 3778: 3773: 3772: 3758: 3757: 3753: 3739: 3738: 3731: 3715: 3714: 3710: 3694: 3693: 3689: 3673: 3672: 3668: 3658: 3656: 3647: 3646: 3642: 3627: 3626: 3622: 3613: 3612: 3608: 3598: 3596: 3587: 3586: 3582: 3572: 3570: 3561: 3560: 3556: 3546: 3545: 3541: 3531: 3529: 3520: 3519: 3515: 3505: 3503: 3498: 3497: 3493: 3478: 3477: 3473: 3464: 3463: 3459: 3449: 3447: 3438: 3437: 3433: 3423: 3421: 3413: 3412: 3408: 3398: 3396: 3388: 3387: 3383: 3369: 3368: 3361: 3352: 3351: 3347: 3333: 3332: 3328: 3314: 3313: 3309: 3295: 3294: 3290: 3280: 3278: 3276:Boom Supersonic 3270: 3269: 3265: 3251: 3250: 3246: 3232: 3231: 3227: 3217: 3215: 3210: 3209: 3202: 3192: 3190: 3176: 3175: 3168: 3151: 3150: 3146: 3136: 3135: 3131: 3121: 3119: 3105: 3104: 3100: 3091:Wayback Machine 3081: 3077: 3063: 3062: 3058: 3048: 3046: 3037: 3036: 3032: 3022: 3020: 3019:. June 15, 2005 3011: 3010: 3006: 2993: 2992: 2988: 2981: 2977: 2963: 2962: 2958: 2945: 2944: 2940: 2922: 2921: 2917: 2907: 2905: 2900: 2899: 2895: 2885: 2883: 2882:on May 11, 2014 2869: 2868: 2861: 2847: 2846: 2842: 2828: 2827: 2823: 2809: 2808: 2804: 2794: 2793: 2789: 2779: 2777: 2768: 2767: 2763: 2709: 2708: 2704: 2694: 2692: 2679: 2678: 2674: 2667: 2663: 2649: 2648: 2644: 2630: 2629: 2625: 2617: 2613: 2604: 2602: 2595: 2592:Wayback Machine 2585: 2581: 2571: 2569: 2560: 2559: 2555: 2544: 2542: 2534: 2533: 2529: 2511: 2510: 2506: 2493: 2492: 2488: 2476: 2472: 2462: 2460: 2455: 2454: 2447: 2437: 2435: 2431: 2426: 2425: 2421: 2411: 2409: 2407:telegraph.co.uk 2400: 2399: 2395: 2385: 2383: 2370: 2369: 2365: 2351: 2350: 2346: 2336: 2334: 2320: 2319: 2315: 2303: 2302: 2298: 2288: 2286: 2282: 2255: 2247: 2246: 2242: 2230: 2226: 2213: 2212: 2208: 2195: 2194: 2190: 2180: 2178: 2170: 2169: 2165: 2152: 2151: 2147: 2134: 2133: 2129: 2116: 2115: 2111: 2098: 2097: 2093: 2080: 2079: 2075: 2064: 2060: 2051: 2047: 2037: 2035: 2030: 2029: 2025: 2020: 1999:Aviation portal 1997: 1992: 1990: 1987: 1919:SR-71 Blackbird 1752: 1742: 1724:Virgin Galactic 1705:noise shielding 1675:are allowed by 1626:reauthorization 1503: 1397:Boom Technology 1395:In March 2016, 1393: 1385:Gulfstream X-54 1379:The supersonic 1374:Lockheed Martin 1307: 1274:Lockheed Martin 1263: 1257: 1254: 1247: 1238: 1234: 1227: 1207:Douglas DC-8-43 1203: 1185: 1149:London Heathrow 1133:emissions share 1090: 1082:high-speed rail 1043: 1032: 1026: 1023: 1008: 996: 992: 985: 966: 924:stainless steel 912: 865: 863:Variable speeds 782: 780:Noise pollution 712: 671: 608:British Airways 593:fuel efficiency 586: 552:speeds (around 531: 516: 511: 468:London Heathrow 453: 440: 388: 344:nitrogen oxides 303: 288: 267:Lockheed L-2000 243:Hawker Siddeley 178: 173: 71: 65: 62: 55: 43:This article's 39: 28: 23: 22: 15: 12: 11: 5: 4560: 4558: 4550: 4549: 4544: 4539: 4534: 4524: 4523: 4515: 4514: 4512: 4511: 4498: 4495: 4494: 4491: 4490: 4487: 4486: 4484: 4483: 4482: 4481: 4470: 4468: 4462: 4461: 4459: 4458: 4453: 4448: 4443: 4438: 4433: 4428: 4419: 4414: 4413: 4412: 4402: 4396: 4394: 4388: 4387: 4385: 4384: 4379: 4374: 4369: 4364: 4359: 4354: 4349: 4347:Delivery drone 4344: 4339: 4333: 4331: 4322: 4313: 4309: 4308: 4303: 4301: 4300: 4293: 4286: 4278: 4269: 4268: 4256: 4253: 4252: 4250: 4249: 4244: 4239: 4233: 4231: 4227: 4226: 4223: 4222: 4220: 4219: 4214: 4208: 4206: 4200: 4199: 4197: 4196: 4191: 4186: 4181: 4176: 4170: 4168: 4161: 4155: 4154: 4151: 4150: 4148: 4147: 4145:Tupolev Tu-444 4142: 4137: 4132: 4127: 4121: 4119: 4113: 4112: 4110: 4109: 4104: 4102:Tupolev Tu-244 4099: 4094: 4089: 4084: 4079: 4074: 4069: 4064: 4059: 4054: 4048: 4046: 4039: 4033: 4032: 4030: 4029: 4027:Tupolev Tu-144 4024: 4018: 4016: 4012: 4011: 4009: 4008: 4007: 4006: 3996: 3994:Civil aviation 3990: 3987: 3986: 3981: 3979: 3978: 3971: 3964: 3956: 3950: 3949: 3936: 3901: 3888: 3880: 3867: 3855: 3824: 3812: 3807:978-0309058780 3806: 3791: 3777: 3776:External links 3774: 3771: 3770: 3751: 3729: 3708: 3687: 3666: 3648:Tegler, Eric. 3640: 3620: 3606: 3580: 3554: 3539: 3513: 3491: 3471: 3457: 3431: 3406: 3381: 3359: 3345: 3326: 3307: 3288: 3263: 3244: 3225: 3200: 3166: 3144: 3129: 3098: 3075: 3056: 3030: 3004: 2986: 2975: 2956: 2938: 2915: 2893: 2859: 2840: 2821: 2802: 2787: 2761: 2702: 2672: 2661: 2642: 2623: 2611: 2579: 2566:Boeing 747-400 2553: 2527: 2504: 2486: 2470: 2445: 2434:(Report). NASA 2419: 2393: 2363: 2344: 2313: 2296: 2240: 2224: 2206: 2188: 2163: 2145: 2127: 2109: 2091: 2073: 2058: 2045: 2034:. Concorde SST 2022: 2021: 2019: 2016: 2015: 2014: 2009: 2003: 2002: 1986: 1983: 1959:liquid methane 1957:, maybe using 1951:heat exchanger 1897:would enhance 1834:cryogenic fuel 1784:Paris Air Show 1779:launch costs. 1741: 1738: 1634:flight-testing 1597: 1596: 1593: 1590: 1587: 1584: 1581: 1578: 1572: 1571: 1568: 1565: 1562: 1559: 1556: 1553: 1547: 1546: 1543: 1540: 1537: 1534: 1531: 1528: 1526:Tupolev Tu-144 1522: 1521: 1520:Thrust/weight 1518: 1515: 1510: 1500: 1497: 1494: 1488: 1487: 1479: 1392: 1389: 1381:Tupolev Tu-444 1306: 1303: 1265: 1264: 1241: 1239: 1232: 1226: 1223: 1184: 1181: 1102:business-class 1089: 1086: 1061:Paris Air Show 1057:Tupolev Tu-144 1045: 1044: 999: 997: 990: 984: 981: 965: 962: 949:In 2017 a new 928:XB-70 Valkyrie 911: 908: 900:XB-70 Valkyrie 864: 861: 813:XB-70 Valkyrie 781: 778: 767: 766: 763: 760: 756: 755: 752: 749: 745: 744: 741: 738: 734: 733: 727: 724: 711: 708: 693:and TU-144 of 675:aeroelasticity 670: 667: 637:jet engines (" 585: 582: 569:wing planforms 529: 515: 512: 510: 507: 491:Tupolev Tu-344 487:Tupolev Tu-244 452: 449: 439: 436: 387: 384: 333:global warming 287: 284: 177: 174: 172: 169: 142:Tupolev Tu-144 134:speed of sound 106:Tupolev Tu-144 73: 72: 52:the key points 42: 40: 33: 26: 24: 14: 13: 10: 9: 6: 4: 3: 2: 4559: 4548: 4545: 4543: 4540: 4538: 4535: 4533: 4530: 4529: 4527: 4520: 4510: 4509: 4500: 4499: 4496: 4480: 4477: 4476: 4475: 4472: 4471: 4469: 4467: 4463: 4457: 4454: 4452: 4449: 4447: 4444: 4442: 4439: 4437: 4434: 4432: 4429: 4427: 4423: 4420: 4418: 4415: 4411: 4408: 4407: 4406: 4403: 4401: 4398: 4397: 4395: 4393: 4389: 4383: 4380: 4378: 4375: 4373: 4370: 4368: 4365: 4363: 4360: 4358: 4355: 4353: 4350: 4348: 4345: 4343: 4340: 4338: 4335: 4334: 4332: 4330: 4326: 4323: 4321: 4317: 4314: 4310: 4306: 4299: 4294: 4292: 4287: 4285: 4280: 4279: 4276: 4266: 4265: 4254: 4248: 4245: 4243: 4240: 4238: 4235: 4234: 4232: 4228: 4218: 4215: 4213: 4210: 4209: 4207: 4205: 4204:Business jets 4201: 4195: 4192: 4190: 4187: 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by 1952: 1948: 1944: 1940: 1936: 1932: 1928: 1924: 1920: 1916: 1912: 1908: 1904: 1900: 1896: 1892: 1888: 1884: 1880: 1876: 1872: 1868: 1863: 1859: 1851: 1847: 1845: 1841: 1837: 1835: 1831: 1827: 1822: 1820: 1816: 1815: 1810: 1809: 1804: 1799: 1795: 1793: 1789: 1785: 1780: 1777: 1776:semiballistic 1773: 1768: 1766: 1762: 1758: 1751: 1747: 1739: 1737: 1734: 1731: 1729: 1725: 1720: 1717: 1716:Exosonic, Inc 1712: 1710: 1706: 1702: 1696: 1694: 1690: 1686: 1682: 1678: 1674: 1670: 1669:airport noise 1666: 1662: 1657: 1655: 1651: 1647: 1643: 1639: 1635: 1631: 1627: 1622: 1620: 1616: 1612: 1608: 1604: 1594: 1591: 1588: 1585: 1582: 1579: 1577: 1574: 1573: 1569: 1566: 1563: 1560: 1557: 1554: 1552: 1549: 1548: 1544: 1541: 1538: 1535: 1532: 1529: 1527: 1524: 1523: 1519: 1516: 1514: 1511: 1507: 1501: 1498: 1495: 1492: 1491: 1484: 1480: 1476: 1472: 1471: 1470: 1468: 1463: 1461: 1457: 1453: 1449: 1445: 1440: 1439:MAKS Air Show 1436: 1431: 1429: 1425: 1421: 1417: 1413: 1410: 1409:low-noise SST 1406: 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Index

Suborbital transport

lead section
summarize
provide an accessible overview

Concorde
ogival
delta wing
Rolls-Royce/Snecma Olympus 593

Tupolev Tu-144
civilian
supersonic aircraft
speed of sound
Concorde
Tupolev Tu-144
NASA
ferry flight
supersonic business jet
sonic booms
lift
lift-to-drag ratio
sortie

fighter aircraft
delta wing
Sud Aviation Super-Caravelle
Bristol Type 223
Armstrong-Whitworth

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