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Saturn I SA-2

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SA-2's dummy upper stages contained approximately 190,000 pounds (86,000 kg) of water, or 22,900 U.S. gallons (86,685 L), used to simulate the mass of future payloads. Stage two contained 97,000 pounds (44,000 kg) of water, and stage three contained 93,000 pounds (42,000 kg). When
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in that it was primarily a test of the Saturn I rocket and the new H-1 engines. Specifically, its goals were to prove propulsion performance and mission adequacy, vehicle structural design and aerodynamic characteristics, guidance and control systems, and launch facility and ground support equipment.
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The H-1 engines shut down at an altitude of 35 miles (56 km) after firing for 1 minute 55 seconds and reaching a maximum velocity of 3,750 miles per hour (6,040 km/h; 1,680 m/s). The vehicle continued to coast to an altitude of 65.4 miles (105.3 km), at which point, 2 minutes 40
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Cameras on the ground immediately recorded the water cloud, and personnel at a ground station began to observe it about four to five seconds after release. Those personnel reported that the cloud dispersed from vision within an average of five seconds, while more sensitive instruments tracked the
310:. The only hold in the countdown sequence was for 30 minutes due to a vessel which entered the flight safety zone 60 miles (96 km) down range. The rocket carried 619,000 pounds (281,000 kg) of propellant, about 83% of its maximum capacity. 279:; while attempts were made to fix the problem, it was eventually decided to launch without replacing the engine. Minor problems were found in the guidance subsystem and service structure operations, damaged 259:
Launch preparation for the mission began at Cape Canaveral on February 27, 1962, with the arrival of the second Saturn I launch vehicle. The only significant change made to the vehicle from the previous
287:(S-V-D) third stage had to be replaced. Problems arose with two of the fueling computers, but each was repaired. Three hydraulic systems were also listed as potential problems. 307: 150: 730: 1543: 1169: 1494: 384: 1226: 445: 578: 1298: 1016: 635: 703: 698: 366:
described as "probably the first synthetic thunderstorm ever generated in space." Project Highwater on this flight was also declared a success.
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the terminate command was sent to the rocket, dynamite charges split the second stage longitudinally, instantly releasing its water load.
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seconds after launch, officials sent a terminate command to the rocket, setting off several charges which caused the vehicle to destruct.
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Despite the issues encountered during flight preparation, none required the target launch date of April 25 to be pushed back.
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charges created several 1-foot (0.30 m) holes in the third stage, releasing its water over a period of several seconds.
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cloud to a maximum altitude of 100 miles (161 km). The cloud produced lightning-like effects, which Dr.
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NASA declared all objectives as successful. Additionally, the fuel sloshing issue from SA-1 was minimized.
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water from the second and third stages which allowed scientists to investigate the nature of Earth's
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were found in a liquid oxygen stud and truss member, and a manhole cover on the dummy
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A leak was detected between the liquid oxygen dome and injector for the #4
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Saturn-Apollo 2 was launched at 14:00:34 UTC on April 25, 1962, from
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Brooks, Courtney G; Grimwood, James M; Swenson, Jr, Loyd S (1979).
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Moonport: A History of Apollo Launch Facilities and Operations
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Second flight of the Saturn I launch vehicle, April 25, 1962
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Chariots for Apollo: A History of Manned Lunar Spacecraft
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Woodbridge, David D; Lasater, James A (March 6, 1965).
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The objectives of SA-2 were much the same as those of
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Benson, Charles D; Faherty, William Barnaby (1978).
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The rocket was launched on April 25, 1962, from 548: 546: 544: 542: 540: 538: 536: 534: 495:"Big US Rocket Releases 95 Tons of Water in Sky" 489: 487: 485: 524:The Apollo Spacecraft: A Chronology - Volume 1 1495:Third-party evidence for Apollo Moon landings 629: 385:National Aeronautics and Space Administration 31:SA-2 sitting on Pad 34 with service structure 8: 1507:Symbol indicates failure or partial failure 467: 465: 463: 407: 405: 403: 401: 399: 397: 395: 330:A second objective of both this mission and 19: 516: 514: 834: 714: 636: 622: 614: 521:Ertel, Ivan D; Morse, Mary Louise (1969). 431: 429: 25: 18: 268:in the propellant tanks to mitigate fuel 391: 556:An Analysis of Project High Water Data 448:from the original on December 10, 2022 1544:Spacecraft launched by Saturn rockets 7: 1170:50th Anniversary commemorative coins 239:launch vehicle, the first flight of 581:from the original on March 10, 2023 559:. NASA. Accession number N65-21330. 383:from websites or documents of the 350:and the behavior of ice in space. 14: 571:"Saturn Brews Space Thunderstorm" 414:"Saturn I Launches (1962 - 1965)" 264:flight was the addition of extra 602: 379: This article incorporates 374: 99:420,000 kg (463 short tons) 1422:Apollo Lunar Sounder Experiment 243:, and was part of the American 235:) was the second flight of the 62:2 minutes, 40 seconds 1247:"Houston, we've had a problem" 736:Cape Kennedy Air Force Station 1: 1490:Stolen and missing Moon rocks 1263:Modular Equipment Transporter 503:. 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Index


NASA
Saturn I
Cape Canaveral
LC-34
Project Highwater
Project Apollo
Saturn I SA-1
Saturn I SA-3
Saturn I
Project Highwater
Apollo program
Cape Canaveral
SA-1
baffles
sloshing
H-1 rocket engine
strain gauges
Centaur

Launch Complex 34
SA-1
SA-3
Project Highwater
ballast
ionosphere
noctilucent clouds
Primacord
Wernher von Braun
public domain material

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