Chronology - Quarter 1 1962 home
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1962 January 1 -
  • Only 84 NASA personnel move from Langley to Houston Nation: USA. A survey was performed at the Manned Spacecraft Center to ascertain the number of personnel who intended to move with the Center from Langley Field to Houston, Texas. Only 84 personnel indicated they would not make the move. References: 483.
1962 - Launch Vehicle: Sea Dragon.
  • Sea Dragon low cost heavy-lift vehicle proposed Nation: USA. Sea Dragon was a two-stage design capable of putting 550 tonnes into low Earth orbit. The concept was to achieve minimum launch costs through lower development and production costs. This meant accepting a larger booster with a lower performance propulsion system and higher stage dead weight then traditional NASA and USAF designs.
1962 - Launch Site: Point Mugu. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • PM-6 test Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
1962 - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skua. Model: Skua 1.
  • Test / aeronomy mission Nation: UK. Agency: UK MO. Apogee: 70 km (43 mi). References: 2.
1962 During the Year - Launch Vehicle: Soyuz. Model: Soyuz 11A511.
  • Vostok-Zh studies Nation: USSR. Program: Lunar L1. Class: Manned. Type: Spacecraft. Spacecraft: Vostok-Zh. Vostok-Zh studies conducted for multiple dockings of rocket blocks and payloads in orbit for circumlunar missions, using Vostok rocket. Vostok-Zh spacecraft used to for manual dockings only. Manned reentry vehicle from circumlunar distance is Sever/Soyuz design. Korolev's reaction to Chelomei's exclusive assignment by Khrushchev to circumlunar mission. References: 26.
1962 During the Year - Launch Vehicle: UR-700.
  • Development of RD-270 engine begun Nation: USSR. Program: Lunar L3. Class: Manned. Type: Lunar. Spacecraft: LK-700. The RD-270 engine was proposed for Chelomei's UR-700 and Yangel R-56 lunar landing launchers in competition to Korolev N1. The RD-270 was in the same class as the F-1 engine developed for America's Saturn V launch vehicle, but burned storable but toxic propellants. References: 74.
1962 During the Year -
  • Draft project for Tsiklon experimental navigation satellite completed Nation: USSR. Spacecraft: Tsiklon. Research institute NII-695 completed the draft project for a Tsiklon experimental navigation satellite. It was to use the Doppler navigation method and be placed in 800 to 1000 km altitude orbits. Experimental flights began in 1967 in order to develop a system meeting the required tactical and operational characteristics.
1962 During the Year -
  • Zvezda Long-term Lunar Base (DLB) Nation: USSR. Spacecraft: DLB Module. The N1 draft project of 1962 spoke of 'establishment of a lunar base and regular traffic between the earth and the moon'. Korolev raised the matter informally at tea with Chief Designer of rocket complexes Vladimir Pavlovich Barmin, head of GSKB SpetsMash (State Union Design Bureau of Special Machine-Building). 'You just design the base', Korolev assured him, 'and I'll figure out how to get it there'. Under the DLB studies SpetsMash defined purposes of the base, the principles of its construction, phases of its deployment and composition of its scientific and support equipment. The enthusiasts that worked on the project at Zvezda were naturally known as 'lunatics'.
1962 During the Year - Launch Vehicle: UR-700.
  • UR-700 launch vehicle for manned lunar landing missions. Nation: USSR. Spacecraft: LK-700. Chelomei's TsKBM began work on the UR-700. The conclusion was reached that a direct lunar landing would require a payload of 130 to 170 tonnes. Initial LK-700 spacecraft designs were derived from the 'Raketoplan' family of manned modular space vehicles. Korolev's N1-L3 design was selected in 1964 for the manned lunar landing, but the UR-700 would surface again when the N1 encountered delays.
1962 During the Year - Launch Vehicle: N1, Proton, R-56.
  • GR-2 (Global Rocket 2) requirement. Nation: USSR. The GR-2 was to be a kind of enormous multiple-warhead FOBS (fractional orbit bombing system). Competitors included Korolev's N-11GR; Chelomei's UR-500; and Yangel's R-56
1962 January - Launch Vehicle: Proton. Model: Proton 8K82.
  • Proton design selected Nation: USSR. This 'polyblock' design was chosen for the Proton launch vehicle, following studies that indicated improved wind loads and bending moment characteristics compared to the monoblock design.
1962 January-June -
  • Grumman study on lunar orbit rendezvous Nation: USA. Program: Apollo. Spacecraft: Apollo LM. The Grumman Aircraft Engineering Corporation developed a detailed, company-funded study on the lunar orbit rendezvous technique: characteristics of the system (relative cost of direct ascent, earth orbit rendezvous, and lunar orbit rendezvous); developmental problems (communications, propulsion); and elements of the system (tracking facilities, etc.). Joseph M. Gavin was appointed in the spring to head the effort, and Robert E. Mullaney was designated program manager. References: 16.
1962? - Launch Site: Sary Shagan. Launch Complex: LC6. Launch Pad: -. Launch Vehicle: A-35. Model: A-350Zh. LV Configuration: A-350Zh 5TYa F4.
  • Test mission Nation: USSR. Agency: PRO. Apogee: 10 km (6 mi). References: 2.
During 1962 -
  • First Chinese trainees in satellite technology Nation: China. Spacecraft: DFH-1. Four engineers from the Shanghai Institute of Machine and Electrical Design receive the first Chinese training in satellite design.
Early 1962 - Launch Vehicle: DF-4.
  • Chinese project management Nation: China. Tsien introduced a computer tool for management of Chinese aerospace development projects analogous to the American PERT program.
1962 January 3 - Launch Vehicle: Titan. Model: Titan 2.
  • Statement of Work for the procurement of Titan II launch vehicles for the Gemini program. Nation: USA. Manned Spacecraft Center prepared a Statement of Work to be accomplished by Air Force Space Systems Division (SSD) in its role as contractor to NASA for the procurement of Titan II launch vehicles for the Gemini program. The launch vehicle would retain the general aerodynamic shape, basic systems, and propulsion concepts of the missile. Modifications, primarily for crew safety, were to be kept to a minimum. The Statement of Work accompanied a purchase request for $27 million, dated January 5, 1962, for 15 Titan launch vehicles. Pending ratification of the Gemini Operational and Management Plan, however, funding was limited to $3 million. To oversee this work, SSD established a Gemini Launch Vehicle Directorate, headed by Colonel Richard C. Dineen, on January 11. Initial budgeting and planning were completed by the end of March, and a final Statement of Work was issued May 14; although amended, it remained in effect throughout the program.
1962 January 3 -
  • "Gemini" became the official designation of the Mercury Mark II program. Nation: USA. Program: Gemini. Spacecraft: Gemini. The name had been suggested by Alex P. Nagy of NASA Headquarters because the twin stars Castor and Pollux in constellation Gemini (the Twins) seemed to him to symbolize the program's two-man crew, its rendezvous mission, and its relation to Mercury. Coincidentally, the astronomical symbol (II) for Gemini, the third constellation of the zodiac, corresponded neatly to the Mark II designation.
1962 January 4 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1962 January 5 - Launch Vehicle: Saturn V.
  • Three-man Apollo spacecraft, Saturn C-5 launch vehicle announced Nation: USA. Program: Apollo. Spacecraft: Apollo Lunar Landing. NASA made public the drawings of the three-man Apollo spacecraft to be used in the lunar landing development program, On January 9, NASA announced its decision that the Saturn C-5 would be the lunar launch vehicle. References: 16.
1962 January 5 - 15:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 407.
  • Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2.
1962 January 10 - 20:28 GMT - Launch Site: Mud Lake DZ. Launch Complex: -. Launch Pad: 37.9 N x 117.1 W. Launch Vehicle: X-15. LV Configuration: X-15 1-25-44. FAILURE: Emergency landing at Mud Lake.
  • X-15A High alpha, Aero test Nation: USA. Agency: NASA/USAF. Apogee: 13 km (8 mi). Emergency landing on Mud Lake after engine failed to light. Maximum Speed - 1038 kph. Maximum Altitude - 13,640 m. References: 2.
1962 January 11 -
  • In State of the Union message Kennedy discusses moon program Nation: USA. Program: Apollo. In his State of the Union message to the Congress, President John F . Kennedy said: "With the approval of this Congress, we have undertaken in the past year a great new effort in outer space. Our aim is not simply to be first on the moon, any more than Charles Lindbergh's real aim was to be first to Paris. His aim was to develop the techniques and the authority of this country and other countries in the field of the air and the atmosphere, and our objective in making this effort, which we hope will place one of our citizens on the moon, is to develop in a new frontier of science, commerce and cooperation, the position of the United States and the free world. This nation belongs among the first to explore it. And among the first - if not the first - we shall be." References: 16.
1962 January 11 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: R-14U.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 675 km (419 mi). References: 2.
1962 January 13 - Launch Vehicle: Spiral 50-50.
  • VVS Military-Scientific Conference at Monino Nation: USSR. Spacecraft: Spiral OS. Recommendations made by Kamanin's space unit included:
    • A KLA aerospace vehicle should be developed. This could be flown in a sub-orbital version at altitudes of 60 to 150 km and as an orbital aero-spaceplane at altitudes of 1000 to 3000 km.
    • An aircraft-launcher should be developed to allow air-launch of the KLA as well as air-to-space and space-to-earth missiles
    • Navigation, reconnaissance, guidance, and environmental control systems should be developed for the KLA suitable for flights of up to 30 days duration
    To achieve this it will be necessary to conduct research and development in air-launch and landing of the KLA, and train cosmonauts in engineering, medicine, and other specialties. The IAKM and TsPK would both need improvements. References: 376.
1962 January 13 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1962 January 13 - 16:15 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.68GT.
  • Attitude control test Nation: USA. Agency: NASA. Apogee: 209 km (129 mi). References: 2.
1962 January 13 - 21:41 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 327 / Agena B 1120. FAILURE: Failure.
  • Discoverer 37 Nation: USA. Payload: KH-3 s/n 9030. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-3. Agency: U.S. Air Force. COSPAR: F620113A. Decay Date: 1962-01-13. KH-3. Mission failed. Last attempted flight of KH-3 series. References: 126.
  • SRV 571 Nation: USA. Spacecraft: KH-3. Agency: USAF. COSPAR: F620113B. References: 279.
1962 January 15 - Launch Vehicle: Proton. Model: Proton 8K82.
  • Proton configuration selected. Nation: USSR. Program: GR-2. Manufacturer: OKB-52. The 'polyblock' design was chosen as most advantageous, following studies that indicated improved wind loads and bending moment characteristics compared to the conventional 'monoblock' design. References: 273.
1962 January 15 -
  • Apollo Spacecraft Project Office established Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Apollo Spacecraft Project Office (ASPO) was established at MSC. Charles W. Frick was selected as Manager of the new Office, to assume his duties in February. Frick had been Chief of Technical Staff for General Dynamics Convair. Robert O. Piland was appointed Deputy Manager of ASPO and would serve as Acting Manager until Frick's arrival. ASPO would be responsible for the technical direction of NAA and other industrial contractors assigned to work on the Apollo spacecraft. Additional Details: Apollo Spacecraft Project Office established. References: 16.
1962 January 15 -
  • James A. Chamberlin named Manager of Gemini Project Office (GPO). Nation: USA. Program: Gemini. Spacecraft: Gemini. Director Robert R. Gilruth of Manned Spacecraft Center (MSC) appointed James A. Chamberlin, Chief of Engineering Division, as Manager of Gemini Project Office (GPO). The next day MSC advised McDonnell, by amendment No. 1 to letter contract NAS 9-170, that GPO had been established. It was responsible for planning and directing all technical activities and all contractor activities within the scope of the contract.
1962 January 15-17 - Launch Vehicle: Atlas. Model: Atlas D.
  • Recovery swimmers trained for Mercury MA-6. Nation: USA. Program: Mercury. Recovery area swimmers were trained at the Pensacola Naval Air Station, Florida, for use in the Mercury-Atlas 6 (MA-6) manned orbital mission. Instruction included films, briefings, auxiliary flotation collar deployment, and jumps from a helicopter. References: 483.
1962 January 15 - 11:07 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2D. LV Configuration: Thor DSV-2D 337.
  • AVT-1 Satellite test Nation: USA. Agency: USAF. Apogee: 1,400 km (800 mi). References: 2.
1962 January 16 - Launch Vehicle: Atlas. Model: Atlas D.
  • Mercury spacecraft 16 delivered to Cape Canaveral Nation: USA. Program: Mercury. Spacecraft: Mercury. Spacecraft 16 was delivered to Cape Canaveral for the third manned (Schirra) orbital flight, Mercury-Atlas 8 (MA-8). References: 483.
1962 January 16 - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150.
  • Extreme ultraviolet Mon / X-ray counter Solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1962 January 16 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1962 January 17 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1962 January 17 - 20:00 GMT - Launch Site: Mud Lake DZ. Launch Complex: -. Launch Pad: 37.9 N x 117.1 W. Launch Vehicle: X-15. LV Configuration: X-15 3-2-3.
  • X-15A MH-96. Mach 5 test Nation: USA. Agency: NASA/USAF. Apogee: 40 km (24 mi). Maximum Speed - 6058 kph. Maximum Altitude - 40690 m. References: 2.
1962 January 17 - 21:02 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 123D.
  • Operational missile test Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 January 18 - Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Korolev requests new Vostoks Nation: USSR. Program: Vostok. Spacecraft: Vostok, Vostok-Zh, Zenit-4. Korolev has issued a letter requested eight new Vostok 3A spacecraft to be built in 1962-1963. He recommends that they should be finished as the 1100 to 1300 kg heavier 'Vostok-2', to be boosted by the 11A57 rocket, developed originally for the Zenit-4 spy satellite. These Vostok-2's will be used for docking experiments, to form EO Experimental Orbital stations, and to develop spacecraft systems for flight to the moon. The VVS fully supports these plans. One of the docking spacecraft will be piloted, the other unpiloted. References: 376.
1962 January 18 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus.
  • Test mission Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
1962 January 21 - 00:57 GMT - Launch Site: Vandenberg. Launch Complex: 395-A3. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-4.
  • Demo Nation: USA. Agency: USAF SAC?. Apogee: 1,000 km (600 mi). References: 2.
1962 January 22 -
  • First Apollo engineering order issued Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The first Apollo engineering order was issued to fabricate mockups of the Apollo command and service modules. References: 16.
1962 January 23 - 17:05 GMT - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-17 (A2G-2). FAILURE: Failure.
  • Test mission Nation: USA. Agency: USN. Apogee: 0 km ( mi). References: 2.
1962 January 23 - 21:28 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 132D.
  • Operational missile test Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 January 24 - 09:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar 311 AB010. FAILURE: Failure.
  • Lofti 2 Nation: USA. Mass: 99 kg (218 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Lofti 2. Agency: U.S. Navy. COSPAR: F620124A. Decay Date: 1962-01-24. Carried 5 satellites. References: 126.
  • Solrad 4 Nation: USA. Payload: GRAB 4. Mass: 18 kg (39 lb). Class: Sigint. Spacecraft: GRAB. Agency: USAF. COSPAR: F620124B. References: 279.
  • Secor Nation: USA. Payload: Secor. Spacecraft: SECOR. Agency: USAF. COSPAR: F620124C. References: 279.
  • Injun 2 Nation: USA. Payload: Injun 2. Spacecraft: Injun. Agency: USAF. COSPAR: F620124D. References: 279.
  • Surcal Nation: USA. Payload: Surcal. Class: Calibration. Spacecraft: Surcal. Agency: USAF. COSPAR: F620124E. References: 279.
1962 January 25 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1962 January 25 - 15:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 408.
  • Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2.
1962 January 25 - 22:02 GMT - Launch Site: Point Mugu. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus.
  • PM-7 Sim target Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
1962 January 26 - Launch Vehicle: Titan. Model: Titan 2.
  • Titan II plans to ensure flight safety and enhance reliability. Nation: USA. After investigating potential malfunction problems of the modified Titan II/Gemini launch vehicle, Martin-Baltimore prepared a study report with plans to provide the components necessary to ensure flight safety and enhance reliability. Martin defined the malfunction problem quantitatively in terms of the probability of each cause and its characteristic effect on the system and vehicle. Martin intended to keep the launch vehicle as much like the weapon system as possible; thus the data obtained from the Air Force's weapon system development program would be applicable to the launch vehicle. Only minimal modifications to enhance probability of mission success, to increase pilot safety, and to accommodate the Gemini spacecraft as the payload were to be made. These included a malfunction detection system; backup guidance, control, and hydraulic systems; and selective electrical redundancies.
1962 January 26 - 20:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 121D (AA3) / Agena B 6003 (AA3). FAILURE: Agena B second stage guidance system failure.
  • Ranger 3 Nation: USA. Program: Ranger. Payload: NASA P-34 (RA-3). Mass: 327 kg (720 lb). Class: Planetary. Type: Lunar. Spacecraft: Ranger 3-4-5. Agency: NASA. COSPAR: 1962-Alpha-1. USAF Sat Cat: 221. Lunar impact probe; missed the moon by 36,874 km and went into solar orbit. A malfunction in the booster guidance system resulted in excessive spacecraft speed. Reversed command signals caused the telemetry antenna to lose earth acquisition, and mid-course correction was not possible. Some useful data were obtained from the flight. Of four scientific experiments only one was partially completed: gamma-ray readings of the lunar surface. Attempts to relay television pictures of the moon and to bounce radar signals off the moon at close range were unsuccessful. References: 2, 6, 16, 278, 296.
1962 January 27 - Launch Vehicle: Atlas. Model: Atlas D.
  • Mercury MA-6 postponed at T-minus 29 minutes Nation: USA. Program: Mercury. The Mercury-Atlas 6 (MA-6) manned orbital flight was postponed at T-minus 29 minutes due to weather conditions. References: 483.
1962 January 29 - 20:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee 200. LV Configuration: Astrobee 200 CRL AA15.109.
  • Day Airglow Test / aeronomy mission Nation: USA. Agency: USAF. Apogee: 250 km (150 mi). References: 2.
1962 January 29 - 23:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I M-7.
  • Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
1962 January 30 - Launch Vehicle: Atlas. Model: Atlas D.
  • Mercury MA-6 postponed Nation: USA. Program: Mercury. The Mercury-Atlas 6 (MA-6) mission was postponed because of technical difficulties with the launch vehicle. References: 483.
1962 January -
  • Preliminary layouts of the Apollo command module Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NAA engineers began preliminary layouts to define the elements of the command module (CM) configuration. Additional requirements and limitations imposed on the CM included reduction in diameter, paraglider compatibility, 250 pounds of radiation protection water, redundant propellant tankage for the attitude control system, and an increase in system weight and volume. Additional Details: Preliminary layouts of the Apollo command module. References: 16.
1962 January -
  • Storable liquid propellant selected for Apollo service module Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The solid propellant called for in the original NAA proposal on the service module propulsion system was replaced by a storable, hypergolic propellant. Multitank configurations under study appeared to present offloading capabilities for alternative missions. References: 16.
1962 February 1 -
  • Mercury MA-6 scheduled Nation: USA. Program: Mercury. Flight: Mercury MA-6. NASA Headquarters announced that the Mercury-Atlas 6 (MA-6) manned orbital mission would be scheduled no earlier than February 13, 1962, and that repair of the Atlas launch vehicle fuel tank leak would be completed well before that time. References: 483.
1962 February 1 -
  • Communist China and Soviet Union split in conflict over Communist ideology. Nation: China.
1962 February 1 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • 3 stage control test Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
During February 1962 - Launch Vehicle: N1, Proton, R-16, R-56, R-9, UR-200.
  • Pitsunda Conference - Decision to start design of UR-500 and N1 lunar boosters Nation: USSR. The Soviet leadership attends a secret exhibition of Soviet rocket technology in a sporting hall at Pitsunda, on the Black Sea. The Chief Designers offer competing designs. It is decided that the R-16, R-9, UR-200, UR-500, and N1 will go forward. Yangel's R-56 is rejected. Additional Details: Pitsunda Conference - Decision to start design of UR-500 and N1 lunar boosters. References: 539.
1962 February 5 - 20:58 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5C. LV Configuration: Skylark-5C SL35B.
  • Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 215 km (133 mi). References: 2.
1962 February 6 -
  • Langley presentation of lunar orbit rendezvous Nation: USA. Program: Apollo. Spacecraft: Apollo LM. John C. Houbolt of Langley Research Center and Charles W. Mathews of MSC made a presentation of lunar orbit rendezvous versus earth orbit rendezvous to the Manned Space Flight Management Council. References: 16.
1962 February 7 -
  • Kennedy comments on moon program Nation: USA. Program: Apollo. At his regular press conference, President John F. Kennedy was asked for his "evaluation of our progress in space at this time" and whether the United States had changed its "timetable for landing a man on the moon." He replied: "As I said from the beginning, we have been behind . . . and we are running into the difficulties which came from starting late, We, however, are going to proceed by making a maximum effort. As you know, the expenditures in our space program are enormous . . . the time schedule, at least our hope, has not been changed by the recent setbacks (Ranger failures)." References: 16.
1962 February 7 -
  • Single-engine design for the Apollo service module Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. On the basis of a study by NAA, a single-engine configuration was chosen as the optimum approach for the service module propulsion subsystem. The results of the study were presented to MSC representatives and NAA was authorized to issue a work statement to begin procurement of an engine for this configuration. Agreement was also reached at this meeting on a vacuum thrust level of 20,000 pounds for the engine. This would maintain a thrust-to-weight ratio of 0.4 and allow a considerable increase in the lunar liftoff weight of the spacecraft. References: 16.
1962 February 7 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus.
  • Test mission Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
1962 February 7 - 11:50 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.16AI.
  • Ionosphere mission Nation: USA. Agency: NASA. Apogee: 960 km (590 mi). References: 2.
1962 February 8 - 12:43 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta. LV Configuration: Thor Delta 317/D7.
  • Tiros 4 Nation: USA. Program: Tiros. Payload: Tiros D (A-9). Mass: 129 kg (284 lb). Class: Earth. Type: Weather. Spacecraft: Tiros. Agency: NASA. Perigee: 693 km (430 mi). Apogee: 812 km (504 mi). Inclination: 48.30 deg. Period: 99.90 min. COSPAR: 1962-Beta-1. USAF Sat Cat: 226. Returned 32593 cloud cover photos. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6.
1962 February 9 -
  • General Electric selected for Apollo support Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NASA announced that the General Electric Company had been selected for a major supporting role in the Apollo project, to provide integration analysis of the total space vehicle (including booster-spacecraft interface), ensure reliability of the entire space vehicle, and develop and operate a checkout system. References: 16.
1962 February 10 -
  • Sever spacecraft trials Nation: USSR. Spacecraft: Sever. Two officers start a 15 day test aboard a mock-up of the Sever spacecraft, but without the participation of the IAKM. The whole thing was planned by Voronin's OKB in GKNII. References: 376.
1962 February 11 - Launch Site: Kapustin Yar. Launch Complex: silo. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: R-14U.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 675 km (419 mi). References: 2.
1962 February 12 - Launch Site: Point Mugu. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. FAILURE: Failure.
  • PM-8 Dummy St 3? Nation: USA. Agency: USA. Apogee: 10 km (6 mi). References: 2.
1962 February 13 -
  • Contract for Apollo launch escape system rocket Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A contract for the escape rocket of the Apollo spacecraft launch escape system was awarded to the Lockheed Propulsion Company by NAA. The initial requirements were for a 200,000-pound-thrust solid- propellant rocket motor with an active thrust-vector-control subsystem. Additional Details: Contract for Apollo launch escape system rocket. References: 16.
1962 February 13 - 20:55 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 40E.
  • Research and development test Nation: USA. Agency: USAF. Apogee: 1,600 km (900 mi). Last Atlas E R&D flight. References: 2.
1962 February 14 - Launch Vehicle: Atlas. Model: Atlas D.
  • Mercury MA-6 postponed. Nation: USA. Program: Mercury. Unfavorable weather conditions caused the Mercury-Atlas 6 (MA-6) manned orbital mission to be postponed. References: 483.
1962 February 15 - Launch Vehicle: Titan. Model: Titan 2.
  • Aerospace Corporation to support of the Gemini Launch Vehicle Program. Nation: USA. Air Force Space Systems Division issued a Technical Operating Plan to Aerospace Corporation, El Segundo, California, for support of the Gemini Launch Vehicle Program; a contract followed on March 15. Aerospace was to assume responsibility for general systems engineering and technical direction of the development of the launch vehicle and its associated subsystems. Aerospace had already established a Gemini Launch Vehicle Program Office in January.
1962 February 15 - 15:35 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 410.
  • Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2.
1962 February 16 -
  • Delay of Mercury MA-6 schedule Nation: USA. Program: Mercury. Walter C. Williams, Project Mercury Operations Director, announced that because of weather conditions February 20, 1962, would be the earliest date that the Mercury-Atlas 6 mission could be launched. References: 483.
1962 February 16 -
  • Female Cosmonaut Training Group selected. Nation: USSR. The group was selected to provide female astronauts for the Vostok manned spaceflight program.. Qualifications: Parachutists under 30 years of age; under 170 cm tall; under 70 kg in weight.. Cosmonaut commander Nikolai Kamanin obtained official approval to train a cadre of female cosmonauts in October 1961. The pool of Soviet female pilots being limited, potential candidates were also sought who were active sport parachutists. Five Soviet women were selected on 16 February 1962 and reported for training a month later. However the flight of a woman in space had little support from Chief Designer Korolev or Kamanin's military commanders.

    In May 1962 a Soviet delegation, including cosmonaut Gherman Titov and Kamanin, visited Washington. On May 3 Kamanin and Titov were invited to a barbecue at the home of astronaut John Glenn. Glenn, already politically-connected, was an enthusiastic supporter of the 'Mercury 13' - female pilots who had passed the astronaut physical and were lobbying to be trained as Mercury astronauts. Kamanin understood from Glenn that the first American woman would make a three-orbit Mercury flight by the end of 1962. Armed with the threat that 'the Americans will beat us', Kamanin was able to obtain a decision to go ahead with the first flight of a Soviet woman within weeks of his return.

    Meanwhile the five female cosmonaut were going through the complete course of cosmonaut training, including weightless flights, parachute jumps, isolation tests, centrifuge tests, and academic studies of rocket theory and spacecraft engineering. The women undertook 120 parachute jumps and received pilot training in MiG-15UTI jet trainers.

    Even though NASA's female astronaut flight never materialised, Valentina Tereshkova of the Soviet Union became the first woman in space on June 16, 1963. Following her flight the women were enrolled in the arduous test pilot course at the Zhukovskiy Academy (except Ponomareva, who was a graduate engineer from the Moscow Aviation Institute). There were plans for all-female Vostok or Soyuz flights, but these never materialised. The female training group was disbanded in October 1969. The Soviet Union used only male cosmonauts until the 1980's, when women were again recruited, in order to again have a Soviet woman in space before the Americans finally began flying female astronauts on the space shuttle.

1962 February 16 - 23:04 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 137D.
  • Operational missile test Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 February 17 -
  • Immediate Vostok launches demanded Nation: USSR. Program: Vostok. Flight: Vostok 3, Vostok 4. Ustinov wants launch of two cosmonauts within a month to answer the American Glenn flight. Of seven candidates, Nikolayev and Popovich are most likely to be selected. Meanwhile Titov has more incidents. He has driven his Volga into a bus. This is his third accident within a year. References: 376.
1962 February 17 - 19:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.41NP.
  • LeRC LH2 test Technology test Nation: USA. Agency: NASA. Apogee: 157 km (97 mi). References: 2.
1962 February 18 - Launch Vehicle: Atlas. Model: Atlas D.
  • NASA announced Project Fire Nation: USA. Program: Apollo. Spacecraft: FIRE. NASA announced Project Fire, a high-speed reentry heat research program to obtain data on materials, heating rates, and radio signal attenuation on spacecraft reentering the atmosphere at speeds of about 24,500 miles per hour. Information from the program would support technology for manned and unmanned reentry from lunar missions. Under the management of the Langley Research Center, Project Fire would use Atlas D boosters and the reentry package would be powered by an Antares solid-fuel motor (third stage of the Scout). References: 16.
1962 February 20 -
  • Vostok 3/4 training Nation: USSR. Program: Vostok. Flight: Vostok 3, Vostok 4. Kamanin selects the cosmonauts for the dual flight ordered by Ustinov: Nikolayev and Popovich, with Nelyubov and Bykovsky as back-ups. Ustinov has ordered launch by 10-12 March. - such is the Soviet's lousy leadership, Kamanin notes. They don't do anything for months, then suddenly want a manned launch within 10 days. Korolev wants a three-day flight, but the VVS wants no more than two days, and only then if the cosmonauts are in excellent condition after the first day. References: 376.
1962 February 20 - 13:28 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.90UA.
  • Composition Aeronomy mission Nation: USA. Agency: NASA. Apogee: 132 km (82 mi). References: 2.
1962 February 20 - 14:47 GMT - Launch Site: Cape Canaveral. Launch Complex: LC14. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 109D.
  • Mercury MA-6 Nation: USA. Program: Mercury. Payload: Mercury SC13. Mass: 1,355 kg (2,987 lb). Class: Manned. Type: Spacecraft. Spacecraft: Mercury. Location of Spacecraft: National Air and Space Museum (Smithsonian Institution), Washington, DC. Agency: NASA. Perigee: 159 km (98 mi). Apogee: 265 km (164 mi). Inclination: 32.50 deg. Period: 88.60 min. COSPAR: 1962-Gamma-1. USAF Sat Cat: 240. Duration: 0.21 days. Decay Date: 1962-02-20. Crew: Glenn. Flight: Mercury MA-6. First US manned orbital mission. John Glenn finally puts America in orbit. False landing bag deploy light led to reentry being started with retropack left in place on heat shield. It turned out that indicator light was false and a spectacular reentry ensued, with glowing chunks of the retropack whizzing by the window. After four hours and 43 minutes the spacecraft reentered the atmosphere and landed at 2:43 pm EST in the planned recovery area NE of the Island of Puerto Rico. All flight objectives were achieved. Glenn was reported to be in excellent condition. Beause of failure of one of the automatic systems, the astronaut took over manual control of the spacecraft during part of the flight. With this flight, the basic objectives of Project Mercury had been achieved. References: 2, 6, 26, 33, 59, 60, 278.
1962 February 21 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: RAM. Model: RAM A. LV Configuration: RAM A RAM A-2.
  • RAM A-2 re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 1,000 km (600 mi). References: 2.
1962 February 21 - 18:44 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 332 / Agena B 2301. FAILURE: Partial failure. Agena failed to restart to circularize orbit.
  • Ferret 1 Nation: USA. Payload: Ferret 1 / Agena B 2301. Mass: 1,500 kg (3,300 lb). Class: Sigint. Spacecraft: Ferret. Agency: U.S. Air Force. Perigee: 169 km (105 mi). Apogee: 219 km (136 mi). Inclination: 81.90 deg. Period: 88.30 min. COSPAR: 1962-Delta-1. USAF Sat Cat: 242. Decay Date: 1962-03-04. References: 2, 6.
1962 February 21 - 22:30 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 52D. FAILURE: Failure.
  • Operational missile test Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 February 22 - Launch Vehicle: Titan. Model: Titan 2.
  • Proposal for redundant subsystems for the Gemini launch vehicle. Nation: USA. Spacecraft: Gemini. Martin-Baltimore submitted its initial proposal for the redundant flight control and hydraulic subsystems for the Gemini launch vehicle; on March 1, Martin was authorized to proceed with study and design work. The major change in the flight control system from Titan II missile to Gemini launch vehicle was substitution of the General Electric Mod IIIG radio guidance system (RGS) and Titan I three-axis reference system for the Titan II inertial guidance system. Air Force Space Systems Division issued a letter contract to General Electric Company, Syracuse, New York, for the RGS on June 27. Technical liaison, computer programs, and ground-based computer operation and maintenance were contracted to Burroughs Corporation, Paoli, Pennsylvania, on July 3.
1962 February 23 -
  • Dyna-Soar limited to an orbital research system. Nation: USA. Spacecraft: Dynasoar. Secretary of Defense, Robert S. McNamara, officially limited the objective of the Dyna-Soar program to the development of an orbital, research system. Now it is only a research and development program to demonstrate re-entry and landing of a spaceplane.
1962 February 23 - Launch Site: Vandenberg. Launch Complex: 395-A1. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-18. FAILURE: Failure.
  • Research and development Cat II / operational test Nation: USA. Agency: USAF AFSC. Apogee: 50 km (31 mi). References: 2.
1962 February 24 - Launch Site: Sea-launched. Launch Complex: -. Launch Pad: UNKPL. Launch Vehicle: R-21.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 293 km (182 mi). References: 2.
1962 February 25 - Launch Vehicle: Atlas. Model: Atlas D.
  • Factory roll-out inspection of Mercury Atlas launch vehicle 107-D. Nation: USA. Program: Mercury. Flight: Mercury MA-7. Factory roll-out inspection of Atlas launch vehicle 107-D, designated for the Mercury-Atlas 7 (MA-7) manned orbital mission, was conducted at Convair. References: 483.
1962 February 26 -
  • John Glenn Day in Washington, D.C. Nation: USA. Program: Mercury. This featured the reception of the astronaut at the White House, a parade, and his address to joint session of Congress. References: 483.
1962 February 27 - 19:39 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 241 / Agena B 1123.
  • Discoverer 38 Nation: USA. Payload: KH-4 s/n 9031 / Agena B 1123. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 207 km (128 mi). Apogee: 277 km (172 mi). Inclination: 82.20 deg. Period: 89.40 min. COSPAR: 1962-Epsilon-1. USAF Sat Cat: 247. Decay Date: 1962-03-21. First mission of the KH-4 series. Much of film slightly out of focus.. Capsule recovered 4.1 days later. References: 2, 6.
1962 February - Launch Vehicle: Little Joe.
  • Little Joe dropped for Apollo tests Nation: USA. Program: Apollo. NASA wind tunnel data on the adaptation of the Project Mercury Little Joe booster to the Apollo launch escape system were analyzed. The booster fins were ineffective in maintaining the stability of the configuration and the project was canceled. The later Little Joe II depended on the inherent stability of the total vehicle to attain a successful ballistic trajectory to test altitude. References: 16.
1962 March 1 -
  • Chance Vought to study spacecraft rendezvous Nation: USA. Program: Apollo. Spacecraft: Apollo LM. NASA Headquarters selected the Chance Vought Corporation of Ling-Temco-Vought, Inc., as a contractor to study spacecraft rendezvous. A primary part of the contract would be a flight simulation study exploring the capability of an astronaut to control an Apollo-type spacecraft. References: 16.
1962 March 1 -
  • 4 million New Yorkers greet Glenn Nation: USA. Program: Mercury. An estimated 4 million people lined the streets of New York City for John Glenn Day. Mayor Robert Wagner presented Glenn and Robert R. Gilruth the city's Medal of Honor. References: 483.
1962 March 1 -
  • Plans for astronaut/cosmonaut meeting Nation: USSR. Glenn is in Washington, and meets the Secretary General of the United Nations, who mentions a plan of the Soviet ambassador to the UN. Gagarin and Titov might visit New York to address the United Nations on 19 March. This would provide an opportunity for the cosmonauts and US astronauts to meet. References: 376.
1962 March 1 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: RT-1. FAILURE: Failure.
  • Nation: USSR. Agency: RVSN. Apogee: 10 km (6 mi). References: 2.
1962 March 1 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-27 (A2G-5).
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 March 1 - 00:14 GMT - Launch Site: Vandenberg. Launch Complex: OSTF1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 66E.
  • Research and development Category II test Nation: USA. Agency: USAF. Apogee: 1,600 km (900 mi). References: 2.
1962 March 1 - 05:07 GMT - Launch Site: Wallops Island. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-1A. LV Configuration: Scout X-1A ST-8.
  • Reentry 1 re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 214 km (132 mi). References: 2.
1962 March 1 - 17:07 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AA6.167.
  • 7-inch Sphere Aeronomy mission Nation: USA. Agency: USAF. Apogee: 144 km (89 mi). References: 2.
1962 March 1 - 23:23 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.100CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 135 km (83 mi). References: 2.
1962 March 2 -
  • Marquardt to build the reaction control rocket engines for the Apollo spacecraft Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Marquardt Corporation was selected by NAA's Space and Information Systems Division to design and build the reaction control rocket engines for the Apollo spacecraft. The contract was signed during April. References: 16.
1962 March 2 - 00:05 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.38GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 113 km (70 mi). References: 2.
1962 March 2 - 10:47 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.70GT.
  • Water test Nation: USA. Agency: NASA. Apogee: 145 km (90 mi). References: 2.
1962 March 2 - 10:54 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.101CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 134 km (83 mi). References: 2.
1962 March 2 - 11:15 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.39GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 115 km (71 mi). References: 2.
1962 March 3 -
  • Aerojet-General named for the Apollo service module propulsion system Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Aerojet-General Corporation was named by NAA as a subcontractor for the Apollo service module propulsion system. References: 16.
1962 March 5 -
  • Vostok 3/4 delayed Nation: USSR. Program: Vostok. Spacecraft: Zenit-2. Flight: Vostok 3, Vostok 4. Due to technical problems and the launch failure of a Zenit spy satellite, the launch of the dual Vostoks is pushed back to April. Therefore a trip to New York by the cosmonauts in March will not be possible. In any case the Presidium has decided against allowing them to address the United Nations. References: 376.
1962 March 5 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • KMR-2 Sim target Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
1962 March 5 - 09:55 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL66.
  • Grenades / Chaff / Sodium release Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 233 km (144 mi). References: 2.
1962 March 6 - Launch Vehicle: Atlas. Model: Atlas D.
  • Mercury Atlas launch vehicle 107-D delivered to Cape Canaveral Nation: USA. Program: Mercury. Atlas launch vehicle 107-D was delivered to Cape Canaveral for the Mercury-Atlas 7 (MA-7) mission. References: 483.
1962 March 6 - 12:35 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL160.
  • Grenades / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 173 km (107 mi). References: 2.
1962 March 6 - 13:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AB3.150.
  • Ultraviolet Absorption Aeronomy mission Nation: USA. Agency: USAF. Apogee: 323 km (200 mi). References: 2.
1962 March 7 -
  • Orbiting Solar Observatory (OSO) Nation: USA. Program: Mercury. The first Orbiting Solar Observatory (OSO) performed remarkably well in conducting the thirteen different experiments for which it was programmed. Especially relevant to manned space flight were its measurements of solar radiation in high frequency ranges, of cosmic dust effects, and of the thermal properties of spacecraft surface materials. References: 483.
1962 March 7 - 16:06 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta. LV Configuration: Thor Delta 301/D8.
  • OSO 1 Nation: USA. Payload: OSO A (S-16). Mass: 208 kg (458 lb). Class: Solar. Spacecraft: OSO. Agency: NASA. Perigee: 522 km (324 mi). Apogee: 553 km (343 mi). Inclination: 32.80 deg. Period: 95.30 min. COSPAR: 1962-Zeta-1. USAF Sat Cat: 255. Decay Date: 1981-10-08. Orbiting Solar Observatory; solar flare observations. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1962 March 7 - 22:10 GMT - Launch Site: Vandenberg. Launch Complex: SLC3E. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 112D / Agena B 2204.
  • Samos 6 Nation: USA. Payload: Samos E-5 no. 3. Mass: 1,860 kg (4,100 lb). Class: Surveillance. Type: Military. Spacecraft: Samos. Agency: U.S. Air Force. Perigee: 236 km (146 mi). Apogee: 686 km (426 mi). Inclination: 90.90 deg. Period: 93.90 min. COSPAR: 1962-Eta-3. USAF Sat Cat: 259. Decay Date: 1963-06-07. First generation photo surveillance; return of camera and film by capsule; SAMOS type satellite. Failed to return camera and film. Samos film return project cancelled; remaining 4 cameras placed in warehouse and later used on KH-6 Lanyard. References: 2, 6, 278.
1962 March 8 -
  • Contract for the Apollo spacecraft fuel cell to Pratt & Whitney Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NAA awarded a development contract for the Apollo spacecraft fuel cell to Pratt & Whitney Aircraft Division of United Aircraft Corporation. References: 16.
1962 March 8 - 15:24 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 409.
  • Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2.
1962 March 10 -
  • Soyuz Technical Project approved. Nation: USSR. Spacecraft: L1-1962, Vostok-Zh, OS-1962. Korolev approved the technical project 'Complex docking of spacecraft in earth orbit - Soyuz'. The Soyuz would first be tested using multiple launches of an R-7 derived rocket. In this concept a large spacecraft was assembled in earth orbit by a Vostok-Zh (or Vostok-7) manoeuvrable manned satellite, piloted by a 'cosmonaut assemblyman'. Following completion of assembly, the Vostok would return to earth. The assembled circumlunar craft would put the L1, with a crew of one to three, on a circumlunar trajectory. The Vostok-Zh could be used on another mission to assemble a 15 tonne OS orbital station with the mission of observing the earth.
1962 March 12 -
  • Apollo program moved to Houston Nation: USA. Program: Apollo. Primary MSC activities for the Apollo program were relocated from Langley Field, Va., to the Manned Spacecraft Center, Houston, Tex. References: 16.
1962 March 13 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Simulated target Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
1962 March 13 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Simulated target Nation: USA. Agency: USA. Apogee: 150 km (90 mi). References: 2.
1962 March 14 - Launch Site: Vandenberg. Launch Complex: LC-B. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Asp IV.
  • Vista-300 test Nation: USA. Agency: USN. Apogee: 150 km (90 mi). References: 2.
1962 March 15 - Launch Vehicle: Atlas. Model: Atlas D.
  • Carpenter replaces Slayton on Mercury-Atlas 7 (MA-7) Nation: USA. Program: Mercury. Flight: Mercury MA-7. NASA Headquarters publicly announced that Scott Carpenter would pilot the Mercury-Atlas 7 (MA-7) manned orbital mission replacing Donald Slayton. The latter, formerly scheduled for the flight, was disqualified because of a minor erratic heart rate. References: 483.
1962 March 16 - 11:59 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. LV Configuration: Kosmos 63S1 6LK.
  • Cosmos 1 Nation: USSR. Program: DS. Payload: DS-2 s/n 2. Mass: 47 kg (103 lb). Class: Technology. Spacecraft: DS-2. Agency: RVSN. Perigee: 207 km (128 mi). Apogee: 649 km (403 mi). Inclination: 49.00 deg. Period: 93.10 min. COSPAR: 1962-Theta-1. USAF Sat Cat: 266. Completed Operations Date: 1962-03-26. Decay Date: 1962-05-25. After five months of further work and tests to improve the reliability of the second stage, Yangel's team felt it was ready to again attempt a launch of the 63S1 booster. 63S1 s/n 6LK put a DS-2 satellite into orbit, which conducted studies of the ionosphere. This was the first successful launch of the Kosmos 63S1 launch vehicle. A decision was made after two unsuccessful launches of the DS-1 to create a simplified DS-2 spacecraft based on the equipment and structural elements of DS-1 spacecraft. The cylindrical section for mission avionics was completely omitted. References: 2, 6, 99.
1962 March 16 - 18:09 GMT - Launch Site: Cape Canaveral. Launch Complex: LC16. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-2.
  • Mk 6 re-entry vehicle test launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). The Air Force successfully launched a Titan II intercontinental ballistic missile. This was the first full-scale test of the vehicle; it flew 8000 km out over the Atlantic Ocean. References: 2.
1962 March 18 - Launch Vehicle: Saturn V.
  • Saturn C-5 first launch scheduled in the last quarter of 1965 Nation: USA. Program: Apollo. Marshall Space Flight Center's latest schedule on the Saturn C-5 called for the first launch in the last quarter of 1965 and the first manned launch in the last quarter of 1967. If the C-5 could be man-rated on the eighth research and development flight in the second quarter of 1967, the spacecraft lead time would be substantially reduced. References: 16.
1962 March 19 - 11:04 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL161.
  • Grenades / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 140 km (80 mi). References: 2.
1962 March 19 - 23:28 GMT - Launch Site: Vandenberg. Launch Complex: SLC10E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 229.
  • Combat training launch Nation: USA. Agency: RAF. Apogee: 520 km (320 mi). References: 2.
1962 March 21 - Launch Vehicle: Titan. Model: Titan 2.
  • Contract to Aerojet-General for 15 propulsion systems for the Gemini launch vehicle. Nation: USA. Air Force Space Systems Division awarded a letter contract to Aerojet-General Corporation, Azusa, California, for the research, development, and procurement of 15 propulsion systems for the Gemini launch vehicle. It also included the design and development of the related aerospace ground equipment. Aerojet had been authorized to go ahead with work on the engines on February 14, 1962, and the final engine was scheduled for delivery by April 1965.
1962 March 21 - Launch Site: Jiuquan. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: DF-2. Model: DF-2. FAILURE: Failure of guidance and engine mounting. Impacted after 69 seconds of flight.
  • Nation: China. Agency: PRC. Apogee: 0 km ( mi). First DF-2 launch attempt. The rocket impacted the earth after only 69 seconds of flight. Fundamental design errors were discovered in calculating flexing of the rocket in flight, placement of the guidance system, and engine mounting. The missile was completely redesigned for reduced thrust. References: 2.
1962 March 21 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-9. Model: Romashka. FAILURE: Failure.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1962 March 23 - Launch Vehicle: Titan. Model: Titan 2.
  • Air Force Space Systems Division published the "Development Plan for the Gemini Launch Vehicle System". Nation: USA. From experience in Titan II and Mercury programs, the planners estimated a budget of $164.4 million, including a 50 percent contingency for cost increases and unforeseen changes.
1962 March 23 -
  • Luna E-6 soft lander approved. Nation: USSR. Spacecraft: Luna E-6. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On Luna spacecraft for soft-landing on the Moon' was issued. References: 474.
1962 March 23 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 411.
  • Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2.
1962 March 23 - 23:44 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.102CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 142 km (88 mi). References: 2.
1962 March 23 - 23:54 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.40GA.
  • Grenade, Inflating Sphere 3 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 121 km (75 mi). References: 2.
1962 March 24 - 00:39 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 134D.
  • Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). President John F. Kennedy visited Vandenberg AFB and witnessed the launch of Atlas 134D. References: 2.
1962 March 25-31 - Launch Vehicle: Little Joe II.
  • Little Joe II test launch vehicle development approved Nation: USA. Program: Apollo. NASA Headquarters approved plans for the development of the Little Joe II test launch vehicle. Prospective bidders were notified of a briefing to be held at MSC on April 6, at which time Requests for Proposals would be distributed. References: 16.
1962 March 26 - 19:03 GMT - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Caleb. LV Configuration: Caleb NC17.121. FAILURE: Failure.
  • Test / aeronomy mission Nation: USA. Agency: USN NOTS. Apogee: 21 km (13 mi). References: 2.
1962 March 27 - 23:48 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.103CA.
  • Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi). References: 2.
1962 March 28 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Hercules intercept Nation: USA. Agency: USA. Apogee: 40 km (24 mi). References: 2.
1962 March 28 - 00:03 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.41GA.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 123 km (76 mi). References: 2.
1962 March 29 -
  • Chance Vought briefed on lunar orbit rendezvous Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Members of Langley Research Center briefed representatives of the Chance Vought Corporation of Ling- Temco-Vought, Inc., on the lunar orbit rendezvous method of accomplishing the lunar landing mission. The briefing was made in connection with the study contract on spacecraft rendezvous awarded by NASA Headquarters to Chance Vought on March 1. References: 16.
1962 March 29 -
  • Republic to build two experimental FIRE spacecraft Nation: USA. Program: Apollo. Spacecraft: FIRE. NASA announced that a $5 million contract would be awarded to Republic Aviation Corporation for the construction of two experimental reentry spacecraft. Republic was selected from eight companies that submitted bids on March 12. The contract was part of Project Fire, to develop a spacecraft capable of withstanding reentry into the earth's atmosphere from a lunar mission. Plans called for the spacecraft to be tested during the second half of 1963. References: 16.
1962 March 29 - 07:27 GMT - Launch Site: Wallops Island. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-2. LV Configuration: Scout X-2-1C ST-9.
  • P-21A Plasma / aeronomy mission Nation: USA. Agency: NASA. Apogee: 6,291 km (3,909 mi). References: 2.
1962 March 29 - 09:28 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 105.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 125 km (77 mi). References: 2.
1962 March 30 - Launch Vehicle: Titan. Model: Titan 2.
  • Martin-Baltimore submitted a "Description of the Launch Vehicle for the Gemini Spacecraft" to Air Force Space Systems Division. Nation: USA. This document laid the foundation for the design of the Gemini launch vehicle by defining the concept and philosophy of each proposed subsystem.
1962 March 30 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-28 (A2M-3). FAILURE: Failure.
  • Test mission Nation: USA. Agency: USN. Apogee: 0 km ( mi). References: 2.
1962 March 31 -
  • The configuration of the Gemini spacecraft was formally frozen. Nation: USA. Program: Gemini. Spacecraft: Gemini. Following receipt of the program go-ahead on December 22, 1961, McDonnell began defining the Gemini spacecraft. At that time, the basic configuration was already firm. During the three-month period, McDonnell wrote a series of detailed specifications to define the overall vehicle, its performance, and each of the major subsystems. These were submitted to NASA and approved. During the same period, the major subsystems specification control drawings - the specifications against which equipment was procured - were written, negotiated with NASA, and distributed to potential subcontractors for bid.

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