1962 July 1 - -
Kennedy Space Center founded. Nation: USA.
1962 July 1 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 1017. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Successful missile test. Missed aimpoint by 390 m. References: 2.
1962 July - -
Hamilton Standard to develop the Apollo space suit Nation: USA. Program: Apollo. Spacecraft: A7L. Hamilton Standard Division of United Aircraft Corporation selected by NASA to develop the Apollo space suit. References: 16.
1962 July - Launch Vehicle: UR-200. -
Kosmoplan and UR-200 draft projects completed. Nation: USSR. Spacecraft: US-A, IS-A, Kosmoplan. Trial flights of the ICBM version ran from 4 November 1963 to 20 October 1964. Versions of the Kosmoplan would fly as the reactor-powered US-A and solar-powered US-P ELINT satellites and the I2P ASAT.
1962 Q3 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Berenice. LV Configuration: Berenice 003. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 270 km (160 mi). References: 2.
Last half 1962 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: RT-1. FAILURE: Failure. -
Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2.
Last half 1962 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: RT-1. FAILURE: Failure. -
Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2.
1962 July 5 - 03:46 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5. LV Configuration: Skylark-5 SL164. -
Grenades / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 111 km (68 mi). References: 2.
1962 July 6 - Launch Vehicle: Titan. Model: Titan 2. -
Martin prepared a plan for flight testing the malfunction detection system (MDS) for the Gemini launch vehicle on development flights of the Titan II weapon system. Nation: USA. Gemini Project Office (GPO) had requested Martin to prepare Systems Division and Aerospace approved the plan and won GPO concurrence early in August. This so-call 'piggyback plan' required installing the Gemini MDS in Titan II engines on six Titan II flights to demonstrate its reliability before it was flown on Gemini.
1962 July 6 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Berenice. LV Configuration: Berenice 002. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 270 km (160 mi). References: 2.
1962 July 8 - -
Operation Dominic Nation: USA. Controversial Operation Dominic succeeded, after two previous attempts in June, in exploding a megaton-plus hydrogen device at more than 200-mile altitude over Johnston Island in the Pacific. Carried aloft by a Thor rocket and synchronized with the approach of a TRAAC satellite, this highest thermonuclear blast ever achieved was designed to test the influence of such an explosion on the Van Allen radiation belts. The sky above the Pacific Ocean from Wake Island to New Zealand was illuminated by the blast. Later observations by probes and satellites showed another artificial radiation belt to have been created by this series of nuclear tests.
References: 483.
1962 July 8 - Launch Vehicle: Soyuz. Model: Molniya 8K78L. -
Molniya 8K78L preliminary design completed Nation: USSR. The Molniya 8K78L was designed by Korolev's design bureau for launching a manned spacecraft on a flyby of the Moon and return to earth. To achieve this it would have used Lox/LH2 engines in the third and fourth stages. Such technology was years away in the Soviet Union and the project was not pursued further.
1962 July 9 - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Journeyman. -
Magnetosphere mission Nation: USA. Agency: AEC. Apogee: 1,500 km (900 mi). References: 2.
1962 July 9 - Launch Site: Johnston Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin J1. -
Thermal electrons Ionosphere mission Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). References: 2.
1962 July 9 - Launch Site: Johnston Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin J2. -
Thermal electrons Ionosphere mission Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). References: 2.
1962 July 9 - 08:46 GMT - Launch Site: Johnston Island. Launch Complex: LE1. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2E. LV Configuration: Thor DSV-2E 195. -
STARFISH PRIME Nuclear test Nation: USA. Agency: USAF. Apogee: 400 km (240 mi). Successful high-altitude test of a Thor IRBM with a live nuclear warhead. The payload included test instrumentation and a W-49 warhead/Mk-4 re-entry vehicle. The 1.45 megaton bomb exploded at an altitude of 400 km. The explosion was visible 2,600 km away, at Kwajalein Atoll; an artificial aurora lasted seven minutes. The unforeseen and most militarily significant effect was the electromagnetic pulse (EMP) generated by the test. This caused power mains surges in Oahu, knocking out street lights, blowing fuses and circuit breakers, and triggering burglar alarms (and this in the days before microelectronics). The explosion supercharged the Van Allen radiation belts, resulting in several satellites malfunctioning.
References: 2.
1962 July 9 - 08:59 GMT - Launch Site: Johnston Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Nike. LV Configuration: HJ Nike X-3. FAILURE: Failure. -
Ionosphere mission Nation: USA. Agency: USAF. Apogee: 0 km ( mi). References: 2.
1962 July 9 - 09:08 GMT - Launch Site: Johnston Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Nike. LV Configuration: HJ Nike X-4. -
Ionosphere mission Nation: USA. Agency: USAF. Apogee: 100 km (60 mi). References: 2.
1962 July 10 - -
First Apollo mockup inspection Nation: USA. Program: Apollo. The first Apollo spacecraft mockup inspection was held at NAA's Space and Information Systems Division. In attendance were Robert R. Gilruth, Director, MSC; Charles W. Frick, Apollo Program Manager, MSC; and Astronaut Virgil I. Grissom. References: 16.
1962 July 10-11 - -
Apollo atmosphere to be pure oxygen Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. At the monthly Apollo spacecraft design review meeting with NAA, MSC officials directed NAA to design the spacecraft atmospheric system for 5 psia pure oxygen. From an engineering standpoint, the single-gas atmosphere offered advantages in minimizing weight and leakage, in system simplicity and reliability, and in the extravehicular suit interface.
Additional Details: Apollo atmosphere to be pure oxygen. References: 16.
1962 July 10 - 08:35 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta. LV Configuration: Thor Delta 316/D11. -
Telstar 1 Nation: USA. Mass: 77 kg (169 lb). Class: Communications. Spacecraft: Telstar. Agency: ATT. Perigee: 945 km (587 mi). Apogee: 5,643 km (3,506 mi). Inclination: 44.80 deg. Period: 157.80 min. COSPAR: 1962-A-Epsilon-1. USAF Sat Cat: 340. First commercial comsat; active repeater. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6.
1962 July 10 - 15:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.47NP. -
Radar test Technology test Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). References: 2.
1962 July 11 - Launch Vehicle: Nova, Saturn I, Saturn V. -
Selection of LOR as Apollo Mission Mode Nation: USA. Program: Apollo. Class: Manned. Spacecraft: Apollo Lunar Landing. Following a long controversy NASA selected Lunar Orbit Rendezvous (LOR) as the fastest, cheapest, and safest mode to accomplish the Apollo mission. LOR solved the engineering problem of how to land. The EOR or Direct Landing approaches required the Apollo crew to be on their backs during the landing and having to use television or mirrors to see the lunar surface. A lunar crasher stage approach had finally emerged as lesser of evils but raised other issues. LOR allowed a purpose-built lander with a logical helicopter-like crew station layout. Studies indicated LOR would allow landing 6-8 months earlier and cost $9.2 billion vs $ 10.6 billion for EOR or direct. Direct flight by this time would not involve Nova, but a scaled-down two-man spacecraft that could be launched by the Saturn C-5.
Additional Details: Selection of LOR as Apollo Mission Mode. References: 26, 27.
1962 July 11 - -
Project Apollo to use lunar orbit rendezvous. Nation: USA. Program: Apollo. NASA officials announced the basic decision for the manned lunar exploration program that Project Apollo shall proceed using the lunar orbit rendezvous as the prime mission mode. Based on more than a year of intensive study, this decision for the lunar orbit rendezvous (LOR), rather than for the alternative direct ascent or earth orbit rendezvous modes, enables immediate planning, research and development, procurement, and testing programs for the next phase of space exploration to proceed on a firm basis.
References: 483.
1962 July 11 - 18:51 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-6. -
Mk 6 re-entry vehicle test launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1962 July 12 - Launch Vehicle: Titan. Model: Titan 2. -
Gemini-Titan Launch Operations Committee. Nation: USA. A technical team at Air Force Missile Test Center, Cape Canaveral, Florida - responsible for detailed launch planning, consistency of arrangements with objectives, and coordination - met for the first time with official status and a new name. The group of representatives from all organizations supplying major support to the Gemini-Titan launch operations, formerly called the Gemini Operations Support Committee, was now called the Gemini-Titan Launch Operations Committee.
1962 July 12 - 16:57 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 141D. -
NTMP K-2 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 July 12 - 18:35 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-11. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 July 12 - 20:05 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-10. -
Operational Test - Flight over 80 minutes Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 July 13 - Launch Site: Baikonur. Launch Complex: LC60/8. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. FAILURE: Failure. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). References: 2.
1962 July 13 - 21:11 GMT - Launch Site: Vandenberg. Launch Complex: OSTF1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 67E. FAILURE: Failure. -
Research and development Category II test Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi). References: 2.
1962 July 15 - Launch Vehicle: UR-200. -
UR-200 draft project is completed. Nation: USSR. Manufacturer: OKB-52. References: 273.
1962 July 16 - 22:09 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 1-31-52. FAILURE: Power trips. -
X-15A Notch/ASAS/Aero drag test Nation: USA. Agency: NASA/USAF. Apogee: 32 km (19 mi). Maximum Speed - 5911 kph. Maximum Altitude - 32670 m. References: 2.
1962 July 17 - -
Nuclear blasts to clear inner radiation belts for Apollo Nation: USA. Program: Apollo. In an address to the American Rocket Society lunar missions meeting in Cleveland, Ohio, James A. Van Allen, Chairman of the Department of Physics and Astronomy, State University of Iowa, said that protons of the inner radiation belt could be a serious hazard for extended manned space flight and that nuclear detonations might be able to clean out these inner belt protons, perhaps for a prolonged period, making possible manned orbits about 300 miles above the earth.
References: 16.
1962 July 17 - 17:31 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 3-7-14. -
X-15A MH-96 Demo test Nation: USA. Agency: NASA/USAF. Apogee: 95 km (59 mi). FAI world altitude record. Maximum Speed - 6166 kph. Maximum Altitude - 95940 m. First astronaut wings flight (USAF definition). References: 2.
1962 July 18 - 09:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2D. LV Configuration: Thor DSV-2D 338. -
AVT 2 Satellite test Nation: USA. Agency: USAF. Apogee: 1,484 km (922 mi). References: 2.
1962 July 18 - 20:51 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 120D. -
Samos 9 Nation: USA. Payload: Samos E-2 no. 3 / Agena B 2403. Mass: 1,860 kg (4,100 lb). Class: Surveillance. Type: Military. Spacecraft: Samos. Agency: U.S. Air Force. Perigee: 184 km (114 mi). Apogee: 234 km (145 mi). Inclination: 96.00 deg. Period: 88.60 min. COSPAR: 1962-A-Zeta-1. USAF Sat Cat: 342. Decay Date: 1962-07-25. First generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results. References: 2, 6, 278.
-
FTV 2403 RV Nation: USA. Payload: E-6 RV. Spacecraft: Samos. Agency: USAF. COSPAR: 1962-A-Zeta-2. USAF Sat Cat: 343. Decay Date: 1962-07-27. References: 2, 279.
1962 July 19 - 11:05 GMT - Launch Site: Vandenberg. Launch Complex: 576B1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 13D. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 July 19 - 17:53 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 2-25-45. -
X-15A Heating rates, drag test Nation: USA. Agency: NASA/USAF. Apogee: 26 km (16 mi). Maximum Speed - 5590 kph. Maximum Altitude - 25680 m. References: 2.
1962 July 20 - -
NASA Mission Control Center would be located at Houston Nation: USA. Program: Apollo. Spacecraft: Gemini. NASA Administrator James E. Webb announced that the Mission Control Center for future manned space flights would be located at MSC. The Center would be operational in time for Gemini rendezvous flights in 1964 and later Apollo lunar missions. The overriding factor in the choice of MSC was the existing location of the Apollo Spacecraft Project Office, the astronauts, and Flight Operations Division at Houston.
References: 16.
1962 July 21 - Launch Vehicle: Saturn V. -
Apollo advanced Saturn launch complex northwest of Cape Canaveral Nation: USA. Program: Apollo. NASA announced plans for an advanced Saturn launch complex to be built on 80,000 acres northwest of Cape Canaveral. The new facility, Launch Complex 39, would include a building large enough for the vertical assembly of a complete Saturn launch vehicle and Apollo spacecraft.
References: 16.
1962 July 21 - -
Egyptians parade rockets Nation: Egypt. The Egyptian government exhibits mock-ups of missiles they are developing with assistance from German engineers. The El Qahir (conqueror) is 11 m long and was said to have a range of 600 km. The El Zafir (Victor) is 5.5 km long and had a range of 300 km. Later it is announced that a two-stage Al Ared (Pioneer) rocket is being developed that will have a range of 1000 km. A modification of this will be capable of launching satellites. Engineers involved in development of the rockets are said to be Wolfgang Pilz, Hans Goercke, and Hans Kleinwaechter. Eugen Saenger at the Stuttgart Propulsion Institute is also implicated. Saenger, who is working with his wife on steam-rocket boosted ramjet aircraft, denies this.
References: 47.
1962 July 21 - Launch Site: Al Kahir. Launch Complex: -. Launch Pad: -. Launch Vehicle: Al Kahir. -
Test mission Nation: Egypt. Agency: Egypt. Apogee: 50 km (31 mi). References: 2.
1962 July 21 - Launch Site: Al Kahir. Launch Complex: -. Launch Pad: -. Launch Vehicle: Al Kahir. -
Test mission Nation: Egypt. Agency: Egypt. Apogee: 50 km (31 mi). References: 2.
1962 July 21 - 00:56 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 342 / Agena B 1130. -
KH-4 9039 Nation: USA. Payload: KH-4 s/n 9039 / Agena B 1130. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 206 km (128 mi). Apogee: 376 km (233 mi). Inclination: 70.00 deg. Period: 90.30 min. COSPAR: 1962-A-Eta-1. USAF Sat Cat: 344. Decay Date: 1962-08-14. KH-4. Aborted after 6 photo passes. Heavy corona and radiation fog. References: 2, 6.
1962 July 21 - 20:50 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-12. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 July 21 - 22:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-13. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 July 21 - 23:50 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2P-2. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 July 22 - 09:21 GMT - Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 145D (AA5) / Agena B 6901 (AA5). FAILURE: Destroyed by range safety. -
Mariner 1 Nation: USA. Program: Mariner. Payload: Mariner R-1. Mass: 200 kg (440 lb). Class: Planetary. Type: Venus. Spacecraft: Mariner 1-2. Agency: NASA. COSPAR: F620722A. Decay Date: 1962-07-22. Venus probe. References: 126, 278.
1962 July 23 - Launch Site: Johnston Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. -
Mass spectrometer Aeronomy mission Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). References: 2.
1962 July 24 - 17:29 GMT - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Scout. Model: Blue Scout Jr SLV-1C. LV Configuration: Blue Scout Jr SLV-1C 101. -
ERCS / 279L 2 Communications mission Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
1962 July 24 - 21:41 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.23US. -
Lyra alpha test Solar ultraviolet mission Nation: USA. Agency: NASA. Apogee: 208 km (129 mi). References: 2.
1962 July 25 - -
Invitation to bid for the Apollo lunar excursion module Nation: USA. Program: Apollo. Spacecraft: Apollo LM, Apollo Lunar Landing. MSC invited 11 firms to submit research and development proposals for the lunar excursion module (LEM) for the manned lunar landing mission. The firms were Lockheed Aircraft Corporation, The Boeing Airplane Company, Northrop Corporation, Ling-Temco-Vought, Inc., Grumman Aircraft Engineering Corporation, Douglas Aircraft Company, General Dynamics Corporation, Republic Aviation Corporation, Martin- Marietta Company, North American Aviation, Inc., and McDonnell Aircraft Corporation.
Additional Details: Invitation to bid for the Apollo lunar excursion module. References: 16.
1962 July 25-26 - Launch Vehicle: Titan. Model: Titan 2. -
A reliability review of the Titan II launch vehicle engine system was held in Sacramento, California, at Aerojet-General's Liquid Rocket Plant, the site where the engines were being developed. Nation: USA. Gemini engines had to be more reliable than did intercontinental ballistic missile (ICBM) engines. This requirement meant supplementing the ICBM engine reliability program, a task being performed by Aerojet under Air Force Space Systems Division direction.
1962 July 25 - 15:41 GMT - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Caleb. LV Configuration: Caleb NC17.117. -
Test / aeronomy mission Nation: USA. Agency: USN NOTS. Apogee: 1,166 km (724 mi). References: 2.
1962 July 25 - 16:17 GMT - Launch Site: Cape Canaveral. Launch Complex: LC16. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-4. -
Mk 6 re-entry vehicle test launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1962 July 26 - 09:13 GMT - Launch Site: Johnston Island. Launch Complex: LE1. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2E. LV Configuration: Thor DSV-2E 180. FAILURE: Thor exploded on liftoff. -
BLUEGILL PRIME Nuclear test Nation: USA. Agency: USAF. Apogee: 0 km ( mi). Second attempt to launch a nuclear weapon using the Thor IRBM. The payload consisted of two re-entry vehicles, one with an instrument pod, the other with the warhead. The missile engine malfunctioned immediately on ignition. Range safety fired the destruct system whille the missile was still on the launch pad. The Johnston Island launch complex was heavily damaged and contaminated with plutonium. Three months of repairs and decontamination were necessary before tests could resume.
References: 2.
1962 July 26 - 17:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2TF-1. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 July 26 - 19:22 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 1-32-53. -
X-15A Aero stab. and drag test Nation: USA. Agency: NASA/USAF. Apogee: 30 km (18 mi). Maximum Speed - 6418 kph. Maximum Altitude - 30150 m. Roller coaster descent to simulate emergency reentry. References: 2.
1962 July 27 - Launch Vehicle: Atlas. Model: Atlas D. -
Mercury Atlas launch vehicle No. 113-D accepted Nation: USA. Program: Mercury. Atlas launch vehicle No. 113-D was inspected at Convair and accepted for the Mercury-Atlas 8 (MA-8) manned orbital mission. References: 483.
1962 July 27 - -
First Zero-G training on Tu-104 Nation: USSR. Program: Vostok. Flight: Vostok 3, Vostok 4. The Soviets conduct their first cosmonaut zero-G training on an aircraft flying parabolic trajectories. 6 to 25 seconds of weightlessness is experienced on each manoeuvre. References: 376.
1962 July 27 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1P-4. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1962 July 27 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1P-1. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1962 July 27 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1P-2. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1962 July 27 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1P-3. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1962 July 28 - 00:30 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 347 / Agena B 1131. -
KH-4 9040 Nation: USA. Payload: KH-4 s/n 9040 / Agena B 1131. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 204 km (126 mi). Apogee: 403 km (250 mi). Inclination: 71.00 deg. Period: 90.60 min. COSPAR: 1962-A-Theta-1. USAF Sat Cat: 345. Decay Date: 1962-08-24. KH-4; film capsule recovered 4.1 days later. No filters on slave horizon cameras. Heavy corona and radiation fog. References: 2, 6.
1962 July 28 - 02:50 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trailblazer. Model: Trailblazer 1. LV Configuration: Trailblazer 1 TB Ik. -
Re-entry Vehicle test Nation: USA. Agency: NASA. Apogee: 280 km (170 mi). References: 2.
1962 July 28 - 09:18 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 T15000-07. -
Cosmos 7 Nation: USSR. Payload: Zenit-2 11F61 s/n 4. Mass: 4,610 kg (10,160 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: RVSN. Perigee: 197 km (122 mi). Apogee: 356 km (221 mi). Inclination: 64.90 deg. Period: 90.00 min. COSPAR: 1962-A-Iota-1. USAF Sat Cat: 346. Duration: 4.00 days. Decay Date: 1962-08-01. Area survey photo reconnaissance satellite. Also performed radiation measurements. References: 2, 6, 93.
1962 July 29 - 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 July 31 - Launch Site: Baikonur. Launch Complex: LC60/8. 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 July - -
Design of heatshield for Apollo boilerplates completed Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NAA completed the analysis and design of the Fibreglass heatshield. It duplicated the stiffness of the aluminum heatshield and would be used on all boilerplate spacecraft. References: 16.
1962 August 1 - -
Russian methods for sending a man to the moon Nation: USSR. Program: Lunar L3. A recent Russian article discussed various methods which the Soviet Union had been studying for sending a man to the moon during the decade. The earth orbital rendezvous method was reported the most reliable, but consideration also had been given to the direct ascent method, using the "Mastodon" rocket.
References: 16.
1962 August 1 - -
Cuban missile crisis Nation: USSR. Cuban missile crisis - U.S.S.R. to build missile bases in Cuba; Kennedy orders Cuban blockade, lifts blockade after Russians back down
1962 August 1 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 1015. FAILURE: Human error in repair of pitch .potentiometer. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Missile test failure. Missed aimpoint by 3,191 m. References: 2.
1962 August 1 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 1007. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Successful missile test. Missed aimpoint by 167 m. References: 2.
1962 August 1 - Launch Site: Cape Canaveral. Launch Complex: LC26A. Launch Pad: -. Launch Vehicle: Jupiter. LV Configuration: Jupiter IRBM CM-111. -
Combat training launch Nation: Italy. Agency: Italia. Apogee: 500 km (310 mi). References: 2.
1962 August 1 - Launch Site: Kagoshima. Launch Complex: TMP. Launch Pad: -. Launch Vehicle: Kappa. Model: K150. LV Configuration: K150 AT-150. -
Test mission Nation: Japan. Agency: ISAS. Apogee: 5.00 km (3.10 mi). References: 2.
1962 August 1 - 21:07 GMT - Launch Site: Vandenberg. Launch Complex: 576E. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 15F. -
Research and development test Nation: USA. Agency: USAF. Apogee: 1,400 km (800 mi). First successful Atlas F flight at operational site, SMS 576E (15F) References: 2.
1962 August 2 - Launch Vehicle: Saturn I, Saturn V. -
Apollo lunar bus Nation: USA. Program: Apollo. Spacecraft: Lunar Bus. NASA's Office of Manned Space Flight issued Requests for Proposals for a study of the lunar "bus" and studies for payloads which could be handled by the C-1B and C-5 launch vehicles. Contract awards were expected by September 1 and completion of the studies by December 1.
References: 16.
1962 August 2 - 00:17 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena D. LV Configuration: Thor Agena D 344 / Agena D 1152. -
KH-4 9041 Nation: USA. Payload: KH-4 s/n 9041 / Agena D 1152. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 212 km (131 mi). Apogee: 423 km (262 mi). Inclination: 83.00 deg. Period: 90.80 min. COSPAR: 1962-A-Kappa-1. USAF Sat Cat: 360. Decay Date: 1962-08-22. KH-4; film capsule recovered 4.1 days later. Severe corona and radiation fog. References: 2, 6.
1962 August 2 - 17:56 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 3-8-16. -
X-15A MH-96 fixed gain test Nation: USA. Agency: NASA/USAF. Apogee: 44 km (27 mi). Maximum Speed - 5532 kph. Maximum Altitude - 44040 m. References: 2.
1962 August 3 - 17:46 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Exos. -
Bipolar Probe Ionosphere mission Nation: USA. Agency: USAF. Apogee: 365 km (226 mi). References: 2.
1962 August 5 - Launch Site: Vandenberg. Launch Complex: LC-B. Launch Pad: -. Launch Vehicle: Hopi. Model: Kiva/Hopi. -
Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 300 km (180 mi). References: 2.
1962 August 5 - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 124D / Agena B SPS 2404. -
Samos 10 Nation: USA. Payload: Samos E-6 no. 2 / Agena B 2404. Mass: 1,860 kg (4,100 lb). Class: Surveillance. Type: Military. Spacecraft: Samos. Agency: U.S. Air Force. Perigee: 201 km (124 mi). Apogee: 203 km (126 mi). Inclination: 96.20 deg. Period: 88.50 min. COSPAR: 1962-A-Lambda-2. USAF Sat Cat: 361. Decay Date: 1962-08-06. Second generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results. References: 2, 6, 278.
-
FTV 2404 Nation: USA. Payload: AFP-201 PVP 854. Spacecraft: Samos. Agency: USAF. COSPAR: 1962-A-Lambda-1. USAF Sat Cat: 361. Decay Date: 1962-08-06. References: 2, 279.
-
FTV 2404 RV Nation: USA. Payload: E-6 RV. Spacecraft: Samos. Agency: USAF. COSPAR: 1962-A-Lambda-xx. References: 2, 279.
1962 August 7 - -
Apollo BP- 25 impact test in the Pacific Ocean Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The first completed boilerplate model of the Apollo command module, BP- 25, was subjected to a one-fourth-scale impact test in the Pacific Ocean near the entrance to Los Angeles Harbor. Three additional tests were conducted on August 9. References: 16.
1962 August 7 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-1. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 August 7 - 00:47 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-62-1. -
Air sample Aeronomy mission Nation: Sweden. Agency: RTG/AFCRL. Apogee: 105 km (65 mi). References: 2.
1962 August 8 - Launch Vehicle: Saturn I, Saturn V. -
Two Apollo lunar logistic studies Nation: USA. Program: Apollo. Spacecraft: Lunar Bus. At a bidders' conference held at NASA Headquarters, proposals were requested from Centers and industry for two lunar logistic studies: a spacecraft "bus" concept that could be adapted for use first on the Saturn C-1B and later on the Saturn C-5 launch vehicles and a variety of payloads which could be soft-landed near manned Apollo missions. The latter study would determine how a crew's stay on the moon might be extended, how human capability for scientific investigation of the moon might be increased, and how man's mobility on the moon might be facilitated.
References: 16.
1962 August 8 - Launch Vehicle: Atlas. Model: Atlas D. -
Mercury Atlas launch vehicle 113-D delivered to Cape Canaveral Nation: USA. Program: Mercury. Atlas launch vehicle 113-D was delivered to Cape Canaveral for the Mercury-Atlas 8 (MA-8) manned orbital mission. References: 483.
1962 August 8 - 16:55 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.60GT. -
Attitude control test Nation: USA. Agency: NASA. Apogee: 149 km (92 mi). References: 2.
1962 August 8 - 18:08 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 2-26-46. -
X-15A Heating, aero drag test Nation: USA. Agency: NASA/USAF. Apogee: 27 km (16 mi). Maximum Speed - 4735 kph. Maximum Altitude - 27700 m. References: 2.
1962 August 9 - 22:51 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 8D. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 August 9 - 23:05 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 87D. -
Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2.
1962 August 10 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2TF-2. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 August 10 - 21:11 GMT - Launch Site: Vandenberg. Launch Complex: OSTF2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 57F. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 10 km (6 mi). References: 2.
1962 August 11 - -
NASA schedule for Apollo command and service modules Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A NASA program schedule for the Apollo spacecraft command and service modules through calendar year 1965 was established for financial planning purposes and distributed to the NASA Office of Manned Space Flight, Marshall Space Flight Center, and MSC. The key dates were: complete service module drawing release, May 1, 1963; complete command module drawing release, June 15, 1963; manufacture complete on the first spacecraft, February 1, 1964; first manned orbital flight, May 15, 1965. This tentative schedule depended on budget appropriations.
References: 16.
1962 August 11 - -
Eight companies to bid on Apollo lunar excursion module Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Of the 11 companies invited to bid on the lunar excursion module on July 25, eight planned to respond. NAA had notified MSC that it would not bid on the contract. No information had been received from the McDonnell Aircraft Corporation and it was questionable whether the Northrop Corporation would respond.
References: 16.
1962 August 11 - 01:48 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-62-3. -
Air sample Aeronomy mission Nation: Sweden. Agency: RTG/AFCRL. Apogee: 105 km (65 mi). References: 2.
1962 August 11 - 08:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K. -
Vostok 3 Nation: USSR. Program: Vostok. Payload: Vostok 3KA s/n 5. Mass: 4,722 kg (10,410 lb). Class: Manned. Type: Spacecraft. Spacecraft: Vostok. Agency: RVSN. Perigee: 166 km (103 mi). Apogee: 218 km (135 mi). Inclination: 65.00 deg. Period: 88.30 min. COSPAR: 1962-A-Mu-1. USAF Sat Cat: 363. Duration: 3.93 days. Decay Date: 1962-08-15. Crew: Nikolayev. Flight: Vostok 3. Joint flight with Vostok 4. The first such flight, where Vostok capsules were launched one day apart, coming within a few kilometers of each other at the orbital insertion of the second spacecraft. The flight was supposed to occur in March, but following various delays, one of the two Vostok pads was damaged in the explosion of the booster of the third Zenit-2 reconnsat in May. Repairs were not completed until August. Vostok 3 studied man's ability to function under conditions of weightlessness; conducted scientific observations; furthered improvement of space ship systems, communications, guidance and landing. Immediately at orbital insertion of Vostok 4, the spacecraft were less than 5 km apart. Popovich made radio contact with Cosmonaut Nikolayev. Nikolayev reported shortly thereafter that he had sighted Vostok 4. Since the Vostok had no maneuvering capability, they could not rendezvous or dock, and quickly drifted apart. The launches did allow Korolev to offer something new and different, and gave the launch and ground control crews practice in launching and handling more than one manned spacecraft at a time. The cosmonaut took colour motion pictures of the earth and the cabin interior.
Additional Details: Vostok 3. References: 2, 6, 16, 32, 33, 60, 175, 376.
1962 August 12 - 08:02 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K. -
Vostok 4 Nation: USSR. Program: Vostok. Payload: Vostok 3KA s/n 6. Mass: 4,728 kg (10,423 lb). Class: Manned. Type: Spacecraft. Spacecraft: Vostok. Agency: RVSN. Perigee: 159 km (98 mi). Apogee: 211 km (131 mi). Inclination: 65.00 deg. Period: 88.20 min. COSPAR: 1962-A-Nu-1. USAF Sat Cat: 365. Duration: 2.96 days. Decay Date: 1962-08-15. Crew: Popovich. Flight: Vostok 4. Joint flight with Vostok 3. Acquisition of experimental data on the possibility of establishing a direct link between two space ships; coordination of astronauts' operations; study of the effects of identical spaceflight conditions on the human organism. The launch of Popovich proceeds exactly on schedule, the spacecraft launching with 0.5 seconds of the planned time, entering orbit just a few kilometers away from Nikolayev in Vostok 3. Popovich had problems with his life support system, resulting in the cabin temperature dropping to 10 degrees Centigrade and the humidity to 35%. The cosmonaut still managed to conduct experiments, including taking colour motion pictures of the terminator between night and day and the cabin interior.
Despite the conditions, Popovich felt able to go for the full four days scheduled. But before the mission, Popovich had been briefed to tell ground control that he was 'observing thunderstorms' if he felt the motion sickness that had plagued Titov and needed to return on the next opportunity. Unfortunately he actually did report seeing thunderstorms over the Gulf of Mexico, and ground control took this as a request for an early return. He was ordered down a day early, landing within a few mintutes of Nikolayev. Only on the ground was it discovered that he was willing to go the full duration, and that ground control had thought he had given the code.
References: 2, 6, 32, 33, 60, 175, 376.
1962 August 13 - -
Ten Air Force pilots spend a month in a simulated space cabin Nation: USA. Program: Apollo. Ten Air Force pilots emerged from a simulated space cabin in which they had spent the previous month participating in a psychological test to determine how long a team of astronauts could work efficiently on a prolonged mission in space. Project Director Earl Alluisi said the experiment had "far exceeded our expectations" and that the men could have stayed in the cabin for 40 days with no difficulty.
References: 16.
1962 August 13 - 22:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC11. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 7F. -
Research and development / Pod 16 test Nation: USA. Agency: USAF. Apogee: 1,400 km (800 mi). References: 2.
1962 August 14 - -
LEM added to Apollo CSM Statement of Work Nation: USA. Program: Apollo. Spacecraft: Apollo LM. The NAA spacecraft Statement of Work was revised to include the requirements for the lunar excursion module (LEM) as well as other modifications. The LEM requirements were identical with those given in the LEM Development Statement of Work of July 24.The command module (CM) would now be required to provide the crew with a one-day habitable environment and a survival environment for one week after touching down on land or water. In case of a landing at sea, the CM should be able to recover from any attitude and float upright with egress hatches free of water.
Additional Details: LEM added to Apollo CSM Statement of Work. References: 16.
1962 August 14 - -
Flight tests of the half-scale vehicle (HSTV) in the Paraglider Development Program. Nation: USA. Program: Gemini. Spacecraft: Gemini. North American began flight tests of the half-scale vehicle (HSTV) in Phase II-A of the Paraglider Development Program two months behind schedule. The instrumented HSTV with the paraglider predeployed was towed aloft by helicopter. Objectives of the predeployed flights were to evaluate flight performance, longitudinal and lateral control characteristics, effectiveness of control, and the flare maneuver capability of the paraglider. Despite various minor malfunctions in all five test flights (August 14, 17, 23, September 17, and October 23, 1962), test results verified the stability of the wing/vehicle combination in free flight and the adequacy of control effectiveness.
1962 August 14 - 15:20 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL109. -
La / ion / ne Ionosphere mission Nation: Australia. Agency: WRE/RAE. Apogee: 111 km (68 mi). References: 2.
1962 August 14 - 18:41 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 3-9-18. FAILURE: Roll damper failure. -
X-15A Const Theta Entry test Nation: USA. Agency: NASA/USAF. Apogee: 59 km (36 mi). Maximum Speed - 6029 kph. Maximum Altitude - 59010 m. New reentry technique using pitch angle instrument instead of AOA. References: 2.
1962 August 15-16 - -
Manned Spacecraft Center reviewed engineering mock-up of the Gemini spacecraft. Nation: USA. Program: Gemini. Spacecraft: Gemini. Manned Spacecraft Center (MSC) formally reviewed McDonnell's engineering mock-up of the Gemini spacecraft in St Louis. The company had begun building the mock-up in January, shortly after receiving the spacecraft contract. Mock-up review had originally been scheduled for mid-July, but informal examinations by MSC representatives, including James A Chamberlin and several astronauts, had produced some suggested changes. The review itself resulted in McDonnell's receiving 167 requests for alterations. MSC inspected the revised mock-up in November.
1962 August 15 - -
Landing of Vostok 3 Nation: USSR. Program: Vostok. Flight: Vostok 3. Recovered August 15, 1962 6:52 GMT. Landed 48:02N 75:45 E. Both the Vostok 3 and 4 spacecraft land successfully six minutes apart a short distance from each other. References: 376.
1962 August 15 - -
Landing of Vostok 4 Nation: USSR. Program: Vostok. Flight: Vostok 4. Recovered August 15, 1962 6:59 GMT. Landed 48:09 N 71:51 E. By 07:00 the temperature aboard Vostok 4 is down to 10 deg C, and the humidity at 35%. Popovich is ready to continue for a fourth day, but he admits the cold is getting to him. Keldysh and Rudenko now support returning Vostok 4 to earth on the 49th orbit, but Smirnov still wants to go for the extra day. Then Popovich radios 'I observe thunderstorms (groza). Groza is the pre-agreed code word to indicate that the cosmonaut is vomiting. It is believed he is declaring an emergency and requesting an immediate landing. The State Commission meets again and has to decide within 40 minutes whether to begin setting the spacecraft up for retrofire. But then when Korolev and Smirnov ask the cosmonaut to verify, he explains "I am excellent, I was observing meteorological thunderstorms and lightning". However Gagarin and Kamanin are suspicious of the explanation - they believe Popovich had an attack of nausea, panicked, made the emergency radio transmission, but then felt better and didn't want to admit to his weakness when confronted by the leadership. However it is now too late. He is set to return at nearly the same time as Nikolayev on Vostok 3. Both spacecraft land successfully six minutes apart a short distance from each other. However flight plans for the State Commission are wrecked due to bad weather at nearby airfields.
References: 376.
1962 August 16 - Launch Vehicle: Saturn I. -
S-IV successfully static-fired for the first time Nation: USA. Program: Apollo. The second stage (S-IV) of the Saturn C-1 launch vehicle was successfully static-fired for the first time in a ten-second test at the Sacramento, Calif., facility by the Douglas Aircraft Company. References: 16.
1962 August 16 - Launch Site: Mountain Home AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. -
Titan I ICBM 569th SMS (nine missiles) declared operational at Mountain Home AFB Nation: USA.
1962 August 17 - -
Carl Sagan warned scientists of need for sterilization of lunar spacecraft Nation: USA. Program: Apollo. Carl Sagan, University of California astronomer, warned scientists at a lunar exploration conference, Blacksburg, Va., of the need for sterilization of lunar spacecraft and decontamination of Apollo crewmen, pointing out that Lunik II and Ranger IV probably had deposited terrestrial microorganisms on the moon. Even more serious, he said, was the possibility that lunar microorganisms might be brought to earth where they could multiply explosively.
References: 16.
1962 August 18 - 15:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. -
Cosmos 8 Nation: USSR. Program: DS. Payload: DS-K-8 s/n 1. Mass: 337 kg (742 lb). Class: Earth. Type: Micrometeoroid. Spacecraft: DS-K-8. Agency: RVSN. Perigee: 244 km (151 mi). Apogee: 598 km (371 mi). Inclination: 49.00 deg. Period: 92.90 min. COSPAR: 1962-A-Xi-1. USAF Sat Cat: 367. Completed Operations Date: 1962-08-23. Decay Date: 1963-08-17. Detected meteoroid flux in near-earth space and carried unspecified military research equipment. References: 2, 6, 99.
1962 August 19 - 00:57 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-62-4. -
Air sample Aeronomy mission Nation: Sweden. Agency: RTG/AFCRL. Apogee: 109 km (67 mi). References: 2.
1962 August 20 - Launch Vehicle: Titan. Model: Titan 3C. -
US Department of Defense announced Titan III launch vehicle. Nation: USA. The Department of Defense announced plans to develop a Titan III launch vehicle powered by both solid and liquid fuel rocket motors with a total thrust of over 11 million newtons (2.5 million Ibs). .Scheduled to become operational in 1965, the Titan III would be used to launch the Air Force's X-20 (Dyna Soar) manned spacecraft, as well as heavy unmanned military satellites. Martin Marietta Corporation had been selected as prime contractor for the project, at an estimated cost of between $500 million and $1 billion. At a news conference the following day, Defense Secretary Robert S. McNamara cited the Titan III as a major step toward overtaking the Soviet Union in various phases of military space development.
1962 August 20 - 18:08 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 2-27-47. -
X-15A Heating, drag, ASAS test Nation: USA. Agency: NASA/USAF. Apogee: 27 km (16 mi). Maximum Speed - 5686 kph. Maximum Altitude - 27000 m. References: 2.
1962 August 22 - -
Contractor for Apollo CM reaction controls changed Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Responsibility for the design and manufacture of the reaction controls for the Apollo command module was shifted from The Marquardt Corporation to the Rocketdyne Division of NAA, with NASA concurrence. References: 16.
1962 August 22 - -
Length of the Apollo service module increased Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The length of the Apollo service module was increased from 11 feet 8 inches to 12 feet 11 inches to provide space for additional fuel. References: 16.
1962 August 22 - -
Future Vostok flight plans discussed Nation: USSR. Program: Vostok. Flight: Vostok 5, Vostok 6, Vostok 6A, Vostok 7, Vostok 8, Vostok 9, Vostok 10, Vostok 11, Vostok 12. At Baikonur for the launch of a Venera probe, the Soviet space leadership discussed future plans. The female cosmonaut training group was there for their first rocket launch. The next Vostok would carry the first woman into space; Ponomaryova, Solovyova, and Tereshkova were the leading candidates. Flight plans were discussed at a meeting in the evening between Kamanin and Leonid Smirnov. It would be possible to make the flight by the end of 1962, but March-April 1963 was more likely, depending on the final report on the Vostok 3/4 flights. The work force would be fully occupied in August-October in launching probes to Venus and Mars, also probably delaying any Vostok flight until the following spring. The next flight would probably be part of a group flight of two or three spacecraft, piloted by both men and women. The female flights would be limited to three days, while the male flights would last for 7 to 8 days.
Additional Details: Future Vostok flight plans discussed. References: 376.
1962 August 22 - 15:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NE3.128. -
Solar extreme ultraviolet / x-ray mission Nation: USA. Agency: NRL. Apogee: 234 km (145 mi). References: 2.
1962 August 23 - 07:15 GMT - Launch Site: Kagoshima. Launch Complex: TMP. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8L. LV Configuration: Kappa 8L K-8L-1. -
Test mission Nation: Japan. Agency: ISAS. Apogee: 173 km (107 mi). References: 2.
1962 August 23 - 11:44 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-2M. LV Configuration: Scout X-2M S117. -
P 35-2 Nation: USA. Program: DMSP. Mass: 91 kg (200 lb). Class: Earth. Type: Weather. Spacecraft: Program 35. Agency: U.S. Air Force. Perigee: 578 km (359 mi). Apogee: 752 km (467 mi). Inclination: 98.50 deg. Period: 98.10 min. COSPAR: 1962-A-Omicron-1. USAF Sat Cat: 369. Military weather satellite to provide targetting information for reconnaisance satellites. References: 2, 6.
1962 August 23 - 17:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.30CA. -
Structure Aeronomy mission Nation: USA. Agency: NASA. Apogee: 129 km (80 mi). References: 2.
1962 August 24 - 11:38 GMT - Launch Site: Woomera. Launch Complex: LA5B. Launch Pad: LA5B?. Launch Vehicle: Black Knight. Model: Black Knight 301/C. LV Configuration: Black Knight-301/C BK.16. -
Gaslight Re-entry Vehicle test Nation: UK. Agency: RAE. Apogee: 573 km (356 mi). References: 2.
1962 August 25 - Launch Site: Point Mugu. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. FAILURE: Failure. -
PM-14 test Nation: USA. Agency: USA. Apogee: 100 km (60 mi). References: 2.
1962 August 25 - 02:18 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 T103-12. FAILURE: At T+60 min 50 sec one of the four solid motors of the escape stage's BOZ unit did not fire. The resulting asymmetric torque caused the stage to lose correct attitude and three seconds after ignition of the main engine S1.5400A1 it began to tumble. -
Sputnik 19 Nation: USSR. Program: Venera, Vostok. Payload: 2MV-1 s/n 1. Mass: 890 kg (1,960 lb). Class: Planetary. Type: Venus. Spacecraft: Mars 2MV-1. Agency: RVSN. Perigee: 173 km (107 mi). Apogee: 252 km (156 mi). Inclination: 64.90 deg. Period: 88.70 min. COSPAR: 1962-A-Pi-1. USAF Sat Cat: 371. Decay Date: 1962-08-28. Attempt to launch a probe towards Mars. The launch went well, but the fourth stage motor burnt for only 45s of the planned 240s. The stage remained in Earth orbit. However Kamanin notes that it was good that the launch of the basic vehicle was a success - it gave the visiting female cosmonauts confidence in the rocket they will have to ride.
References: 2, 6, 64, 65.
1962 August 27 - -
Female Vostok flights delayed to 1963 Nation: USSR. Program: Vostok. Spacecraft: Sokol SK-1. Flight: Vostok 5, Vostok 6, Vostok 6A, Vostok 7, Vostok 8, Vostok 9, Vostok 10, Vostok 11, Vostok 12. The prospects did not look good for authorisation of production of ten further Vostok spacecraft. In a heated discussion between Rudenko, Ivanovskiy, and Grechko, it was argued that production of further Vostoks would delay flight of the first Soyuz spacecraft by a year. On the other hand this would mean no Soviet manned flights in 1963-1964. Furthermore Ivanovskiy reported that production of the female version of the Vostok space suit could not be completed until the end of 1962. Therefore this meant that the flight of two female cosmonauts in the final two available Vostok spacecraft would be delayed until March-April 1963 - the very end of the storage life of the spacecraft.
References: 376.
1962 August 27 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2TF-4. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 August 27 - 06:53 GMT - Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 179D (AA6) / Agena B 6902 (AA6). -
Mariner 2 Nation: USA. Program: Mariner. Payload: Mariner R-2. Mass: 201 kg (443 lb). Class: Planetary. Type: Venus. Spacecraft: Mariner 1-2. Agency: NASA. COSPAR: 1962-A-Rho-1. USAF Sat Cat: 374. Mariner 2 was the first spacecraft to successfully flyby another planet. It was a backup for the Mariner 1 mission which failed shortly after launch to Venus. After launch and termination of the Agena first burn, the Agena-Mariner was in a 118 km altitude Earth parking orbit. The Agena second burn injected the Mariner 2 spacecraft into a geocentric escape hyperbola at 26 minutes 3 seconds after lift-off. Solar panel extension was completed about 44 minutes after launch. On 29 August 1962 cruise science experiments were turned on. A midcourse maneuver was initiated at 22:49:00 GMT on 4 September and completed at 2:45:25 GMT 5 September. On 8 September at 17:50 GMT the spacecraft suddenly lost its attitude control, which was restored by the gyroscopes 3 minutes later. The cause was unknown but may have been a collision with a small object. On October 31 the output from one solar panel deteriorated abruptly, and the science cruise instruments were turned off. A week later the panel resumed normal function and instruments were turned back on. The panel permanently failed on 15 November, but Mariner 2 was close enough to the Sun that one panel could supply adequate power. On December 14 the radiometers were turned on. Mariner 2 approached Venus from 30 degrees above the dark side of the planet, and passed below the planet at its closest distance of 34,773 km at 19:59:28 GMT 14 December 1962. After encounter, cruise mode resumed. Spacecraft perihelion occurred on 27 December at a distance of 105,464,560 km. The last transmission from Mariner 2 was received on 3 January 1963 at 07:00 GMT. Mariner 2 remains in heliocentric orbit. Scientific discoveries made by Mariner 2 included a slow retrograde rotation rate for Venus, hot surface temperatures and high surface pressures, a predominantly carbon dioxide atmosphere, continuous cloud cover with a top altitude of about 60 km, and no detectable magnetic field. It was also shown that in interplanetary space the solar wind streams continuously and the cosmic dust density is much lower than the near-Earth region. Improved estimates of Venus' mass and the value of the astronomical unit were made.
References: 2, 6, 278, 296.
1962 August 27 - 09:08 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 107. -
Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 114 km (70 mi). References: 2.
1962 August 28 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. -
Test mission Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2.
1962 August 28 - 19:34 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AC6.829. -
EM Absorption Ionosphere mission Nation: USA. Agency: USAF. Apogee: 148 km (91 mi). References: 2.
1962 August 29 - 01:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena D. LV Configuration: Thor Agena D 349 / Agena D 1153. -
KH-4 9044 Nation: USA. Payload: KH-4 s/n 9044 / Agena D 1153. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 187 km (116 mi). Apogee: 400 km (240 mi). Inclination: 65.20 deg. Period: 90.40 min. COSPAR: 1962-A-Sigma-1. USAF Sat Cat: 377. Decay Date: 1962-09-10. KH-4; film capsule recovered 4.1 days later. Erratic vehicle attitude. Radiation fog minimal. References: 2, 6.
1962 August 29 - 01:01 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL28. -
Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 109 km (67 mi). References: 2.
1962 August 29 - 18:36 GMT - Launch Site: Hidden Hills DZ. Launch Complex: -. Launch Pad: 36.1 N x 116.0 W. Launch Vehicle: X-15. LV Configuration: X-15 2-28-48. -
X-15A Heating test Nation: USA. Agency: NASA/USAF. Apogee: 29 km (18 mi). Maximum Speed - 5546 kph. Maximum Altitude - 29630 m. References: 2.
1962 August 30 - -
Korolev supports military Vostok flights Nation: USSR. Program: Vostok. Flight: Vostok 7, Vostok 8, Vostok 9, Vostok 10, Vostok 11, Vostok 12, Vostok 13. Korolev, still very ill in the hospital following a collapse six days earlier, supported Kamanin's plan for acceptance of the Vostok manned spacecraft for military service with the Soviet Air Force. It could enter series production and be used for continuous military research flights. However the General Staff continued to oppose any expansion of manned space flight. It it wasn't for Khrushchev, Korolev noted, there would not be any Soviet manned space programme at all.
References: 376.
1962 August 31 - Launch Site: Wallops Island. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-3A. LV Configuration: Scout X-3A S114. FAILURE: Late stage 3 ignition. -
Reentry 2 Nation: USA. Class: Technology. Type: RV. Agency: NASA. Apogee: 217 km (134 mi). Decay Date: 1962-08-31. References: 2, 126.
1962 August - -
Limited testing planned of fire hazards in pure oxygen atmosphere for Apollo Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A preliminary NAA report was completed on a literature search concerning fire hazards in 100 percent oxygen and oxygen-enriched atmospheres. This report showed that limited testing would be warranted. References: 16.
1962 August 31 - 00:56 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-62-5. -
Air sample Aeronomy mission Nation: Sweden. Agency: RTG/AFCRL. Apogee: 111 km (68 mi). References: 2.
1962 September - -
M2-F1 lifting body first flight. Nation: USA. Spacecraft: M2-F2, HL-10, X-24A. The lifting body concept was first tested at Dryden with a plywood prototype designated the M2-F1 built in late 1962. It featured a plywood shell built by Gus Briegleb, a sailplane builder from Mirage Dry Lake, Calif., placed over a tubular frame built at Dryden. The M2-F1 was towed aloft, first behind an auto and then a C-47 more than 100 times, to validate basic lifting body stability and control characteristics. This led to establishment of the formal program which resulted in the HL-10, M2-F2, M2-F3, X-24A, and X-24B lifting bodies.
1962 September - Launch Site: Schilling AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. -
Atlas SMS 560 operational. Nation: USA. Schilling AFB SMS 550 operational References: 4460.
1962 September 1 - 02:12 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 T103-13. FAILURE: At T+ 61 min 30 sec the fuel valve did not open.; the ignition command was blocked from going to the main engine of Stage 4. -
Sputnik 20 Nation: USSR. Program: Venera. Payload: 2MV-1 s/n 2. Mass: 6,500 kg (14,300 lb). Class: Planetary. Type: Venus. Spacecraft: Mars 2MV-1. Agency: RVSN. Perigee: 185 km (114 mi). Apogee: 246 km (152 mi). Inclination: 64.70 deg. Period: 88.80 min. COSPAR: 1962-A-Tau-1. USAF Sat Cat: 381. Decay Date: 1962-09-06. References: 2, 6, 64, 65.
1962 September 1 - 20:39 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 348 / Agena B 1132. -
KH-5 9042A Nation: USA. Payload: KH-5 s/n 9042A/Agena B 1132. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-5. Agency: U.S. Air Force. Perigee: 293 km (182 mi). Apogee: 639 km (397 mi). Inclination: 82.80 deg. Period: 94.00 min. COSPAR: 1962-A-Upsilon-1. USAF Sat Cat: 385. Decay Date: 1964-10-26. KH-5. Mission failed. Parachute shrouds parted during air catch, capsule sank. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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SRV 600 Nation: USA. Spacecraft: KH-5. Agency: USAF. COSPAR: 1962-A-Upsilon-x. References: 2, 279.
1962 September 4 - -
Nine industry proposals for the Apollo lunar excursion module received Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Nine industry proposals for the lunar excursion module were received from The Boeing Company, Douglas Aircraft Company, General Dynamics Corporation, Grumman Aircraft Engineering Corporation, Ling-Temco-Vought, Inc., Lockheed Aircraft Corporation, Martin-Marietta Corporation, Northrop Corporation, and Republic Aviation Corporation. NASA evaluation began the next day.
Additional Details: Nine industry proposals for the Apollo lunar excursion module received. References: 16.
1962 September 5 - -
Studies of Apollo unmanned logistic system Nation: USA. Program: Apollo. Spacecraft: Apollo ULS. Two three-month studies of an unmanned logistic system to aid astronauts on a lunar landing mission would be negotiated with three companies, NASA announced. Under a $150,000 contract, Space Technology Laboratories, Inc., would look into the feasibility of developing a general-purpose spacecraft into which varieties of payloads could be fitted. Under two $75,000 contracts, Northrop Space laboratories and Grumman Aircraft Engineering Corporation would study the possible cargoes that such a spacecraft might carry. NASA Centers simultaneously would study lunar logistic: trajectories, launch vehicle adaptation, lunar landing touchdown dynamics, scheduling, and use of roving vehicles on the lunar surface.
References: 16.
1962 September 6 - -
Apollo mockups, and boilerplates deleted Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NASA deleted five Apollo mockups, three boilerplate spacecraft, and several ground support equipment items from the NAA contract because of funding limitations. References: 16.
1962 September 6 - 15:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-2. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1962 September 7 - -
Apollo boilerplate model BP-1 accepted by NASA Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Apollo command module boilerplate model BP-1 was accepted by NASA and delivered to the NAA Engineering Development Laboratory for land and water impact tests. On September 25, BP-1 was drop-tested with good results. Earth-impact attenuation and crew shock absorption data were obtained.
References: 16.
1962 September 8 - Launch Vehicle: Atlas. Model: Atlas D. -
Mercury Atlas vehicle 113-D static-fired Nation: USA. Program: Mercury. Atlas launch vehicle 113-D for the Mercury-Atlas 8 (MA-8) manned orbital mission was static-fired at Cape Canaveral. This test was conducted to check modifications that had been made to the booster for the purpose of smoother engine combustion. References: 483.
1962 September 8 - Launch Site: Beale AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. -
Titan I ICBM 851st SMS (nine missiles) declared operational at Beale AFB Nation: USA.
1962 September 9 - Launch Site: Cuxhaven. Launch Complex: -. Launch Pad: -. -
Rocket mail at Cuxhaven Nation: Germany. The DRG (German Rocket Society) made postal launches from spaceport Cuxhaven.
1962 September 10 - -
Apollo command module boilerplate model BP-3 shipped Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Apollo command module boilerplate model BP-3, showing the arrangement of the cabin interior, was shipped to MSC. References: 16.
1962 September 10 - -
Fire in a simulated Air Force space cabin Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Fire broke out in a simulated space cabin at the Air Force School of Aerospace Medicine, Brooks Air Force Base, Tex., on the 13th day of a 14-day experiment to determine the effects of breathing pure oxygen in a long-duration space flight. One of the two Air Force officers was seriously injured. The cause of the fire was not immediately determined. The experiment was part of a NASA program to validate the use of a 5 psia pure oxygen atmosphere for the Gemini and Apollo spacecraft.
References: 16.
1962 September 10 - -
Mercury MA-8 postponed Nation: USA. Program: Mercury. Flight: Mercury MA-8. The Mercury-Atlas 8 (MA-8) manned orbital mission was postponed and rescheduled for September 28, 1962, to allow additional time for flight preparation. References: 483.
1962 September 11 - -
NASA Astronaut Training Group 2 selected. Nation: USA. The group was selected to provide pilots for the Gemini program and early Apollo missions.. Qualifications: Test pilot status (either military, NASA, or aircraft industry), qualified jet pilot with minimum 1,000 flight-hours, under 35 years old, under 183 cm height, excellent health. US citizen.. 253 applicants survived initial NASA screening of their records. Following physical and psychiatric tests, nine were selected. Eight made it to space (See was killed in a T-38 crash before his first spaceflight). This was generally considered the highest quality group of astronauts ever selected. They would command the missions during the glory days of the American space program - Gemini, Apollo, and Skylab. Young was the only astronaut to fly Gemini, Apollo, and the Shuttle program. Armstrong was the only one to fly the X-15, Gemini, and Apollo. Conrad was the only one to fly Gemini, Apollo, and Skylab.
1962 September 11 - 13:30 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2C. LV Configuration: Skylark-2C SL44. -
Elec / Ion / Lang probes Ionosphere mission Nation: Australia. Agency: WRE/RAE. Apogee: 232 km (144 mi). References: 2.
1962 September 11 - 23:24 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AC3.322. -
Day Airglow Aeronomy mission Nation: USA. Agency: USAF. Apogee: 306 km (190 mi). References: 2.
1962 September 12 - -
President Kennedy spoke at Rice University Nation: USA. Program: Apollo. President John F. Kennedy spoke at Rice University, Houston, Tex., where he said:"Man, in his quest for knowledge and progress, is determined and cannot be deterred. The exploration of space will go ahead, whether we join in it or not, and it is one of the great adventures of all time, and no nation which expects to be the leader of other nations can expect to stay behind in this race for space. . . . "We choose to go to the moon in this decade and do the other things, not because they are easy, but because they are hard, because that goal will serve to organize and measure the best of our energies and skills, because that challenge is one that we are willing to accept, one we are unwilling to postpone, and one which we intend to win, and the others, too. "It is for these reasons that I regard the decision last year to shift our efforts in space from low to high gear as among the most important decisions that will be made during my incumbency in the office of the Presidency. . . ."
References: 16.
1962 September 12 - -
President Kennedy visited the Manned Spacecraft Center Nation: USA. President John F. Kennedy visited the Manned Spacecraft Center and was shown exhibits including Mercury, Gemini, and Apollo spacecraft hardware. References: 483.
1962 September 12 - -
First "mystery" satellite in history of space exploration Nation: USA. NASA announced it would launch a special satellite before the end of the year 'to obtain information on possible effects of radiation on future satellites and to give the world's scientific community additional data on the artificial environment created by the radiation belt.' The 100-pound satellite would be launched from Cape Canaveral into an elliptical orbit ranging from about 170-mile perigee to 10,350-mile apogee. First 'mystery' satellite in history of space exploration was launched, according to British magazine Flight International. The magazine said the satellite orbited at a height of 113 miles and reentered the earth's atmosphere 12 days later. The satellite was listed as belonging to the U.S. Air Force, but spokesman said this was a 'scientific guess based on our assessment of previous satellite launchings.' Launching was not confirmed, and no official U.S. listing included such a satellite.
References: 483.
1962 September 12 - 00:59 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 T103-14. FAILURE: At T+531 sec, the fourth vernier chamber of Stage 3's 8D715K engine exploded because the LOX cut-off valve had not closed as scheduled and LOX flowed into the hot chamber. -
Sputnik 21 Nation: USSR. Program: Venera. Payload: 2MV-2 s/n 1. Mass: 6,500 kg (14,300 lb). Class: Planetary. Type: Venus. Spacecraft: Mars 2MV-2. Agency: RVSN. Perigee: 179 km (111 mi). Apogee: 218 km (135 mi). Inclination: 64.90 deg. Period: 88.40 min. COSPAR: 1962-A-Phi-1. USAF Sat Cat: 389. Decay Date: 1962-09-14. The escape stage entered parking orbit but the main engine cut off just 0.8 s after ignition due to cavitation in the oxidiser pump and pump failure. References: 2, 6, 64, 65.
1962 September 12 - 15:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-5. -
Mk 6 re-entry vehicle test launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2.
1962 September 13 - -
General Staff tries to prevent further Soviet manned spaceflights Nation: USSR. Flight: Vostok 5, Vostok 6, Vostok 6A, Vostok 7, Vostok 8, Vostok 9, Vostok 10, Vostok 11, Vostok 12. At a meeting of the General Staff on space plans, it was reported that the Ministry of Defence supported completion of two additional Vostok spacecraft to allow four Vostok flights in 1963. But Malinovskiy was adamant: the Vostok fullfilled no military objectives, would not be accepted for military use, and he would recommend to the Military Industrial Commission that the additional flights be rejected. Kamanin noted that history was repeating itself - fifty years earlier Tsarist generals had rejected the acquisition of aircraft by the Imperial Russian Army.
References: 376.
1962 September 14 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1T-6. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1962 September 15 - Launch Site: Lincoln AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. -
Atlas SMS 551 operational. Nation: USA. Lincoln AFB SMS 551 operational References: 4460.
1962 September 15 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1T-5. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1962 September 17 - 23:46 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 350 / Agena B 1133. -
KH-4 9043 / TRS 1 (ERS 2) Nation: USA. Payload: KH-4 s/n 9043 / TRS 1 (ERS 2) / Agena B 1133. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 204 km (126 mi). Apogee: 668 km (415 mi). Inclination: 81.80 deg. Period: 93.30 min. COSPAR: 1962-A-Chi-1. USAF Sat Cat: 396. Decay Date: 1962-11-16. KH-4; film capsule recovered 1.1 days later; ERS-2 subsatellite failed to deploy. Capping shutter malfunction, slight corona and radiation fog. References: 2, 6.
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TRS Nation: USA. Payload: ERS 2. Class: Earth. Type: Magnetosphere. Spacecraft: ERS. Agency: USAF. COSPAR: 1962-A-Chi-xx. References: 2, 279.
1962 September 18 - -
Slayton designated Coordinator of Astronaut Activities Nation: USA. Program: Mercury. Donald Slayton, one of the seven chosen for the astronaut training program, was designated Coordinator of Astronaut Activities at the Manned Spacecraft Center. References: 483.
1962 September 18 - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 421. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2.
1962 September 18 - 08:53 GMT - Launch Site: |