Chronology - Quarter 2 1962

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Previous Home Next 1962 April - Launch Vehicle: Atlas. Model: Atlas F. Atlas F training facility activated. Nation: USA. VAFB Atlas F training facility turned over to SAC References: 4460. 1962 April - Launch Vehicle: Atlas. Model: Atlas D. Crash program completed to clear Atlas configuration problems. Nation: USA. Golden Ram follow-on completed at all Atlas D operational bases References: 4460. 1962 April 1-7 - Design criteria of the Apollo service module for the lunar landing maneuver Nation: USA. Program: Apollo. Spacecraft: Apollo CSM, Apollo Lunar Landing. NAA was directed by the MSC Apollo Spacecraft Project Office to begin a study to define the configuration and design criteria of the service module which would make the lunar landing maneuver and touchdown. References: 16. 1962 April 3 - 04:57 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trailblazer. Model: Trailblazer 1. LV Configuration: Trailblazer 1 TB Ij. Re-entry Vehicle test Nation: USA. Agency: NASA. Apogee: 260 km (160 mi). References: 2. 1962 April 4 - Mockup of the Apollo command module made public Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. A mockup of the Apollo command module, built by the Space and Information Systems Division of NAA, was made public for the first time during a visit to NAA by news media representatives. References: 16. 1962 April 5 - 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 April 5 - 15:47 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL163. Grenades / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 238 km (147 mi). References: 2. 1962 April 5 - 18:04 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 3-3-7. X-15A MH-96 test Nation: USA. Agency: NASA/USAF. Apogee: 54 km (33 mi). Maximum Speed - 4586 kph. Maximum Altitude - 54860 m. The X-15 was flown in a test of a new automatic control system to be used in the Dyna-Soar and Apollo spacecraft. The previous electronic control system had been automatic only while the X-15 was in the atmosphere; the new system was automatic in space as well. References: 2. 1962 April 6 - Launch Vehicle: Little Joe II. Request for proposal for the Little Joe II launch vehicle Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The request for a proposal on the Little Joe II test launch vehicle was submitted to bidders by a letter from MSC, together with a Work Statement. Five launches, which were to test boilerplate models of the Apollo spacecraft command module in abort situations, were called for: three in 1963 and two in 1964. Additional Details: Request for proposal for the Little Joe II launch vehicle. References: 16. 1962 April 6 - Thiokol selected for Apollo launch escape tower jettison motors Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Thiokol Chemical Corporation was selected by NAA to build the solid-fuel rocket motor to be used to jettison the Apollo launch escape tower following a launch abort or during a normal mission. References: 16. 1962 April 6 - Launch Vehicle: Atlas. Model: Atlas D. Symposium on the results of Mercury MA-6 Nation: USA. Program: Mercury. NASA sponsored a 1-day symposium in Washington on the results of the Mercury-Atlas 6 (MA-6) three-orbit flight of John Glenn. One of the items of particular interest was Glenn's 'fire-flies,' or luminous particles, and their possible origin. References: 483. 1962 April 6 - 17:15 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. LV Configuration: Kosmos 63S1 5LK. Cosmos 2 Nation: USSR. Program: MS. Payload: 1MS s/n 1. Mass: 285 kg (628 lb). Class: Technology. Spacecraft: 1MS. Agency: RVSN. Perigee: 207 km (128 mi). Apogee: 1,485 km (922 mi). Inclination: 49.00 deg. Period: 101.80 min. COSPAR: 1962-Iota-1. USAF Sat Cat: 269. Decay Date: 1963-08-20. Radiation, cosmic ray data. Decay date suspect Investigation of the upper atmosphere and outer space; development of elements in the design of space craft. References: 2, 6. 1962 April 9 - 15:04 GMT - Launch Site: Vandenberg. Launch Complex: SLC3E. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 110D. Midas 5 Nation: USA. Payload: Midas / Agena TV 1203. Mass: 1,860 kg (4,100 lb). Class: Early Warning. Spacecraft: Midas. Agency: U.S. Air Force. Perigee: 2,784 km (1,729 mi). Apogee: 3,405 km (2,115 mi). Inclination: 86.70 deg. Period: 152.90 min. COSPAR: 1962-Kappa-1. USAF Sat Cat: 271. Missile Defense Alarm System. References: 2, 6, 171, 172, 278. West Ford Drag Nation: USA. Payload: West Ford Drag Experiment. Spacecraft: WestFord Needles. Agency: USAF. COSPAR: 1962-Kappa-2. USAF Sat Cat: 272. Decay Date: 1962-05-04. References: 2, 279. 1962 April 9 - 20:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC11. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 11F. FAILURE: Failure. Research and development launch Nation: USA. Agency: USAF. References: 2. 1962 April 11 - DX (highest) priority for the Apollo program Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. President John F, Kennedy designated the Apollo program including essential spacecraft, launch vehicles, and facilities as being in the highest national priority category (DX) for research and development and for achieving operational capability. References: 16. 1962 April 12 - Launch Vehicle: N1. First Soviet announcement of manned lunar goals Nation: USSR. Program: Lunar L1. Class: Manned. Type: Spacecraft. Spacecraft: Soyuz A, Soyuz B, Soyuz V. First Soviet public announcement of manned lunar goals. References: 72. 1962 April 12 - Launch Site: Point Mugu. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. PM-10? 3-stage test Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2. 1962 April 12 - 01:57 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 129D. Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2. 1962 April 12 - 16:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18B. Launch Pad: LC18B. Launch Vehicle: Scout. Model: Blue Scout 1. LV Configuration: Blue Scout I D-7. FAILURE: Failure. Reentry Test re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 30 km (18 mi). References: 2. 1962 April 13 - Launch Vehicle: N1. N1 development slowed. Nation: USSR. Decree 'On restriction of work on the N1' was issued. References: 474. 1962 April 16 - Launch Vehicle: N1, R-56, Tsiklon. N1, R-36, R-36-O, and R-56 rockets authorised. Nation: USSR. Decree 'On Important Development of Intercontinental Ballistic and Global Missiles and Carriers-Rockets for Space Objects--work on the N1, R-36, R-36-O, and R-56' was issued. References: 474. 1962 April 16 - Soyuz A circumlunar spacecraft authorised. Nation: USSR. Spacecraft: Soyuz A, Soyuz B, Soyuz V. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On the Development of the 'Soyuz' Complex for Piloted flight to the Moon--approving the Soyuz program for circumlunar flight' was issued. The Soyuz was to be capable of the following: Automatic rendezvous with other spacecraft Automatic approach and alignment Automatic docking Exit of crew into open space for transfer from spacecraft to spacecraft Astronavigation Maneuvering in orbit (changing of orbital parameters) Test of re-entry using body lift to modify the landing point and alleviate G-forces Test of the operation of radio equipment and tracking equipment Scientific research 1962 April 17 - 09:28 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.42GA. Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 119 km (73 mi). References: 2. 1962 April 17 - 09:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.20CA. Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 201 km (124 mi). References: 2. 1962 April 17 - 17:20 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NA3.114F?. Aeronomy mission Nation: USA. Agency: NRL. Apogee: 286 km (177 mi). References: 2. 1962 April 18 - Launch Site: Lowry AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. Titan I ICBM 848th SMS (nine missiles) declared operational at Lowry AFB Nation: USA. 1962 April 18 - 00:54 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 331 / Agena B 1124. Discoverer 39 Nation: USA. Payload: KH-4 s/n 9032 / Agena B 1124. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 158 km (98 mi). Apogee: 540 km (330 mi). Inclination: 73.50 deg. Period: 91.60 min. COSPAR: 1962-Lambda-1. USAF Sat Cat: 276. Decay Date: 1962-05-28. KH-4. Best mission to date. References: 2, 6. 1962 April 18 - 18:17 GMT - Launch Site: Cape Canaveral. Launch Complex: LC26A. Launch Pad: -. Launch Vehicle: Jupiter. LV Configuration: Jupiter IRBM CM-114. CTL Nation: Turkey. Agency: Turkey. Apogee: 500 km (310 mi). Combat Training Launch fired from AMR at 1317 hours and 54.1 seconds EST to a predicted impact point of 1,514 nm from the firing site. All functions of the flight were normal up to 153 seconds, at which time fuel depletion was reached and normal guidance cut-off was not achieved. The missile impacted approximately 230 miles short of the intended target. All missions assigned to the NATO training launch crew were accomplished. References: 2. 1962 April 19 - Launch Site: AMR DZ. Launch Complex: -. Launch Pad: 29.0 N x 79.0 W. Launch Vehicle: Skybolt. LV Configuration: Skybolt ALBM 20025. FAILURE: Failure. Test mission Nation: USA. Agency: USAF. Apogee: 10 km (6 mi). References: 2. 1962 April 19 - 18:02 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 1-26-46. X-15A ASAS, alpha 20, M=5 test Nation: USA. Agency: NASA/USAF. Apogee: 46 km (28 mi). Maximum Speed - 6220 kph. Maximum Altitude - 46940 m. References: 2. 1962 April 20 - Launch Vehicle: N1. OP -Orbital Belt Nation: USSR. Spacecraft: OP. Korolev’s fantastic ‘Orbitalniy Poyas’ (OP -Orbital Belt) scheme anticipated Ronald Reagan’s Strategic Defence Initiative by 25 years. Two to three large N-I launched military manned stations would control a constellation of strategic assets. Geosynchronous nuclear-powered satellites would provide secure communications. Piloted reconnaissance spacecraft would surprise the enemy, observing military preparations without warning. The orbital stations would provide continuous observations of the territory of the imperialist block. 1962 April 20 - 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 April 20 - 19:26 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 3-4-8. X-15A MH-96, M=5 test Nation: USA. Agency: NASA/USAF. Apogee: 63 km (39 mi). Maximum Speed - 6097 kph. Maximum Altitude - 63250 m. References: 2. 1962 April 23 - 20:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 133D (AA4) / Agena B 6004 (AA4). Ranger 4 Nation: USA. Program: Ranger. Mass: 328 kg (723 lb). Class: Planetary. Type: Lunar. Spacecraft: Ranger 3-4-5. Agency: NASA. COSPAR: 1962-Mu-1. USAF Sat Cat: 280. Decay Date: 1962-04-26. Ranger IV was launched by an Atlas-Agena B booster from the Atlantic Missile Range, attained a parking orbit, and was fired into the proper lunar trajectory by the restart of the Agena B engine. Failure of a timer in the spacecraft payload caused loss of both internal and ground control over the vehicle. The Goldstone Tracking Station maintained contact with the spacecraft until it passed behind the left edge of the moon on April 26. It impacted at a speed of 9,617 km per hour, the first American spacecraft to land on the lunar surface. The Agena B second stage passed to the right of the moon and later went into orbit around the sun. Lunar photography objectives were not achieved. References: 2, 6, 278, 296. 1962 April 24 - Indecision on the lunar mission mode causing delays in Apollo program Nation: USA. Program: Apollo. Spacecraft: Apollo LM, Apollo Lunar Landing. MSC Associate Director Walter C. William reported to the Manned Space Flight Management Council that the lack of a decision on the lunar mission mode was causing delays in various areas of the Apollo spacecraft program, especially the requirements for the portions of the spacecraft being furnished by NAA. References: 16. 1962 April 24 - Launch Vehicle: Nova. Model: Nova 8L. Delay in award of a Nova launch vehicle study contract Nation: USA. Program: Apollo. The Manned Space Flight Management Council decided to delay the awarding of a Nova launch vehicle study contract until July 1 at the earliest to allow time for an in-house study of bids submitted and for further examination of the schedule for a manned lunar landing using the direct ascent technique. References: 16. 1962 April 24 - Launch Vehicle: Proton. Model: Proton 8K82. Approval to proceed with the UR-500 (8K82) was provided in a Central Committee decree Nation: USSR. Spacecraft: LK-1. Council of Soviet Ministers (SM) Decree 'On start of work on the UR-500 missile and carrier-rocket' was issued. The rocket was to be built initially for the GR-2 requirement - a heavy rocket that could be used to launch large military payloads into space as well as act as a ballistic missile for multiple nuclear warheads up to 100 MT in yield. The decree ordered development of this powerful new rocket to be completed within three years. This was a difficult task, considering the factory and launch facilities that would have to be built to allow testing of the rocket to begin. The draft project UR-500 was completed in 1963. 1962 April 24 - 04:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. LV Configuration: Kosmos 63S1 4LK. Cosmos 3 Nation: USSR. Program: MS. Payload: 2MS s/n 1. Mass: 330 kg (720 lb). Class: Technology. Spacecraft: 2MS. Agency: RVSN. Perigee: 216 km (134 mi). Apogee: 707 km (439 mi). Inclination: 49.00 deg. Period: 93.80 min. COSPAR: 1962-Nu-1. USAF Sat Cat: 281. Decay Date: 1962-10-17. Cosmic ray, radiation data. Investigation of the upper atmosphere and outer space; development of elements in the design of space craft. References: 2, 6. 1962 April 25 - Launch Site: Edwards. Launch Complex: RW04/22. Launch Pad: -. Launch Vehicle: X-15. LV Configuration: X-15 2- A-38. FAILURE: Failure. X-15A test Nation: USA. Agency: NASA/USAF. Apogee: 14 km (8 mi). Maximum Speed - 5879 kph. Maximum Altitude - 32160 m. References: 2. 1962 April 25 - 14:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC34. Launch Pad: -. Launch Vehicle: Saturn I. Model: Saturn C-1. LV Configuration: Saturn C-1 SA-2. Nation: USA. Agency: NASA. Apogee: 145 km (90 mi). Second suborbital test of Saturn I. The Saturn SA-2 first stage booster was launched successfully from Cape Canaveral. The rocket was blown up intentionally and on schedule about 2.5 minutes after liftoff at an altitude of 65 miles, dumping the water ballast from the dummy second and third stages into the upper atmosphere. The experiment, Project Highwater, produced a massive ice cloud and lightning-like effects. The eight clustered H-1 engines in the first stage produced 1.3 million pounds of thrust and the maximum speed attained by the booster was 3,750 miles per hour. Modifications to decrease the slight fuel sloshing encountered near the end of the previous flight test were successful. References: 2. 1962 April 25 - 16:50 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-1. Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 April 26 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. First West Coast launch of a Scout space booster. Nation: USA. References: 88. 1962 April 26 - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-2. LV Configuration: Scout X-2 S111. FAILURE: Failure. Solrad 4B Nation: USA. Payload: GRAB 4B. Mass: 91 kg (200 lb). Class: Sigint. Spacecraft: GRAB. Agency: U.S. Navy. COSPAR: F620426A. Decay Date: 1962-04-26. Solar radiation monitor. References: 126. 1962 April 26 - 10:02 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K. Cosmos 4 Nation: USSR. Payload: Zenit-2 11F61 s/n 2. Mass: 4,610 kg (10,160 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: RVSN. Perigee: 285 km (177 mi). Apogee: 317 km (196 mi). Inclination: 65.00 deg. Period: 90.50 min. COSPAR: 1962-Xi-1. USAF Sat Cat: 287. Duration: 3.00 days. Decay Date: 1962-04-29. Flight: Vostok 3, Vostok 4. Area survey photo reconnaissance satellite. Program partially completed. Failure of primary spacecraft orientation system. It was to spend four days in space, to be followed by another mission during 5-10 May. This meant that Vostok 3/4 could not be launched before 20-30 May. The cosmonaut prime crew returned from their in-suit parachute training at Fedosiya. References: 2, 6, 93, 175, 376. 1962 April 26 - 16:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.110GI. Japan / US Ionosphere D-Reg Ionosphere mission Nation: USA. Agency: NASA/RRLJ. Apogee: 128 km (79 mi). References: 2. 1962 April 26 - 18:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta. LV Configuration: Thor Delta 320/D9. Ariel 1 Nation: UK. Payload: UK 1 (S-51). Mass: 60 kg (132 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Ariel. Agency: NASA, United Kingdom. Perigee: 398 km (247 mi). Apogee: 1,203 km (747 mi). Inclination: 53.80 deg. Period: 100.80 min. COSPAR: 1962-Omicron-1. USAF Sat Cat: 285. Decay Date: 1976-03-31. Ionospheric studies; returned X-ray, ionospheric, cosmic ray data. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6. 1962 April 26 - 18:56 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 118D / Agena B SPS 2401. Samos 7 Nation: USA. Payload: Samos E-6 no. 1 / Agena B 2401. Mass: 1,588 kg (3,500 lb). Class: Surveillance. Type: Military. Spacecraft: Samos. Agency: U.S. Air Force. COSPAR: 1962-Pi-1. USAF Sat Cat: 286. Decay Date: 1962-04-28. Second generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results. References: 2, 6, 278. FTV 2401 RV Nation: USA. Payload: E-6 RV. Spacecraft: Samos. Agency: USAF. COSPAR: 1962-Pi-xx. References: 2, 279. 1962 April 27 - 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 April 27 - 23:24 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 140D. Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2. 1962 April 28 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: RT-1. Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi). References: 2. 1962 April 29 - 00:30 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 333 / Agena B 1125. KH-4 9033 Nation: USA. Payload: KH-4 s/n 9033 / Agena B 1125. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 180 km (110 mi). Apogee: 475 km (295 mi). Inclination: 73.10 deg. Period: 91.10 min. COSPAR: 1962-Rho-1. USAF Sat Cat: 290. Decay Date: 1962-05-26. KH-4. Mission failed. Parachute ejector squibs holding parachute container cover failed to fire. No recovery. References: 2, 6. 1962 April 30 - Launch Vehicle: Atlas. Model: Atlas D. Swimmer training for Mercury MA-7 Nation: USA. Program: Mercury. Swimmer training was started for the Mercury-Atlas 7 (MA-7) manned orbital mission recovery area. Instruction consisted of films, briefings, exercises in deploying the auxiliary flotation collar, and jumps from a helicopter. References: 483. 1962 April 30 - 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: 200 km (120 mi). References: 2. 1962 April 30 - 18:23 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 1-27-48. X-15A Alt, Low q, Aero test Nation: USA. Agency: NASA/USAF. Apogee: 75 km (46 mi). Design altitude flight. Maximum Speed - 5614 kph. Maximum Altitude - 75190 m. References: 2. 1962 May - Mudflap approved. Nation: USA. Spacecraft: Program 505. US Secretary of Defence McNamara approved the US Army request to proceed with development, under the code-name Mudflap. America's first ASAT system was later known as Program 505, which used prototype Nike Zeus DM-15S anti-ballistic missiles, operated from Kwajalein Atoll by the U.S. Army. 1962 May - Launch Vehicle: GR-1. Draft project for the GR-1 was completed Nation: USSR. 1962 May - Launch Vehicle: Proton. Model: Proton 8K82. Advanced project for the Proton UR-500 completed Nation: USSR. The initial design featured four ungimballed Glushko engines mounted below the core, with four steerable Kosberg engines on the lateral tanks. The second stage of the UR-500 was a larger-diameter variant of the first stage of the UR-200, with the engines gimballed for directional control. The third stage used the UR-200’s fixed engine with a four-nozzled steering engine. In order to meet the constant diameter requirement the third stage used toroidal propellant tanks. 1962 May 1 - 13:13 GMT - Launch Site: Woomera. Launch Complex: LA5B. Launch Pad: LA5B?. Launch Vehicle: Black Knight. Model: Black Knight 201. LV Configuration: Black Knight-201 BK.15. Gaslight Re-entry Vehicle test Nation: UK. Agency: RAE. Apogee: 795 km (493 mi). References: 2. 1962 May 2 - 22:53 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.361. Day airglow Aeronomy mission Nation: USA. Agency: USAF. Apogee: 275 km (170 mi). References: 2. 1962 May 2 - 23:44 GMT - Launch Site: Johnston Island. Launch Complex: LE1. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2E. LV Configuration: Thor DSV-2E 177. TIGERFISH test Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). References: 2. 1962 May 3 - Titov meets Glenn Nation: USSR. Spacecraft: Mercury. They view the Redstone and Atlas rockets and a Mercury space capsule. Kamanin finds the Mercury very cramped, but notes that it is equipped with all the necessities. Glenn tells him it was possible for the astronaut to wear a parachute, but Glenn chose not to - he didn't believe he could really use it in an emergency anyway. Afterwards they were introduced to President Kennedy and Vice-President Johnson. References: 376. 1962 May 3 - 18:03 GMT - Launch Site: Wallops Island. Launch Complex: LA1. Launch Pad: -. Launch Vehicle: Iris. LV Configuration: Iris NASA 5.04GA. Structure Aeronomy mission Nation: USA. Agency: NASA. Apogee: 113 km (70 mi). References: 2. 1962 May 3 - 20:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.21GI. ELF electron trap Ionosphere mission Nation: USA. Agency: NASA. Apogee: 845 km (525 mi). References: 2. 1962 May 4 - Titov in Baltimore Nation: USSR. Spacecraft: Mercury, Vostok. Titov and Kamanin meet journalist Drew Pierson, who claims that five Soviet cosmonauts died before Gagarin flew. They are introduced to Wernher Von Braun. In the afternoon they go to a barbecue at Glenn's house in Virginia. Kamanin carefully notes the technical information he has gleaned: Glenn wore no parachute; the Mercury's solid fuel retrorockets fire in 28 seconds, much more quickly and with more force than the Vostok's low-thrust liquid propellant engine; it is planned to launch a modernised version of Mercury on a one-day flight by the end of 1962; the astronauts train in the centrifuge to 16 G's (versus 12 G's for the cosmonauts); the NASA manned space headquarters is moving to Texas; Mercury is only capable of water landings, no work has been done on land landings or equipping the capsule with an ejection seat; several Amerrican women are considered fit for spaceflight, and the first American woman could make a three-orbit flight in the second half of 1962. References: 376. 1962 May 4 - 01:41 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-18 (A2MG-1). Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 May 4 - 21:43 GMT - Launch Site: Vandenberg. Launch Complex: 395-A1. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-34. Research and development Category II test Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi). References: 2. 1962 May 5 - Launch Site: San Nicolas. Launch Complex: -. Launch Pad: -. Launch Vehicle: Caleb. LV Configuration: Caleb SIP. Test mission Nation: USA. Agency: USN NOTS. Apogee: 20 km (12 mi). References: 2. 1962 May 6 - Preliminary Statement of Work for Apollo lunar excursion module Nation: USA. Program: Apollo. Spacecraft: Apollo LM. A preliminary Statement of Work for a proposed lunar excursion module was completed, although the mission mode had not yet been selected. References: 16. 1962 May 6 - 05:41 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trailblazer. Model: Trailblazer 2. LV Configuration: Trailblazer 2-M TB IIb. Meteor 1 Re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 280 km (170 mi). References: 2. 1962 May 6 - 23:17 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 12.5 N x 134.0 W. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2 A1?. FRIGATE BIRD Nuclear test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). The only US test of an operational ballistic missile with a live 600 kiloton warhead. A Polaris A2 missile was launched from the ballistic missile submarine Ethan Allen (SSBN-608) 2800 km east-northeast of Christmas Island. The re-entry vehicle reached the target zone 1890 km away and detonated at 3,300 m. The resulting mushroom cloud was observed by the submarines Carbonero (SS-337) and Medregal (SS-480), both stationed within 25 km of the predicted impact point. References: 2. 1962 May 7 - Mercury MA-7 delays Nation: USA. Program: Mercury. Flight: Mercury MA-7. NASA announced that the Mercury-Atlas 7 (MA-7) manned orbital flight would be delayed several days due to checkout problems with the Atlas launch vehicle. References: 483. 1962 May 8 - 15:05 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.46NP. Radar test Technology test Nation: USA. Agency: NASA. Apogee: 196 km (121 mi). References: 2. 1962 May 8 - 18:01 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 2-22-40. X-15A Heat T/ASAS/High al. test Nation: USA. Agency: NASA/USAF. Apogee: 21 km (13 mi). Maximum Speed - 5670 kph. Maximum Altitude - 21460 m. First flight to exceed 2000 psf (136 bar) dynamic pressure. References: 2. 1962 May 8 - 19:49 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36A. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Centaur. LV Configuration: Atlas Centaur F-1. FAILURE: Vehicle exploded due to insulation problems on the Atlas. Research and development test Nation: USA. Agency: NASA. Apogee: 6.00 km (3.70 mi). First Centaur flight (unsuccessful). References: 2. 1962 May 9 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Belier. Model: Belier I. LV Configuration: Belier B02. FAILURE: Failure. Test mission Nation: France. Agency: CNES. Apogee: 0 km ( mi). References: 2. 1962 May 10 - Launch Site: Lowry AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. Titan I ICBM 849th SMS (nine missiles) declared operational at Lowry AFB Nation: USA. 1962 May 10 - 12:07 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar 314 AB011. FAILURE: Able-Star failed to ignite. Anna 1A Nation: USA. Payload: Anna 1A. Mass: 160 kg (350 lb). Class: Earth. Type: Geodetic. Spacecraft: Anna. Agency: U.S. Army, U.S. Navy, U.S. Air Force, NASA. COSPAR: F620510A. Decay Date: 1962-05-10. USN, USAF, US Army, NASA joint program. References: 126. 1962 May 11 - Launch Vehicle: Little Joe II. Convair contract for the Little Joe II launch vehicle Nation: USA. Program: Apollo. NASA awarded a letter contract to General Dynamics/Convair to design and manufacture the Little Joe II test launch vehicle which would be used to boost the Apollo spacecraft on unmanned suborbital test flights. The Little Joe II would be powered by clustered solid-fuel engines. At the same time, a separate 30-day contract was awarded to Convair to study the control system requirements. White Sands Missile Range, N. Mex., had been selected for the Little Joe II max q abort and high-altitude abort missions. References: 16. 1962 May 11 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-4. Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 May 11 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 413. Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2. 1962 May 12 - Launch Vehicle: Atlas, Titan. Project Gemini cost estimates had tripled from the original estimate of $250 million. Nation: USA. Program: Gemini. Spacecraft: Gemini. James E. Webb, NASA's new Administrator, reviewed the Gemini program. Project Gemini cost estimates at this point ($744.3 million) had increased substantially over the original estimate of $250 million. Estimated spacecraft cost had risen from $240.5 to $391.6 million; Titan II cost, from $113.0 to $161.8 million; Atlas-Agena, from $88.0 to $106.3 million; and supporting development (including the paraglider program), from $29.0 to $36.8 million. Estimated operations costs had declined from $59.0 to $47.8 million. 1962 May 12 - 00:31 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 127D. Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). References: 2. 1962 May 15 - Launch Vehicle: Proton. Model: Proton 8K82. UR-500 advanced project published. Nation: USSR. Program: GR-2. Manufacturer: OKB-52. References: 273. 1962 May 15 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Belier. Model: Belier I. LV Configuration: Belier B03. FAILURE: Failure. Test mission Nation: France. Agency: CNES. Apogee: 0 km ( mi). References: 2. 1962 May 15 - 19:36 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 334 / Agena B 1126. KH-5 9034A Nation: USA. Payload: KH-5 s/n 9034A/Agena B 1126. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-5. Agency: U.S. Air Force. Perigee: 283 km (175 mi). Apogee: 550 km (340 mi). Inclination: 82.30 deg. Period: 93.00 min. COSPAR: 1962-Sigma-1. USAF Sat Cat: 292. Decay Date: 1963-11-26. KH-5; film capsule recovered 4.1 days later. First successful KH-5 mission. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6. 1962 May 16-17 - Launch Vehicle: Titan. Model: Titan 2. A Launch Vehicle-Spacecraft Interface Working Group was established. Nation: USA. Gemini Project Office (GPO) and Aerospace had agreed on the need for such a group at a Gemini-Titan coordination meeting on May 11. The main function of the group, composed of Martin and McDonnell personnel with a McDonnell representative as chairman, was to provide mutual exchange of design and physical data on mechanical, electrical, and structural details between the spacecraft contractor and the booster contractor. The group would make no policy decisions; its actions were to be reviewed at regularly scheduled coordination meetings held by GPO. 1962 May 16 - 17:03 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.112GI. Japan / US ionosphere Ionosphere mission Nation: USA. Agency: NASA/RRLJ. Apogee: 121 km (75 mi). References: 2. 1962 May 17 - Mercury MA-7 postponed a second time Nation: USA. Program: Mercury. Flight: Mercury MA-7. The Mercury-Atlas 7 (MA-7) manned orbital mission was postponed a second time because of necessary modifications to the altitude-sensing instrumentation in the parachute-deployment system. References: 483. 1962 May 17 - 02:04 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.111GI. Ionosphere mission Nation: USA. Agency: NASA/RRLJ. Apogee: 127 km (78 mi). References: 2. 1962 May 18 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 414. Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2. 1962 May 18 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C10. Test mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 May 18 - 18:01 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.91UA. Composition Aeronomy mission Nation: USA. Agency: NASA. Apogee: 135 km (83 mi). References: 2. 1962 May 19 - Mercury MA-7 postponed a third time Nation: USA. Program: Mercury. Flight: Mercury MA-7. A third postponement was made for the Mercury-Atlas 7 (MA-7) flight mission due to irregularities detected in the temperature control device on a heater in the Atlas flight control system. References: 483. 1962 May 21 - Launch Vehicle: Titan. Model: Titan 2. Amendment No. 6 to the Gemini launch vehicle procurement contract assigned $2.609 million to fund the construction necessary to convert pad 19 at Cape Canaveral for Gemini flights. Nation: USA. The Air Force had originally constructed pad 19 for the Titan I development program. Following the final Titan I development flight (January 29) from the Cape, design of the required modifications had begun in February. In April, Gemini Project Office decided that Pad 19 would have an erector rather than a gantry, the upper third of which would be designed as a white room. The final design review of pad 19 modifications took place July 9-10, and the Army Corps of Engineers awarded the construction contract to Consolidated Steel, Cocoa Beach, Florida. Construction began in September. Work was completed and pad 19 was activated on October 17, 1963. 1962 May 22 - 18:04 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 1-28-49. X-15A Local flow test Nation: USA. Agency: NASA/USAF. Apogee: 30 km (18 mi). Maximum Speed - 5551 kph. Maximum Altitude - 30600 m. Roller coaster flight with three peaks for local airflow investigation. References: 2. 1962 May 23 - Launch Vehicle: Titan. Model: Titan 2. Avco proposal for a space station. Nation: USA. Spacecraft: MOL. Representatives from Avco Manufacturing Corporation made a presentation to MSC on a proposal for a space station. Prime purpose of the station, company spokesmen said, was to determine the effects of zero-g on the crew's ability to stand reentry and thus fix the limit that man could safely remain in orbit. Avco's proposed station design comprised three separate tubes about 3 m in diameter and 6 m long, launched separately aboard Titan IIs and joined in a triangular shape in orbit. A standard Gemini spacecraft was to serve as ferry vehicle. 1962 May 23 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-6. Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 May 23 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-5. Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 May 24 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI39. Aeronomy mission Nation: France. Agency: FR. Apogee: 168 km (104 mi). References: 2. 1962 May 24 - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-2M. LV Configuration: Scout X-2M S112. FAILURE: Failure. P 35-1 Nation: USA. Program: DMSP. Payload: FTV 3501. Class: Earth. Type: Weather. Spacecraft: Program 35. Agency: AFSC. COSPAR: F620524A. Decay Date: 1962-05-24. Military weather satellite to provide targetting information for reconnaisance satellites. References: 126. 1962 May 24 - 10:50 GMT - Launch Site: Akita. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8. LV Configuration: Kappa 8 K-8-10. FAILURE: Failure. Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 0 km ( mi). References: 2. 1962 May 24 - 12:45 GMT - Launch Site: Cape Canaveral. Launch Complex: LC14. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 107D. Mercury MA-7 Nation: USA. Program: Mercury. Payload: Mercury SC18. Mass: 1,349 kg (2,974 lb). Class: Manned. Type: Spacecraft. Spacecraft: Mercury. Location of Spacecraft: Museum of Science and Industry, Chicago, IL. Agency: NASA. Perigee: 154 km (95 mi). Apogee: 260 km (160 mi). Inclination: 32.50 deg. Period: 88.50 min. COSPAR: 1962-Tau-1. USAF Sat Cat: 295. Duration: 0.21 days. Decay Date: 1962-05-24. Crew: Carpenter. Flight: Mercury MA-7. Scott Carpenter in Aurora 7 is enthralled by his environment but uses too much orientation fuel. Yaw error and late retrofire caused the landing impact point to be over 300 km beyond the intended area and beyond radio range of the recovery forces. Landing occurred 4 hours and 56 minutes after liftoff. Astronaut Carpenter was later picked up safely by a helicopter after a long wait in the ocean and fears for his safety. NASA was not impressed and Carpenter left the agency soon thereafter to become an aquanaut. References: 2, 6, 26, 33, 59, 60, 278. 1962 May 25 - 12:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.48GT. Sea recovery test/Ionosphere mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi). Sea recovery test mission. References: 2. 1962 May 26 - Launch Vehicle: Saturn V. Saturn F-1 engine first fired at full power Nation: USA. Program: Apollo. The F-1 engine was first fired at full power more than 1.5 million pounds of thrust) for 2.5 minutes at Edwards Rocket Site, Calif. References: 16. 1962 May 26 - 18:04 GMT - Launch Site: Point Mugu. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. PM-13 Altitude test Nation: USA. Agency: USA. Apogee: 200 km (120 mi). References: 2. 1962 May 28 - 03:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. LV Configuration: Kosmos 63S1 3LK. Cosmos 5 Nation: USSR. Program: MS. Payload: 2MS s/n 2. Mass: 280 kg (610 lb). Class: Technology. Spacecraft: 2MS. Agency: RVSN. Perigee: 192 km (119 mi). Apogee: 1,578 km (980 mi). Inclination: 49.10 deg. Period: 102.60 min. COSPAR: 1962-Upsilon-1. USAF Sat Cat: 297. Decay Date: 1963-05-02. Monitored artificial radiation. Investigation of the upper atmosphere and outer space; development of elements in the design of space craft. References: 2, 6. 1962 May 29 - Launch Vehicle: Saturn V. Mobile launcher concept for the Saturn C-5 approved Nation: USA. Program: Apollo. The Manned Space Flight Management Council approved the mobile launcher concept for the Saturn C-5 at Launch Complex 39, Merritt Island, Fla. References: 16. 1962 May 29 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C12. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 May 29 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: Bacchus?. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C18. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 May 29 - Launch Site: Reggane. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C15. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 May 30 - 01:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 336 / Agena B 1128. KH-4 9035 Nation: USA. Payload: KH-4 s/n 9035 / Agena B 1128. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 192 km (119 mi). Apogee: 350 km (210 mi). Inclination: 74.10 deg. Period: 89.90 min. COSPAR: 1962-Phi-1. USAF Sat Cat: 302. Decay Date: 1962-06-11. KH-4; film capsule recovered 3.1 days later. Slight corona static on film. References: 2, 6. 1962 May 31 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI38. Aeronomy mission Nation: France. Agency: FR. Apogee: 100 km (60 mi). References: 2. 1962 May 31 - 03:01 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: Long Tom. LV Configuration: Long Tom LT14. Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 125 km (77 mi). References: 2. 1962 May 31 - 17:08 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 102. ERCS/279L 1 Communications mission Nation: USA. Agency: USAF. Apogee: 830 km (510 mi). References: 2. 1962 June 1 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 1014. Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Successful missile test. Missed aimpoint by 378 m. References: 2. 1962 June 1 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI41. Aeronomy mission Nation: France. Agency: FR. Apogee: 100 km (60 mi). References: 2. 1962 June - Launch Vehicle: Martlet. Model: Martlet 1. Martlet One Flight Vehicle designed Nation: Canada. This was the first generation test vehicle for the HARP project. 1962 June 1 - 09:38 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92. LV Configuration: Vostok 8A92 E15000-01. FAILURE: Shutdown of Block B strap-on engine stage 1.8 seconds after liftoff. The booster crashed 300 m from the pad. Pad damaged. Zenit-2 11F61 s/n 3 Nation: USSR. Payload: Zenit-2 11F61 s/n 3. Mass: 4,610 kg (10,160 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: RVSN. COSPAR: F620601A. Decay Date: 1962-06-01. Area survey photo reconnaissance satellite. Third attempted launch of Zenit photo-reconnaissance satellite. It blew up 300 m from the pad, and did enough damage to put the launch complex out of operation for a month. Therefore the Vostok 3/4 launches could not take place until the end of July at the earliest. References: 93. 1962 June 1 - 18:51 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 2-23-43. X-15A ASAS, 23 alpha, M=5 test Nation: USA. Agency: NASA/USAF. Apogee: 40 km (24 mi). Maximum Speed - 5913 kph. Maximum Altitude - 40420 m. Steepest reentry descent with highest angle of attack (27 degrees) to date. References: 2. 1962 June 2 - 00:31 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 335 / Agena B 1127. KH-4 9036 Nation: USA. Payload: KH-4 s/n 9036 / Agena B 1127. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 211 km (131 mi). Apogee: 401 km (249 mi). Inclination: 74.50 deg. Period: 90.60 min. COSPAR: 1962-Chi-1. USAF Sat Cat: 304. Decay Date: 1962-06-28. KH-4. Mission failed. During air catch, chute tore loose. Capsule sank. References: 2, 6. Oscar 2 Nation: USA. Program: Oscar. Mass: 10 kg (22 lb). Class: Communications. Type: Amateur Radio. Spacecraft: Oscar. Agency: U.S. Air Force. Perigee: 188 km (116 mi). Apogee: 339 km (210 mi). Inclination: 74.20 deg. Period: 89.80 min. COSPAR: 1962-Chi-2. USAF Sat Cat: 305. Decay Date: 1962-06-21. OSCAR II was launched piggyback with a United States Air Force satellite. OSCAR II was very similar to OSCAR I. Differences included (1) changing the surface thermal coatings to achieve a cooler internal spacecraft environment, (2) modifying the sensing system so the satellite temperature could be measured accurately as the batteries decayed, and (3) lowering the transmitter power output to 100 mW to extend the life of the onboard battery. OSCAR II lasted 18 days ceasing operation on June 20, 1962 and re-entered June 21, 1962. References: 2, 6. 1962 June 2 - 19:17 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-7. Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 June 2 - 22:36 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2PE-8. Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 June 3 - Launch Vehicle: UR-200. US RORSAT development plans. Nation: USSR. Spacecraft: US-A. Decree 'On course of work on the US reconnaissance satellite system launched on the UR-2OO' was issued. References: 474. 1962 June 4 - Launch Site: Reggane. Launch Complex: -. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI42. FAILURE: Failure. Aeronomy mission Nation: France. Agency: FR. Apogee: 100 km (60 mi). References: 2. 1962 June 4 - 09:44 GMT - Launch Site: Johnston Island. Launch Complex: LE1. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2E. LV Configuration: Thor DSV-2E 199. BLUEGILL Nuclear test Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). Initial attempt to launch a live nuclear weapon using the Thor IRBM from Johnston Atoll. The range safety radar had been unreliable before launch,. Five minutes after launch, after shutdown of the booster, the Johnston missile tracking system failed. Unable to monitor the warhead's flight path, the range safety officer destroyed it 10 minutes later, prior to warhead detonation. References: 2. 1962 June 5 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C14. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 June 5 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: Bacchus?. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C19. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 June 5 - Launch Site: Reggane. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C17. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 June 5 - Launch Site: Reggane. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C16. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 June 5 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: Bacchus?. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C09. Aeronomy mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi). References: 2. 1962 June 5 - 12:45 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AB3.133. Extreme ultraviolet Monochromator Aeronomy / solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 216 km (134 mi). References: 2. 1962 June 6 - Launch Site: Reggane. Launch Complex: -. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI43. Aeronomy mission Nation: France. Agency: FR. Apogee: 100 km (60 mi). References: 2. 1962 June 6 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Belier I. LV Configuration: Belier B08. FAILURE: Failure. Aeronomy mission Nation: France. Agency: CNES. Apogee: 0 km ( mi). References: 2. 1962 June 6 - 03:00 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5C. LV Configuration: Skylark-5C SL35C. Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 240 km (140 mi). References: 2. 1962 June 6 - 23:40 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.19UA. UM Pitot 1 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 125 km (77 mi). References: 2. 1962 June 7 - Launch Vehicle: Saturn I, Saturn V. von Braun recommends lunar orbit rendezvous mode for Apollo Nation: USA. Program: Apollo. Spacecraft: Apollo CSM, Apollo Lunar Landing. Wernher von Braun, Director, Marshall Space Flight Center, recommended to the NASA Office of Manned Space Flight that the lunar orbit rendezvous mode be adopted for the lunar landing mission. He also recommended the development of an unmanned, fully automatic, one-way Saturn C-5 logistics vehicle in support of the lunar expedition; the acceleration of the Saturn C-1B program; the development of high-energy propulsion systems as a backup for the service module and possibly the lunar excursion module; and further development of the F-1 and J-2 engines to increase thrust or specific impulse. References: 16. 1962 June 7 - 00:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.43GA. Grenade, Inflating Sphere 4 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 120 km (70 mi). References: 2. 1962 June 7 - 00:56 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.21CA. Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 162 km (100 mi). References: 2. 1962 June 7 - 14:45 GMT - Launch Site: Sonmiani. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun Rehbar 1. Sodium release Aeronomy mission Nation: Pakistan. Agency: SUPARCO. Apogee: 126 km (78 mi). References: 2. 1962 June 7 - 18:21 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II N-1. Mk 6 re-entry vehicle test launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). References: 2. 1962 June 7 - 18:29 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 1-29-50. X-15A Local flow, M=5 test Nation: USA. Agency: NASA/USAF. Apogee: 31 km (19 mi). Maximum Speed - 5908 kph. Maximum Altitude - 31580 m. References: 2. 1962 June 8 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Delta. Model: Thor. Last launch of a Thor IRBM from Vandenberg Nation: USA. Last launch of a Thor IRBM from Vandenberg. (First launch and first missile fired from Vandenberg AFB on 16 December 1958.) References: 88. 1962 June 8 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 415. Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2. 1962 June 8 - 00:53 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.44GA. Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi). References: 2. 1962 June 11 - VVS Conference: Military Use of Space - the Short-Term Perspective Nation: USSR. Spacecraft: Soyuz A, Soyuz B, Soyuz V, Apollo CSM. The projection is made that the US will surpass the USSR in space in 1963-1964. Kennedy's 1961 speech announcing the Apollo project to land on the moon was passed to Vershinin for comment, but no reply was ever received. Rudenko, Vershinin, and especially Malinovskiy see no role for piloted space flight, let alone flights to the moon. America, with its superior electronics capability, is still proceeding with development of manned spacecraft that require the active piloting of the astronaut. Why then, Kamanin fumes, is the USSR trying to develop completely automated manned spacecraft? Military space is being run in the USSR by men who know nothing of it, he notes. Rudenko is ill, and not even at the conference. References: 376. 1962 June 11 - 14:50 GMT - Launch Site: Sonmiani. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun Rehbar 2. Sodium release Aeronomy mission Nation: Pakistan. Agency: SUPARCO. Apogee: 116 km (72 mi). References: 2. 1962 June 12 - 20:04 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 3-5-9. X-15A RCS check, M=5 test Nation: USA. Agency: NASA/USAF. Apogee: 56 km (34 mi). Maximum Speed - 5659 kph. Maximum Altitude - 56270 m. References: 2. 1962 June 12 - 21:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AB3.134. Extreme ultraviolet Monochromator Solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 299 km (185 mi). References: 2. 1962 June 15 - 16:48 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.12GI. Ionosphere mission Nation: USA. Agency: NASA. Apogee: 143 km (88 mi). References: 2. 1962 June 16-22 - 100 percent oxygen atmosphere for Apollo would save 30 pounds Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Results of a preliminary investigation by NAA showed that a 100 percent oxygen atmosphere for the command module would save about 30 pounds in weight and reduce control complexity. References: 16. 1962 June 17 - 18:14 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 115D / Agena B SPS 2402. Samos 8 Nation: USA. Payload: Samos E-2 no. 2 / Agena B 2402. Mass: 1,860 kg (4,100 lb). Class: Surveillance. Type: Military. Spacecraft: Samos. Agency: U.S. Air Force. Perigee: 198 km (123 mi). Apogee: 198 km (123 mi). Inclination: 96.20 deg. Period: 88.40 min. COSPAR: 1962-Psi-1. USAF Sat Cat: 307. Decay Date: 1962-06-18. First generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results. References: 2, 6, 278. FTV 2402 RV Nation: USA. Payload: E-6 RV. Spacecraft: Samos. Agency: USAF. COSPAR: 1962-Psi-xx. References: 2, 279. 1962 June 18 - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 343 / Agena B 2312. Ferret 2 Nation: USA. Payload: Ferret 2 / Agena B 2312. Mass: 1,500 kg (3,300 lb). Class: Sigint. Spacecraft: Ferret. Agency: U.S. Air Force. Perigee: 347 km (215 mi). Apogee: 377 km (234 mi). Inclination: 82.10 deg. Period: 91.80 min. COSPAR: 1962-Omega-2. USAF Sat Cat: 308. Decay Date: 1963-10-30. References: 2, 6. FTV 2312 Nation: USA. Program: ELINT. Payload: Ferret 2. Spacecraft: Ferret. Agency: USAF. COSPAR: 1962-Omega-1. USAF Sat Cat: 308. Decay Date: 1963-10-30. References: 2, 279. 1962 June 19 - 00:30 GMT - Launch Site: Vandenberg. Launch Complex: LE-8. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 269. Combat training launch Nation: USA. Agency: RAF. Apogee: 520 km (320 mi). References: 2. 1962 June 19 - 06:59 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AB3.352. AS&E-3 (Sco X-1) X-ray Astronomy mission Nation: USA. Agency: USAF. Apogee: 224 km (139 mi). References: 2. 1962 June 19 - 12:19 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta. LV Configuration: Thor Delta 321/D10. Tiros 5 Nation: USA. Program: Tiros. Payload: Tiros E (A-50). Mass: 129 kg (284 lb). Class: Earth. Type: Weather. Spacecraft: Tiros. Agency: NASA. Perigee: 580 km (360 mi). Apogee: 880 km (540 mi). Inclination: 58.10 deg. Period: 99.40 min. COSPAR: 1962-A-Alpha-1. USAF Sat Cat: 309. Returned 58226 cloud cover images. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 2, 6. 1962 June 20 - 05:20 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5C. LV Configuration: Skylark-5C SL45. Solar X-rays / La / Gren. / FS Aeronomy / solar x-ray mission Nation: Australia. Agency: WRE/RAE. Apogee: 227 km (141 mi). References: 2. 1962 June 20 - 08:46 GMT - Launch Site: Johnston Island. Launch Complex: LE1. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DSV-2E. LV Configuration: Thor DSV-2E 193. FAILURE: Failure. STARFISH Nuclear test Nation: USA. Agency: USAF. Apogee: 10 km (6 mi). References: 2. 1962 June 20 - 13:29 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.26NP. LeRC LH2 test Technology test Nation: USA. Agency: NASA. Apogee: 158 km (98 mi). References: 2. 1962 Summer-Fall - Microcircuits to be used on the Apollo computer Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NASA and MIT agreed that the Instrumentation Laboratory would use the microcircuit for the prototype Apollo onboard computer. The Fairchild Controls Corporation microcircuit was the only one available in the United States. References: 16. 1962 June 21 - 17:47 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 3-6-10. X-15A MH-96 Demo, M=5 test Nation: USA. Agency: NASA/USAF. Apogee: 75 km (46 mi). Maximum Speed - 5858 kph. Maximum Altitude - 75190 m. References: 2. 1962 June 23 - 00:30 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 339 / Agena B 1129. KH-4 9037 Nation: USA. Payload: KH-4 s/n 9037 / Agena B 1129. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 199 km (123 mi). Apogee: 314 km (195 mi). Inclination: 75.10 deg. Period: 89.60 min. COSPAR: 1962-A-Beta-1. USAF Sat Cat: 315. Decay Date: 1962-07-07. KH-4. Corona static occurs on some film. References: 2, 6. 1962 June 26 - 08:38 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 108. Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 116 km (72 mi). References: 2. 1962 June 26 - 10:57 GMT - Launch Site: Vandenberg. Launch Complex: 576B3. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 21D. NTMP K-1 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi). First launch of an Atlas from Vandenberg AFB as a target for an Army Nike-Zeus from Kwajalein. References: 2. 1962 June 26 - 11:30 GMT - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. FAILURE: Failure. First launch of an Army Nike-Zeus from Kwajalein Nation: USA. Agency: USA. Apogee: 10 km (6 mi). First launch of an Army Nike-Zeus from Kwajalein against an Atlas from Vandenberg AFB. References: 2. 1962 June 27 - NTK formed. Nation: USSR. Ministry of Defence Decree 'On formation of the Scientific-Technical Council of the Strategic Missile Forces' was issued. References: 474. 1962 June 27 - US Plans in Space Nation: USSR. Program: Vostok. Kamanin notes that the US launched 86 satellites up to June 1, 1962 compared to only 21 by the USSR. He believes the Soviet reply should be a vigorous program that would launch 10 to 12 Vostok manned spacecraft in 1963 alone; to finally resolve organisational issues that hindered the Soviet program; and to adopt a goal of landing a man on the moon. References: 376. 1962 June 27 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Berenice. LV Configuration: Berenice 001. Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 270 km (160 mi). References: 2. 1962 June 27 - 14:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. Ionosphere mission Nation: USA. Agency: USN?. Apogee: 200 km (120 mi). References: 2. 1962 June 27 - 21:08 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 1-30-51. X-15A High alpha, Mach 6 test Nation: USA. Agency: NASA/USAF. Apogee: 37 km (22 mi). Unofficial world speed record. Maximum Speed - 6603 kph. Maximum Altitude - 37700 m. References: 2. 1962 June 28 - 00:10 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. Ionosphere mission Nation: USA. Agency: USN?. Apogee: 200 km (120 mi). References: 2. 1962 June 28 - 01:09 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena D. LV Configuration: Thor Agena D 340 / Agena D 1151. KH-4 9038 Nation: USA. Payload: KH-4 s/n 9038 / Agena D 1151. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: U.S. Air Force. Perigee: 205 km (127 mi). Apogee: 698 km (433 mi). Inclination: 76.00 deg. Period: 93.60 min. COSPAR: 1962-A-Gamma-1. USAF Sat Cat: 316. Decay Date: 1962-09-14. KH-4; film capsule recovered 4.1 days later. Severe corona static. References: 2, 6. 1962 June 29 - 05:40 GMT - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 416. Research and development test Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). First Air Force crew launch References: 2. 1962 June 29 - 14:06 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-29 (A2MG-4). Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2. 1962 June 29 - 18:41 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 2-24-44. X-15A Heating rates, notch test Nation: USA. Agency: NASA/USAF. Apogee: 25 km (15 mi). Maximum Speed - 5278 kph. Maximum Altitude - 25360 m. References: 2. 1962 June 29 - 21:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.72UP. JHU Airglow 1 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 210 km (130 mi). References: 2. 1962 June 30 - Launch Vehicle: Titan. Model: Titan 2. Martin-Baltimore's airborne systems functional test stand went into operation at Baltimore. Nation: USA. In this 3000-square-foot facility, all airborne systems in the Gemini launch vehicle - including flight control, hydraulic, electrical, instrumentation, and malfunction detection - were assembled on tables and benches; actual engines, but simulated propellant tanks and guidance, were used. In addition to individual and combined systems tests, the facility was used to check system design changes and trouble-shoot problems encountered in other test programs. 1962 June - Launch Vehicle: Saturn V. Study of repair of J-2 engine in space Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. Five NASA scientists, dressed in pressure suits, completed an exploratory study at Rocketdyne Division of the feasibility of repairing, replacing, maintaining, and adjusting components of the J-2 rocket while in space. The scientific team also investigated the design of special maintenance tools and the effectiveness of different pressure suits in performing maintenance work in space. References: 16. 1962 June 30 - 04:55 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.71UA/UP. JHU Airglow 2 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 208 km (129 mi). References: 2. 1962 June 30 - 16:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1. Cosmos 6 Nation: USSR. Program: DS. Payload: DS-P1 s/n 1. Mass: 355 kg (782 lb). Class: Military. Type: Target. Spacecraft: DS-P1. Agency: RVSN. Perigee: 261 km (162 mi). Apogee: 348 km (216 mi). Inclination: 48.90 deg. Period: 90.60 min. COSPAR: 1962-A-Delta-1. USAF Sat Cat: 338. Completed Operations Date: 1962-07-06. Decay Date: 1962-09-08. Prototype ABM radar target; supported developmental experiments for ABM systems. References: 2, 6, 99. Previous Home Next Contact us with any corrections, additions, or comments. 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