1961 January 1 - -
Council of Chief Designers recognised. Nation: USSR. Decree 'On formalising powers of the Council of Chief Designers' was issued. References: 474.
1961 January 1 - -
Mercury 13 Astronaut Training Group selected. Nation: USA. Qualifications: Qualified jet pilot with minimum 1,500 flight-hours/10 years experience, bachelor's degree or equivalent, under 40 years old, under 180 cm height, excellent physical condition.. Randolph Lovelace was director of the clinic where the Mercury astronauts had undergone their physical examinations. He and Jacqueline Cochran, the first American woman to break the sound barrier, wanted to prove that women were equally qualified to be astronauts. In early 1961 they arranged for 20 highly qualified female pilots to take the same physical tests undergone by the Mercury astronauts. Thirteen passed the tests, but NASA maintained its position that astronauts had to be qualified test pilots (all of whom were white males). One of the thirteen was the wife of a US Senator, and some congressional hearings were arranged. Despite the publicity NASA was still unwilling to place them in the official NASA training program.
Oddly enough, the selection of these women may have resulted in the first woman going into space after all. In May 1962 a Soviet delegation, including cosmonaut Gherman Titov and cosmonaut commander Nikolai Kamanin, visited Washington. Kamanin had been pushing for the flight of a Soviet woman into space since October 1961, and five Soviet female cosmonauts had just reported for training a month earlier. However the flight of a woman in space had little support from Chief Designer Korolev or Kamanin's military commanders. On May 3 Kamanin and Titov were invited to a barbecue at the home of astronaut John Glenn. Glenn, already politically-connected, was an enthusiastic supporter of the 'Lovelace 13'. Kamanin understood from Glenn that the first American woman would make a three-orbit Mercury flight by the end of 1962. Armed with the threat that 'the Americans will beat us', Kamanin was able to obtain a decision to go ahead with the first flight of a Soviet woman within weeks of his return. The Russians were obsessed with being first in space -- and even though NASA's female cosmonauts never materialised, Valentina Tereshkova of the Soviet Union became the first woman in space on June 16, 1963.
1961 January 1 - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Kisha Judi. -
Test mission Nation: USA. Agency: Sandia. Apogee: 100 km (60 mi). References: 2.
1961 - Launch Vehicle: SLS. -
Air Force completed studies on a family of advanced heavy-lift launch vehicles for use in the late 1960's Nation: USA. The launchers used solid rocket boosters together with Lox/LH2 upper stages. The modular stages could be combined in various ways to achieve a range of launch vehicles (as for the USAF Lunex lunar base project). These studies would provide the basis for the later Titan derivatives and, eventually, the final space shuttle design.
1961 - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Jaguar B-57. -
Test / aeronomy mission Nation: USA. Agency: USAF AFSWC. Apogee: 800 km (490 mi). References: 2.
1961 During the Year - -
Competing designs for a reliable manned spacecraft to succeed Vostok. Nation: USSR. Spacecraft: Vostok-Zh, Soyuz A, Soyuz B, Soyuz V, Sever. The Soyuz or Sever designs would utilize body lift to reduce G forces and allo the crew to make re-entries at hyperbolic speeds - when returning from the moon, or Mars. An associated design was a manned orbital tug version of the Vostok capsule to assemble spacecraft in low earth orbit.
1961 During the Year - -
Zenit-2 drawing release completed Nation: USSR. Technical documentation completed for the serial production of the Zenit-2 photo reconnaissance satellite. OKB-1 filial number 3, based in Samara (then Kuibishev), headed by Chief Designer Dmitri Ilyich Kozlov, was also responsible for future development and production support of derivatives of the R-7 family of launch vehicles.
1961 During the Year - -
US Navy lunar landing program Nation: USA. Spacecraft: Navy SLV. A US Navy lunar landing program was headed by the inimitable Dr. Nicolaides at China Lake. The team's Soft-Landing Vehicle (SLV) began control testing in a large rig in 1961. The SLV would have sent a dog to the moon in 1963, and returned a soil sample in 1964. A scaled-up version of the lander was to have put a Navy man on the lunar surface by 1967. Further Navy lunar efforts, like those of the Army and Air Force, were discontinued after NASA was given the Apollo moon landing project in April 1961.
1961 During the Year - Launch Vehicle: R-17. -
R-17 (Scud B) first launch Nation: USSR. The program was conducted by the Votkinsk Machine Building Plant. There design work continued with first launch in 1961 and acceptance into military service in 1964. References: 2.
1961 During the Year - Launch Vehicle: Proton. Model: Initial UR-500. -
Initial UR-500 studies for the GR-2 requirement Nation: USSR. The initial design consisted simply of 4 two-stage UR-200 rockets lashed together, the first and second stages working in parallel in clusters. A third stage would be modified from the UR-200 second stage.
1961 January 2 - Launch Vehicle: Navaho. -
Navaho program closed out. Nation: USA. Program: Navaho. One G-26 missile delivered to Cape Canaveral but not launched was retained there for the open-air missile park. X-10 s/n 1 was displayed in the Air Force Museum in Dayton. Harrison Storms attempted to sell the USAF on using the completed work for space launches. One proposal was to use the boosters as the first stage of a satellite launcher with Able upper stages. Another was to cluster four of them together and launch an X-15 manned rocketplane into orbit. Nothing came of these proposals. Four completed G-26 missiles and the under-construction G-38 missiles were scrapped.
1961 January 3 - -
NASA Space Task Group made official. Nation: USA. Program: Mercury. NASA's Space Task Group, charged with carrying out Project Mercury and other manned space flight programs, officially became a separate NASA field element. References: 18.
1961 January 5 - Launch Vehicle: R-16. -
State Commission Meeting Nation: USSR. Program: Vostok, Venera. Spacecraft: Vostok. Rudnev chaired the meeting, which first heard the failure analysis for the failed Mars launches on 10 and 14 October and the R-16 catastrophe on 24 October. All of these had been accelerated to coincide with Khrushchev's visit to the United Nations in New York, in Kamanin's view a criminal rush that led to the death of 74 officers and men in the R-16 explosion. Future plans were then reviewed. Launches of probes toward Venus were planned for 20-23 January, 28-30 January, and 8-10 February. Four Vostok manned spacecraft were completed, with first launch scheduled for 5 February and the second for 15-20 February.
1961 January 5-6 - -
McDonnell one-man space station: Mercury capsule and a cylindrical space laboratory. Nation: USA. Spacecraft: Mercury Mark I. McDonnell Aircraft Corporation officials proposed to NASA a one-man space station consisting of a Mercury capsule and a cylindrical space laboratory capable of supporting one astronaut in a shirt- sleeve environment for 14 days in orbit. The complete vehicle, McDonnell said, could be placed in a 240-km orbit by an Atlas-Agena booster, thus affording NASA what the company termed a 'minimum cost manned space station.'
1961 January 6 - -
Low Committee established Nation: USA. Program: Apollo. Spacecraft: Apollo CSM, Apollo Lunar Landing. The Manned Lunar Landing Task Group (Low Committee) set up by the Space Exploration Program Council was instructed to prepare a position paper for the NASA Fiscal Year 1962 budget presentation to Congress. The paper was to be a concise statement of NASA's lunar program for Fiscal Year 1962 and was to present the lunar mission in term of both direct ascent and rendezvous. The rendezvous program would be designed to develop a manned spacecraft capability in near space, regardless of whether such a technique would be needed for manned lunar landing. In addition to answering such questions as the reason for not eliminating one of the two mission approaches, the Group was to estimate the cost of the lunar mission and the date of its accomplishment, though not in specific terms. Although the decision to land a man on the moon had not been approved, it was to be stressed that the development of the scientific and technical capability for a manned lunar landing was a prime NASA goal, though not the only one. The first meeting of the Group was to be held on January 9.
References: 16.
1961 January 6-12 - -
First meetings of the Apollo Technical Liaison Groups Nation: USA. Program: Apollo. First meetings of the Apollo Technical Liaison Groups, formed to coordinate NASA inter-Center information exchange. References: 16.
1961 January 7 - 17:33 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18B. Launch Pad: LC18B. Launch Vehicle: Scout. Model: Blue Scout 1. LV Configuration: Blue Scout I D-3. -
HETS A1-1 Plasma / radio astronomy mission Nation: USA. Agency: USAF. Apogee: 1,600 km (900 mi). References: 2.
1961 January 10 - 17:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-3. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1961 January 11 - -
Progress made in mapping the moon Nation: USA. Program: Apollo. John Blake of the Air Force Aeronautical Chart and Information Center (ACIC) described to STG representatives the progress made by ACIC in mapping the moon. Lunar maps to the scale of 1: 5,000,000 and 1: 10,000,000 were later requested and received by STG. In addition, the first two sheets of a projected 144 sheet map coverage of the lunar surface on a 1:1,000,000 scale were forwarded to STG by the Center.
References: 16.
1961 January 11 - 18:40 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1E-15. FAILURE: Failure. -
Operational test Nation: USA. Agency: USN. Apogee: 20 km (12 mi). References: 2.
1961 January 12 - Launch Vehicle: Titan. -
Titan II to be the Dyna-Soar suborbital Step I booster. Nation: USA. Spacecraft: Dynasoar. Air Force headquarters announced that Titan II would be the suborbital Step I booster.
1961 January 12 - 16:54 GMT - Launch Site: Salto di Quirra. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun ISRC-RS-01. -
Aeronomy sodium release mission Nation: Italy. Agency: CRA/NASA. Apogee: 160 km (90 mi). References: 2.
1961 January 13 - Launch Vehicle: Titan. Model: Titan 2. -
USAF changes Dynasoar launch vehicle to Titan II Nation: USA. Class: Manned. Type: Spaceplane. Spacecraft: Dynasoar. References: 26.
1961 January 13 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5. LV Configuration: R-5 V-1000 target. -
Target mission Nation: USSR. Agency: OKB-30. Apogee: 300 km (180 mi). References: 2.
1961 January 14 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1E-14. FAILURE: Failure. -
Operational test Nation: USA. Agency: USN. Apogee: 20 km (12 mi). References: 2.
1961 January 14 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5. LV Configuration: R-5 V-1000 target. -
Target mission Nation: USSR. Agency: OKB-30. Apogee: 300 km (180 mi). References: 2.
1961 January 14 - 01:19 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7A. -
R-7A II-1 operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,350 km (830 mi). Some sources say first launch from LC31 was not until 27 February. References: 2.
1961 January 17 - 21:25 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.36GT. -
Test mission Nation: USA. Agency: NASA. Apogee: 209 km (129 mi). References: 2.
1961 January 18 - 04:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trailblazer. Model: Trailblazer 1. LV Configuration: Trailblazer 1 TB If. -
D58 Trailblazer re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 260 km (160 mi). References: 2.
1961 January 19 - -
Studies of manned lunar and interplanetary expeditions Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. The Marshall Space Flight Center awarded contracts to the Douglas Aircraft Company and Chance Vought Corporation to study the launching of manned exploratory expeditions into lunar and interplanetary space from earth orbits. References: 16.
1961 January 19 - -
Hughes to build Surveyor spacecraft Nation: USA. Spacecraft: Surveyor. After evaluating preliminary design studies, NASA selected the Hughes Aircraft Company to build seven Surveyor spacecraft. This 750-pound, three-legged, unmanned spacecraft would carry 200 pounds of instruments, including zoom television cameras, a drill to sample the lunar soil, chemical analysis equipment, and a seismometer. The first Surveyor was scheduled to be launched in 1963.
References: 16.
1961 January 19 - 12:42 GMT - Launch Site: Wallops Island. Launch Complex: LA1. Launch Pad: -. Launch Vehicle: Iris. LV Configuration: Iris NASA 5.03GT. FAILURE: Failure. -
Aeronomy / test Nation: USA. Agency: NASA. Apogee: 138 km (85 mi). References: 2.
1961 January 20 - -
Space Task Group management discusses a follow-on Mercury program. Nation: USA. Program: Gemini. Spacecraft: Gemini. Space Task Group management held a Capsule Review Board meeting. The first topic on the agenda was a follow-on Mercury program. Several types of missions were considered, including long-duration, rendezvous, artificial gravity, and flight tests of advanced equipment. Major conclusion was that a follow-on program needed to be specified in greater detail.
1961 January 20 - 20:53 GMT - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I AJ-10. FAILURE: Failure. -
Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 0 km ( mi). References: 2.
1961 January 22 - 02:04 GMT - Launch Site: Cape Canaveral. Launch Complex: LC6. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2038. FAILURE: Control system malfunction during re-entry at 370 sec. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Missile test failure. Missed aimpoint by 788 m. References: 2.
1961 January 23 - 21:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC12. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 90D. -
Research and development test Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi). Final test flight of USAF Atlas D traveled 5,000 miles to target down Atlantic Missile Range, representing 35 successes, 8 partials, and 6 failures in 49 test launchings for D model. 75th Atlas launched at AMR, successful References: 2.
1961 January 24 - 21:55 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 8E. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). References: 2.
1961 January 25 - -
Study on the feasibility of refueling a spacecraft in orbit Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. NASA announced that the Lockheed Aircraft Corporation had been awarded a contract by the Marshall Space Flight Center to study the feasibility of refueling a spacecraft in orbit. References: 16.
1961 January 26 - Launch Vehicle: Saturn I. -
Saturn C-1 changed to a two-stage configuration Nation: USA. Program: Apollo. Wernher von Braun, Director of Marshall Space Flight Center, proposed that the Saturn C-1 launch vehicle be changed from a three-stage to a two-stage configuration to meet Apollo program schedules. The planned third stage (S-V) would be dropped. References: 16.
1961 January 30 - Launch Vehicle: Europa. -
Europa conference. Nation: Europe. Conference of 12 European nations held at Strasbourg to discuss a British and French proposal for a European satellite launcher development program. References: 18.
1961 January 30 - -
James E Webb named as NASA Administrator Nation: USA. Program: Apollo. President John F. Kennedy announced that he was nominating James E. Webb as Administrator of the National Aeronautics and Space Administration and Hugh L. Dryden as Deputy Administrator, Senate confirmation followed on February 9 and they were sworn in on February 14.
References: 16.
1961 January 30 - 23:20 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.370. -
Mass spectrometer Aeronomy mission Nation: USA. Agency: USAF. Apogee: 204 km (126 mi). References: 2.
1961 January - Launch Vehicle: Saturn I. -
Saturn first stage recovery system study Nation: USA. Program: Apollo. Marshall Space Flight Center awarded contracts to NAA and Ryan Aeronautical Corporation to investigate the feasibility of recovering the first stage (S-I) of the Saturn launch vehicle by using a Rogallo wing paraglider. References: 16.
1961 January 31 - 16:54 GMT - Launch Site: Cape Canaveral. Launch Complex: LC5. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone MRLV. LV Configuration: Redstone MRLV-2. -
Mercury MR-2 Nation: USA. Agency: NASA. Apogee: 251 km (155 mi). Ham, a 37-pound chimpanzee, was aboard the spacecraft. The over-acceleration of the launch vehicle coupled with the velocity of the escape rocket caused the spacecraft to attain a higher altitude and a longer range than planned. In addition, the early depletion of the liquid oxygen caused a signal that separated the spacecraft from the launch vehicle a few seconds early. However spacecraft recovery was effected, although there were some leaks and the spacecraft was taking on water. Ham appeared to be in good physiological condition, but sometime later when he was shown the spacecraft it was visually apparent that he had no further interest in cooperating with the space flight program. Despite the over-acceleration factor, the flight was considered to be successful.
References: 2.
1961 January 31 - 20:21 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena A. LV Configuration: Atlas Agena A 70D / Agena A 2102. -
Samos 2 Nation: USA. Payload: Samos E-1 no. 2. Mass: 1,900 kg (4,100 lb). Class: Surveillance. Type: Military. Spacecraft: Samos. Agency: U.S. Air Force. Perigee: 474 km (294 mi). Apogee: 557 km (346 mi). Inclination: 97.40 deg. Period: 95.00 min. COSPAR: 1961-Alpha-1. USAF Sat Cat: 70. Decay Date: 1973-10-21. First generation photo surveillance; radio relay of images; micrometeoroid impact data. Poor results. References: 2, 6, 278.
1961 February - -
Astronaut personal parachute in the Mercury program. Nation: USA. Program: Mercury. Spacecraft: Mercury. Flight: Mercury MR-3. Instruction was provided to the astronauts to develop techniques and procedures for using the personal parachute as an additional safety feature in the Mercury program. This parachute was only used during the Mercury-Redstone 3 (MR-3) mission manned by Alan Shepard.
References: 483.
1961 February 1 - 15:59 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31A. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 401. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). References: 2.
1961 February 1 - 18:47 GMT - Launch Site: Palmdale Omni DZ. Launch Complex: -. Launch Pad: 34.7 N x 118.0 W. Launch Vehicle: X-15. LV Configuration: X-15 1-20-35. -
X-15A Ball/side controller test Nation: USA. Agency: NASA/USAF. Apogee: 15 km (9 mi). Maximum Speed - 1949 kph. Maximum Altitude - 15170 m. References: 2.
1961 February 2 - Launch Vehicle: Saturn C-3, Saturn I, Saturn V. -
NERVA Request for Proposal. Nation: USA. Program: NERVA. NASA-AEC Space Nuclear Propulsion Office invited industry to submit proposals for participation in development of Nerva (nuclear engine for rocket vehicle application), a part of Project Rover initiated in 1955 by USAF-AEC. References: 18.
1961 February 2 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-11. Model: R-11A. -
Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 200 km (120 mi). References: 2.
1961 February 2 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-11. Model: R-11A. -
Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 200 km (120 mi). References: 2.
1961 February 2 - 19:00 GMT - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: LC41/pad?. Launch Vehicle: R-16. LV Configuration: R-16 3L-5T. FAILURE: Failure. -
First successful R-16 launch. Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi). The missile was supposed to be launched at 18:00, but is then delayed to 24:00 due to technical problems. It is a clear night, illuminated by the moon, and the missile takes off at midnight. The first three minutes of flight are successful, but then the second stage fails to ignite. The missiles impacts 520 km downrange from the launch pad.
References: 2.
1961 February 4 - 01:18 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 L1-7. 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 7 Nation: USSR. Program: Venera. Payload: 2MV-2 s/n 1. Mass: 6,483 kg (14,292 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 1VA. Agency: RVSN. Perigee: 212 km (131 mi). Apogee: 318 km (197 mi). Inclination: 64.90 deg. Period: 89.80 min. COSPAR: 1961-Beta-1. USAF Sat Cat: 71. Decay Date: 1961-02-26. 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.. The payload attached together with escape stage remained in Earth orbit.The booster launched into a beautiful clear sky, and it could be followed by the naked eye for four minutes after launch. The third stage reached earth parking orbit, but the fourth stage didn't ignite. It was at first believed a radio antenna did not deploy from the interior of the stage, and it did not receive the ignition commands. Therefore the Soviet Union has successfully orbited a record eight-tonne 'Big Zero' into orbit. The State Commission meets two hours after the launch, and argues whether to make the launch public or not, and how to announce it. Glushko proposes the following language for a public announcement: 'with the objective of developing larger spacecraft, a payload was successfully orbited which provided on the first revolution the necessary telemetry'. Korolev and the others want to minimize any statement, to prevent speculation that it was a reconnaissance satellite or a failed manned launch. Kamanin's conclusion - the rocket didn't reach Venus, but it did demonstrated a new rocket that could deliver an 8 tonne thermonuclear warhead anywhere on the planet. The commission heads back to Moscow.
References: 2, 6, 64, 65, 376.
1961 February 5 - 13:48 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.38NP. -
LeRC LH2 test Technology test Nation: USA. Agency: NASA. Apogee: 152 km (94 mi). References: 2.
1961 February 6 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Centaur LV-3C. -
Liquid hydrogen tests. Nation: USA. NASA Aerobee-Hi successfully reached 96 miles above Wallops Station in test of behavior of liquid hydrogen in zero gravity for Lewis Research Center hydrogen propulsion development. References: 18.
1961 February 6 - 21:40 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-6. FAILURE: Failure. -
Test mission Nation: USA. Agency: USN. Apogee: 0 km ( mi). References: 2.
1961 February 7 - Launch Vehicle: Atlas. Model: Atlas Centaur LV-3C. -
Centaur development milestones set. Nation: USA. Meeting of NASA and contractor personnel held at NASA headquarters to review Centaur development program. References: 18, 278.
1961 February 7 - Launch Vehicle: Nova, Saturn C-2. -
Final report of the Low Committee Nation: USA. Program: Apollo. Spacecraft: Apollo Lunar Landing. The Manned Lunar Landing Task Group (Low Committee) transmitted its final report to NASA Associate Administrator Robert C. Seamans, Jr. The Group found that the manned lunar landing mission could be accomplished during the decade, using either the earth orbit rendezvous or direct ascent technique. Multiple launchings of Saturn C-2 launch vehicles would be necessary in the earth orbital mode, while the direct ascent technique would require the development of a Nova-class vehicle. Information to be obtained through supporting unmanned lunar exploration programs, such as Ranger and Surveyor, was felt to be essential in carrying out the manned lunar mission. Total funding for the program was estimated at just under $7 billion through Fiscal Year 1968.
References: 16.
1961 February 7 - 12:46 GMT - Launch Site: Woomera. Launch Complex: LA5A. Launch Pad: -. Launch Vehicle: Black Knight. Model: Black Knight 201. LV Configuration: Black Knight-201 BK.13. -
Gaslight Re-entry Vehicle test Nation: UK. Agency: RAE. Apogee: 687 km (426 mi). References: 2.
1961 February 7 - 20:56 GMT - Launch Site: Silver Lake DZ. Launch Complex: -. Launch Pad: 35.3 N x 116.1 W. Launch Vehicle: X-15. LV Configuration: X-15 1-21-36. -
X-15A Stab./Control test Nation: USA. Agency: NASA/USAF. Apogee: 23 km (14 mi). Maximum Speed - 3660 kph. Maximum Altitude - 23820 m. Last XLR-11 flight. References: 2.
1961 February 10 - -
Voice message sent by way of the moon Nation: USA. Program: Apollo. A voice message was sent from Washington, D.C., to Woomera, Australia, by way of the moon. NASA Deputy Administrator Hugh L. Dryden spoke by telephone to Goldstone, Calif., which "bounced" it to the deep-space instrumentation station at Woomera. The operation was conducted as part of the official opening ceremony of the Australian facility.
References: 16.
1961 February 10 - Launch Vehicle: Saturn V. -
First static test of prototype F-1 thrust chamber Nation: USA. Program: Apollo. Rocketdyne Division's first static test of a prototype thrust chamber for the F-1 engine achieved a thrust of 1.550 million pounds in a few seconds at Edwards Air Force Base, Calif. References: 16.
1961 February 10 - -
Air Force interest in spacecraft similar to the Apollo Nation: USA. Program: Lunex. At the first meeting of the House Committee on Science and Astronautics, during the first session of the 87th Congress, Charles F. Ducander, Executive Director and Chief Counsel of the Committee staff, outlined a number of proposed subjects for study. One subject was the Air Force's interest in a three-man spacecraft similar to the Apollo spacecraft planned by NASA. A Committee staff member had been assigned to investigate this duplication of effort. On February 22, testifying before the Committee, Air Force Undersecretary Joseph V. Charyk stated that the Dyna-Soar program was a direct approach to manned military space applications. The Air Force interest in an Apollo-type spacecraft was part of the post-Dyna-Soar program, Charyk said.
References: 16.
1961 February 10 - 05:55 GMT - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I AJ-11. -
Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
11-12 February 1961 - Launch Site: Cuxhaven. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kumulus. -
Kumulus rocket reaches 19.75 km Nation: Germany. The DRG (German Rocket Society) launched four MVR-I rockets on Saturday and two on Sunday. The Saturday launches were tracked to an altitude of 15 km and impacted 15 to 30 km from the launch point in the North Sea. The rockets were 18 cm in diameter, 2 m long, and had a mass of 24 kg. One of the Sunday launches reached 19,750 m altitude with a meteorological payload built by the Max Planck Institute. The rocket had a thrust of 508 kgf and weighted 19.9 kg. German television covered the launches.
1961 February 11 - 10:41 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI27. -
Airglow Aeronomy mission Nation: France. Agency: FR. Apogee: 91 km (56 mi). References: 2.
1961 February 12 - 00:34 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 L1-6B. -
Venera 1 Nation: USSR. Program: Venera. Payload: 1VA s/n 2, Venera 1 (Sputnik 8, AMS). Mass: 644 kg (1,419 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 1VA. Agency: RVSN. COSPAR: 1961-Gamma-1. USAF Sat Cat: 80. Venera 1 was the first spacecraft to fly by Venus. The 6424 kg assembly was launched first into a 229 x 282 km parking orbit, then boosted toward Venus by the restartable Molniya upper stage. On 19 February, 7 days after launch, at a distance of about two million km from Earth, contact with the spacecraft was lost. On May 19 and 20, 1961, Venera 1 passed within 100,000 km of Venus and entered a heliocentric orbit. This failure resulted in only the following objectives being met: checking of methods of setting space objects on an interplanetary course; checking of extra-long-range communications with and control of the space station; more accurate calculation of the dimension of the solar system; a number of physical investigations in space.
Additional Details: Venera 1. References: 2, 6, 64, 296, 376.
1961 February 13 - Launch Vehicle: Titan. Model: Titan 2. -
Beginning of Gemini Nation: USA. Program: Gemini. Class: Manned. Type: Spacecraft. Spacecraft: Gemini. First formal NASA/McDonnell discussions on Mercury Mark II (Gemini). References: 26.
1961 February 13 - -
NASA and McDonnell began discussions of an advanced Mercury spacecraft. Nation: USA. Program: Gemini. Spacecraft: Gemini. McDonnell had been studying the concept of a maneuverable Mercury spacecraft since 1959. On February 1, Space Task Group (STG) Director Robert R. Gilruth assigned James A. Chamberlin, Chief, STG Engineering Division, who had been working with McDonnell on Mercury for more than a year, to institute studies with McDonnell on improving Mercury for future manned space flight programs.
Additional Details: NASA and McDonnell began discussions of an advanced Mercury spacecraft..
1961 February 13 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI28. FAILURE: Failure. -
Aeronomy mission Nation: France. Agency: FR. Apogee: 0 km ( mi). References: 2.
1961 February 13 - 04:39 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7A. LV Configuration: R-7A L1-3T. -
R-7A II-2 operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,350 km (830 mi). Some sources say first launch from LC31 was not until 27 February. References: 2.
1961 February 13 - 13:58 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark-2 SL36. -
Grenades / Chaff Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 146 km (90 mi). References: 2.
1961 February 14 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Strongarm. Model: Strongarm. LV Configuration: Strongarm E22-H1-1. FAILURE: Failure. -
Geodetic Flares test Nation: USA. Agency: USA BRL. Apogee: 100 km (60 mi). References: 2.
1961 February 14 - 23:50 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.07GA. -
Grenade Aeronomy mission Nation: USA. Agency: NASA. Apogee: 130 km (80 mi). NASA Nike-Cajun rocket launched from Wallops Station, carrying 60-pound payload ejecting explosive charges, which fired at intervals from 20- to 80-mile altitude to provide data on density of the atmosphere. References: 2.
1961 February 15 - -
Acoustic tests. Nation: USA. Acoustic test chamber for recording sound of rocket operations and to study human stress limits completed at Environmental Simulation Laboratory, Naval Missile Center, at Pacific Missile Range. References: 18.
1961 February 15 - -
James E. Webb sworn in as Administrator of NASA. Nation: USA. After his nomination by the President as Administrator of NASA on January 30, 1961, James E. Webb was sworn into office, replacing T. Keith Glennan. References: 483.
1961 February 15 - 22:01 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI29. -
Aeronomy mission Nation: France. Agency: FR. Apogee: 150 km (90 mi). References: 2.
1961 February 16 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. -
First satellite launch from Wallops Island. Nation: USA. NASA Explorer IX placed in orbit by four-stage Scout booster from Wallops Station, the first satellite launching from Wallops, and the first satellite boosted by a solid-fuel rocket. Explorer IX was a 12-foot diameter sphere after inflation at orbital altitude.
References: 18.
1961 February 16 - -
Soviet decree 'On measures to improve military technology' . Nation: USSR. This decree laid the basis for institution of quality control by the military to improve the reliability of space systems.
1961 February 16 - 13:05 GMT - Launch Site: Wallops Island. Launch Complex: LA3. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-1. LV Configuration: Scout X-1 ST-4. -
Explorer 9 Nation: USA. Program: Explorer. Payload: S-56A. Mass: 7.00 kg (15.40 lb). Class: Earth. Type: Atmosphere. Spacecraft: S-56. Agency: U.S. Air Force. Perigee: 757 km (470 mi). Apogee: 2,433 km (1,511 mi). Inclination: 38.80 deg. Period: 118.00 min. COSPAR: 1961-Delta-1. USAF Sat Cat: 81. Decay Date: 1964-04-09. 12 foot dia. balloon; atmospheric density studies. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1961 February 17-20 - Launch Vehicle: Atlas. Model: Atlas D. -
Rules for the Mercury MA-2 Nation: USA. Program: Mercury. Spacecraft: Mercury. Spacecraft, mission, and launch vehicle flight safety rules for the Mercury-Atlas 2 (MA-2) mission were reviewed by Space Task Group personnel. References: 483.
1961 February 17 - 07:17 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache AA5.391. -
Test mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1961 February 17 - 19:04 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.129. -
Extreme ultraviolet Monochromator Solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 275 km (170 mi). References: 2.
1961 February 17 - 20:25 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 298. -
Discoverer 20 Nation: USA. Payload: KH-5 s/n 9014A / Agena B 1104. Mass: 1,110 kg (2,440 lb). Class: Surveillance. Type: Military. Spacecraft: KH-5. Agency: U.S. Navy. Perigee: 277 km (172 mi). Apogee: 491 km (305 mi). Inclination: 80.80 deg. Period: 92.30 min. COSPAR: 1961-Epsilon-1. USAF Sat Cat: 83. Decay Date: 1962-07-28. KH-5; film capsule not ejected. Mission failed. Program malfunctioned and capsule did not reenter. First attempted ARGON mission. Officially: Spacecraft Engaged in investigation of spaceflight techniques and technology (US Cat A). References: 2, 6.
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SRV 520 Nation: USA. Spacecraft: KH-5. Agency: USAF. COSPAR: 1961-Epsilon-4. USAF Sat Cat: 90. Decay Date: 1961-10-31. References: 2, 279.
1961 February 18 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5. LV Configuration: R-5 V-1000 target. -
Target mission Nation: USSR. Agency: OKB-30. Apogee: 300 km (180 mi). References: 2.
1961 February 18 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI30. FAILURE: Failure. -
Aeronomy mission Nation: France. Agency: FR. Apogee: 0 km ( mi). References: 2.
1961 February 18 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Strongarm. Model: Strongarm. LV Configuration: Strongarm E22-H1-2. -
Geodetic Flares test Nation: USA. Agency: USA BRL. Apogee: 2,027 km (1,259 mi). References: 2.
1961 February 18 - 22:58 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 261 / Agena B 1102. -
Discoverer 21 Nation: USA. Payload: Midas test payload. Mass: 1,110 kg (2,440 lb). Class: Early Warning. Spacecraft: Midas. Agency: U.S. Navy. Perigee: 212 km (131 mi). Apogee: 458 km (284 mi). Inclination: 80.60 deg. Period: 91.30 min. COSPAR: 1961-Zeta-1. USAF Sat Cat: 84. Decay Date: 1962-04-20. Tested IR sensors for Midas program; did not carry camera or film capsule. References: 2, 6.
1961 February 20 - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I AJ-13. -
Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
1961 February 21 - -
First Mercury crews selected. Nation: USA. Program: Mercury. NASA Space Task Group selected John H. Glenn, Jr., Virgil I. Grissom, and Alan B. Shepard, Jr., to begin special training for first manned Mercury space flight. References: 18.
1961 February 21 - 14:12 GMT - Launch Site: Cape Canaveral. Launch Complex: LC14. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 67D. -
Mercury MA-2 Nation: USA. Agency: USAF. Apogee: 182 km (113 mi). Mercury-Atlas 2 (MA-2) was launched from Cape Canaveral in a test to check maximum heating and its effects during the worst reentry design conditions. The flight closely matched the desired trajectory and attained a maximum altitude of 114.04 statute miles and a range of 1,431.6 statute miles. Inspection of the spacecraft aboard the recovery ship some 55 minutes after launch (actual flight time was 17.56 minutes) indicated that test objectives were met, since the structure and heat protection elements appeared to be in excellent condition. The flight control team obtained satisfactory data; and the complete launch computing and display system, operating for the first time in a flight, performed satisfactorily.
References: 2.
1961 February 22 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5. LV Configuration: R-5 V-1000 target. -
Target mission Nation: USSR. Agency: OKB-30. Apogee: 300 km (180 mi). References: 2.
1961 February 22 - 03:45 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar 313 AB007. -
Transit 3B Nation: USA. Program: Transit. Mass: 112 kg (246 lb). Class: Navigation. Spacecraft: Transit. Agency: U.S. Navy. COSPAR: 1961-Eta-1. USAF Sat Cat: 87. Decay Date: 1961-02-22. Lofti 1 piggyback payload did not separate. Nevertheless Transit 3B returned useful data needed for design of the operational satellites. It carried a digital clock driven by the same oscillator that drove the transmitters. It transmitted timing signals governed by the clock and a 384-bit memory. This allowed testing of the techniques for loading the memory from the ground, the ability of the memory to hold a message in orbit, and the ability to encode the memory contents by means of a frequency modulation on one of the main transmitters. It was also shown that ±60° phase modulation could be used to transmit the contents of the satellite memory without degradation of the accuracy of the Doppler signal and Doppler measurements.
References: 2, 6.
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Lofti 1 Nation: USA. Program: Transit. Mass: 25 kg (55 lb). Class: Navigation. Spacecraft: Transit. Agency: U.S. Navy. Perigee: 188 km (116 mi). Apogee: 983 km (610 mi). Inclination: 28.30 deg. Period: 96.40 min. COSPAR: 1961-Eta-2. USAF Sat Cat: 87. Decay Date: 1961-03-30. Failed to separate from Transit 3B. References: 2, 6.
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Lofti Nation: USA. Spacecraft: Lofti. Agency: USAF. COSPAR: 1961-Eta-xx. References: 2, 279.
1961 February 22 - 07:00 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. LV Configuration: Veronique AGI24. -
Life Science mission Nation: France. Agency: FR. Apogee: 110 km (60 mi). French Veronique launched capsule containing rat (Hector) to 152 km altitude, recovered successfully. References: 2.
1961 February 24 - Launch Vehicle: Atlas. Model: Atlas D. -
Mercury spacecraft No. 9 was delivered to Cape Canaveral Nation: USA. Program: Mercury. Spacecraft: Mercury. Spacecraft No. 9 was delivered to Cape Canaveral for the Mercury-Atlas 5 (MA-5) orbital primate (Enos) mission. References: 483.
1961 February 24 - 00:19 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AA6.170. -
Sphere Aeronomy mission Nation: USA. Agency: USAF. Apogee: 133 km (82 mi). References: 2.
1961 February 24 - 18:29 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 9E. -
Research and development test Nation: USA. Agency: USAF. Apogee: 1,500 km (900 mi). First successful Atlas E flight. References: 2.
1961 February 25 - -
Successful drop test using Mercury boilerplate. Nation: USA. Program: Mercury. Spacecraft: Mercury. McDonnell conducted a successful drop test, using a boilerplate spacecraft fitted with impact skirt, straps and cables, and a beryllium heat shield. During the tests the stainless steel straps were successfully stretched to design limits. References: 483.
1961 February 25 - 00:13 GMT - Launch Site: Cape Canaveral. Launch Complex: LC26B. Launch Pad: -. Launch Vehicle: Jupiter. Model: Juno II. LV Configuration: Juno II AM-19F. FAILURE: Third Stage failed to ignite. -
Explorer Nation: USA. Program: Explorer. Payload: S-45. Mass: 34 kg (74 lb). Class: Solar. Spacecraft: P-14. Agency: NASA. COSPAR: F610224A. Decay Date: 1961-02-24. References: 2, 126.
1961 February 27 - 00:52 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7. LV Configuration: R-7 L2-1. -
Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,350 km (830 mi). References: 2.
1961 March 1 - Launch Vehicle: Saturn C-2, Saturn I. -
Current Saturn launch vehicle configurations announced Nation: USA. Program: Apollo. The current Saturn launch vehicle configurations were announced: - C-1:
- S-I stage eight H-1 engines, 1.5 million pounds of thrust; S-IV stage four (LR-119 engines, 70,000 pounds of thrust); and S-V stage (two LR-119 engines, 35,000 pounds of thrust).
- C-2 (four-stage version):
- S-1 stage (same as first stage of the C-1); S-II (not determined); S-IV (same as second stage of the C-1); S-V (same as third Stage of C- 1).
- C-2 (three-stage version):
- S-I (same as first stage of C-1); S-II (not determined); and S-IV (same as third stage of C-1).
References: 16.
1961 March - -
Early Spring first presented to Congress. Nation: USA. Spacecraft: Early Spring. Early Spring was a conventional ASAT launched by Polaris missiles from US Navy ballistic missile submarines. As an enemy satellite passed overhead, a Polaris missile would be launched. The ASAT used a restartable upper stage to 'hover' in front of the oncoming satellite. An optical homing system would first locate, track the target satellite, and then ASAT would put itself on a collision course with the target. A proximity fuse would detonate a warhead with thousands of steel pellets.
1961 March - Launch Vehicle: RS. -
RS project cancelled Nation: USSR. Tsybin's design bureau had been taken over by Chelomei, and work on the RS was stopped in the spring of 1961, with three airframes nearly finished. Tsybin went to work for Korolev at OKB-1.
1961 March 1 - 15:42 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp AA8.820. -
VLF Propagation Solar extreme ultraviolet mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi). References: 2.
1961 March 1 - 18:19 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-7. -
Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). The fourth firing of an advanced Polaris A-2, and the first from a ship, was made by the U.S.S. Observation Island as she cruised at 8 knots, 10 miles offshore from Cape Canaveral. References: 2.
1961 March 2 - Launch Site: Makat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: R-12. -
V-1000 target mission Nation: USSR. Agency: OKB-30. Apogee: 402 km (249 mi). References: 2.
1961 March 3 - Launch Vehicle: Atlas. Model: Atlas D. -
Mercury Atlas launch vehicle No. 100-D rolled out. Nation: USA. Program: Mercury. Factory roll-out inspection of Atlas launch vehicle No. 100-D was conducted at Convair-Astronautics. This launch vehicle was allocated for the Mercury-Atlas 3 (MA-3) mission. References: 483.
1961 March 3 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Antares. LV Configuration: Antares 010. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 150 km (90 mi). References: 2.
1961 March 3 - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I AJ-12. FAILURE: Failure. -
Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 0 km ( mi). References: 2.
1961 March 3 - 13:59 GMT - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: LC41/pad?. Launch Vehicle: R-16. LV Configuration: R-16 4L-6T. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi). References: 2.
1961 March 3 - 16:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC18B. Launch Pad: LC18B. Launch Vehicle: Scout. Model: Blue Scout 2. LV Configuration: Blue Scout II D-4. -
HETS A2-1 Plasma mission Nation: USA. Agency: USAF. Apogee: 2,540 km (1,570 mi). References: 2.
1961 March 4 - Launch Site: Makat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: R-12. -
V-1000 target mission Nation: USSR. Agency: OKB-30. Apogee: 460 km (280 mi). References: 2.
1961 March 6 - Launch Vehicle: UR-200. -
US RORSAT authorised. Nation: USSR. Spacecraft: US-A. Decree 420·1741 'On approval of work on the US satellite and UR-200 launch vehicle / ICBM' was issued. References: 474.
1961 March 6 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Antares. LV Configuration: Antares 011. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 150 km (90 mi). References: 2.
1961 March 6 - 09:56 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 2C. LV Configuration: Skylark-2C SL63. -
Grenade / Chaff / Sodium release Aeronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 231 km (143 mi). References: 2.
1961 March 7 - Launch Vehicle: Saturn I. -
First flight Saturn I on test stand. Nation: USA. Program: Apollo. First flight model of Saturn booster (SA-1) installed on static test stand for preflight checkout, Marshall Space Flight Center, Huntsville. References: 18, 27.
1961 March 7 - Launch Site: Warren AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. -
Atlas SMS 565 operational. Nation: USA. Warren-2 AFB SMS 565 operational References: 4460.
1961 March 7 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Antares. LV Configuration: Antares 012. -
Re-entry Vehicle test Nation: France. Agency: ONERA. Apogee: 150 km (90 mi). References: 2.
1961 March 7 - 18:28 GMT - Launch Site: Silver Lake DZ. Launch Complex: -. Launch Pad: 35.3 N x 116.1 W. Launch Vehicle: X-15. LV Configuration: X-15 2-13-26. -
X-15A Mach 4 flight test Nation: USA. Agency: NASA/USAF. Apogee: 23 km (14 mi). Maximum Speed - 4674 kph. Maximum Altitude - 23610 m. References: 2.
1961 March 8 - 16:53 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 300. LV Configuration: Aerobee 300 AA10.192. -
Ne / RPA Ionosphere mission Nation: USA. Agency: USAF. Apogee: 400 km (240 mi). References: 2.
1961 March 8 - 17:53 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee 1500. LV Configuration: Astrobee 1500 AE16.305. -
Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 431 km (267 mi). References: 2.
1961 March 9 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-8. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1961 March 9 - 02:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC6. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2040. FAILURE: Control system malfunction during re-entry at 374 sec. -
Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Missile test failure. Missed aimpoint by 358 m. References: 2.
1961 March 9 - 06:29 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K. LV Configuration: Vostok 8K72K E103-14. -
Korabl-Sputnik 4 Nation: USSR. Program: Vostok. Payload: Vostok 3KA s/n 1. Mass: 4,700 kg (10,300 lb). Class: Manned. Type: Spacecraft. Spacecraft: Vostok. Agency: RVSN. Perigee: 173 km (107 mi). Apogee: 239 km (148 mi). Inclination: 64.90 deg. Period: 88.60 min. COSPAR: 1961-Theta-1. USAF Sat Cat: 91. Duration: 0.0700 days. Decay Date: 1961-03-09. Flight: Vostok 1. Carried dog Chernushka, mannequin Ivan Ivanovich, and other biological specimens. Ivanovich was ejected from the capsule and recovered by parachute, and Chernsuhka was successfully recovered with the capsule on March 9, 1961 8:10 GMT. Officially: Development of the design of the space ship satellite and of the systems on board, which ensure necessary conditions for man's flight.
Additional Details: Korabl-Sputnik 4. References: 2, 6, 175, 376.
1961 March 10 - Launch Site: Hammaguira. Launch Complex: -. Launch Pad: -. Launch Vehicle: SE.4400. LV Configuration: SE4400 F92. -
Test mission Nation: France. Agency: STA. Apogee: 67 km (41 mi). References: 2.
1961 March 14 - Launch Vehicle: Atlas. Model: Atlas D. -
Mercury Atlas launch vehicle 100-D delivered to Cape Canaveral Nation: USA. Program: Mercury. Atlas launch vehicle 100-D was delivered to Cape Canaveral for the Mercury-Atlas 3 (MA-3) mission. References: 483.
1961 March 14 - 04:17 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 13E. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 500 km (310 mi). References: 2.
1961 March 14 - 21:52 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AA6.801. -
Antenna Breakdown Experiment Ionosphere mission Nation: USA. Agency: USAF. Apogee: 118 km (73 mi). References: 2.
1961 March 15 - -
Mercury Bermuda tracking station agreement. Nation: USA. Program: Mercury. United States and United Kingdom signed formal agreement covering Mercury tracking stations on Bermuda. References: 18.
1961 March 15 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-10. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi). References: 2.
1961 March 15 - 17:47 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.49GT. -
Cajun fin test Nation: USA. Agency: NASA. Apogee: 130 km (80 mi). References: 2.
1961 March 16 - -
Mercury spacecraft No. 10 was withdrawn from the flight program Nation: USA. Program: Mercury. Spacecraft: Mercury. It was allocated to a ground test simulating orbital flight environmental conditions at the McDonnell plant site. References: 483.
1961 March 16 - Launch Vehicle: UR-200. -
UR-200 (8K81) launch vehicle development authorised. Nation: USSR. Spacecraft: Kosmoplan, IS-A, US-A, US-P, OGCh. An enabling decree was issued on 1 August 1961 by the Central Committee and Politburo. The UR-200 was designed not only to send a thermonuclear warhead over a range of 12,000 km, but also to orbit all of the Kosmoplan military variants: the IS ASAT; the US nuclear-powered naval intelligence satellite; and the Kosmoplan combat re-entry vehicle.
1961 March 16 - -
Project SAINT Phase I contract signed by RCA. Nation: USA. Spacecraft: SAINT, SAINT II. Project SAINT (SAtellite INTerceptor) was a large and still deeply classified US Air Force program begun in the late 1950's covering a wide range of technologies for interception, inspection, and destruction of enemy spacecraft. After studies in the 1950’s. The Phase I development contract was let to Radio Corporation of America. Saint Phase I would have weighted 1,100 kg and been launched by Atlas D/Agena B.
1961 March 17 - Launch Vehicle: Vanguard. -
Vanguard third anniversary. Nation: USA. Program: Vanguard. Class: Technology. Spacecraft: Vanguard 1. Vanguard I completed third year in orbit and was still transmitting. Vanguard I provided much useful data on orbits, including the slight pear-shape of the Earth and the effect of solar pressure. Vanguard also provided the second stage for the Able, Delta, and Able-Star, as well as the third stage of Scout, pioneering solid-propellant stages used in Polaris and Minuteman.
References: 18.
1961 March 18 - 16:49 GMT - Launch Site: Wallops Island. Launch Complex: LA1. Launch Pad: -. Launch Vehicle: Little Joe. Model: Little Joe 1 4C. LV Configuration: Little Joe 1-4C LJ-5A. FAILURE: Escape tower fired prematurely. -
Mercury LJ-5A Nation: USA. Agency: NASA. Apogee: 12 km (7 mi). Mercury Little Joe 5A (LJ-5A), the sixth in the series of Little Joe missions, was launched from Wallops Island. This flight was intended to satisfy test objectives, which were not met previously because of the failure of the spacecraft to separate from the launch vehicle during the Little Joe 5 (LJ-5) mission flown on November 8, 1960. For reference, the purpose of this test was to demonstrate primarily the structural integrity of the spacecraft and the escape system during an escape maneuver initiated at the highest dynamic pressure anticipated during an Atlas launch for orbital flight. Little Joe 5A (LJ-5A) lifted off normally, but 19 seconds later the escape tower fired prematurely, a situation closely resembling the November 1960 flight. The signal to initiate the abort maneuver was given; and the launch vehicle-adapter clamp ring was released as intended, but the spacecraft remained on the launch vehicle since the escape motor was already expended. The separation was effected by using the retrorockets, but this command was transmitted before the flight had reached its apex, where separation had been planned. Therefore, the separation was rather violent. The parachutes did deploy at about 40,000 feet, and after recovery it was found that the spacecraft had actually incurred only superficial structural damage. In fact, this spacecraft was later used for the subsequent Little Joe 5B (LJ-5B) flight test. Test objectives of the Little Joe 5A (LJ-5A) were not met.
References: 2.
1961 March 20 - -
Phase III of the Mercury spacecraft airdrop program Nation: USA. Program: Mercury. Spacecraft: Mercury. Primary objectives of the drops were to study further the spacecraft suitability and flotation capability after water impact. Six drops were made, but later (April 24-28, 1961) the tests were extended for two additional drops to monitor hard-surface landing effects. In the water phase of the program, spacecraft components under particular scrutiny were the lower pressure bulkhead and its capability to withstanding heat shield recontact without impairing flotation capability. Helicopters were used to make the drops.
References: 483.
1961 March 21 - Launch Vehicle: Atlas. Model: Atlas D. -
The Mercury-Atlas Missile Range Projects Office designated as a staff function Nation: USA. Program: Mercury. The Mercury-Atlas Missile Range Projects Office, headed by Elmer H. Buller, was designated as a staff function of the Space Task Group Director's office. References: 483.
1961 March 23 - Launch Vehicle: Saturn C-2, Saturn I. -
Configuration changes for the Saturn C-1 launch vehicles Nation: USA. Program: Apollo. Representatives of Marshall Space Flight Center recommended configuration changes for the Saturn C-1 launch vehicles to NASA Headquarters. These included: - Elimination of third-stage development, since two stages could put more than ten tons into earth orbit.
- Use of six LR-115 (15,000-pound) Centaur engines (second-stage thrust thus increased from 70,000 to 90,000 pounds).
- Redesign of the first stage (S-1) to offer more safety for manned missions.
Plans were also presented to accelerate the development of the Saturn C- 2, and a recommendation was made that a prime contractor be selected to work on the second stage (S-II) of the C-2. NASA Headquarters approved the C-2 plans on March 31.
References: 16.
1961 March 23 - -
Cosmonaut Bondarenko dies at age of 24. Nation: USSR. Program: Vostok. Spacecraft: Vostok. Flight: Vostok 1. At Tyuratam in the morning, LII engineers brief the cosmonauts on correcting the Globus instrument in flight, which indicates their position over the earth. Korolev checks in for a few minutes to make sure the cosmonauts have everything they need. In the evening the news of the death of cosmonaut Bondarenko reaches the cosmodrome. He died on the tenth day of a 15-day endurance experiment in a pressure chamber at IAKM when a fire broke out in the pure-oxygen cabin. Kamanin blames his death on IAKM's poor organisation and control of the experiment.
References: 376.
1961 March 23 - 19:25 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1E-17. -
Operational test Nation: USA. Agency: USN. Apogee: 500 km (310 mi). References: 2.
1961 March 24 - -
Mercury MR-3A (cancelled) Nation: USA. Program: Mercury. Payload: Mercury SC7. Spacecraft: Mercury. Location of Spacecraft: U.S. Naval Academy, College of Medicine, Anapolis, MD. Crew: Shepard. Flight: Mercury MR-3A. After booster problems on the Mercury MR-2 chimp test flight, Von Braun insisted on a further unmanned booster test flight, against the wishes of Shepard and others at NASA. A Mercury boilerplate capsule was launched on a flawless test on 24 March. If NASA had overruled Von Braun, the manned Freedom 7 capsule would have flown instead. Shepard would have been the first man in space (though not in orbit), beating Gagarin's flight by three weeks.
References: 26, 33, 59, 60.
1961 March 24 - -
Mercury MR-BD Nation: USA. Program: Mercury. Spacecraft: Mercury. After analyzing launch vehicle behavior in the Mercury-Redstone 1A (MR-1A) and Mercury-Redstone 2 (MR-2), officials at the Marshall Space Flight Center and the Space Task Group were of the opinion that there were a number of problems that needed to be corrected prior to the advent of manned flight. The problems to be resolved included jet-vane vibration, instrumentation compartment vibration, failure of the thrust-controller system, and several other areas that needed attention. Many of these problems were studied by the personnel of engineering activities and proposed solutions were formulated. It was felt, however, that flight was necessary to verify the corrections and the Mercury-Redstone Booster Development test was scheduled and flown. All test objectives were met; as a result of this test, the launch vehicle was man-rated for the planned suborbital flights.
References: 483.
1961 March 24 - 17:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC5. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone MRLV. LV Configuration: Redstone MRLV-5. -
Mercury MR-BD Nation: USA. Agency: NASA. Apogee: 181 km (112 mi). Suborbital test of Redstone modifications using a boilerplate Mercury capsule. The test was done at von Braun's insistence against Shepard's wishes, thereby putting the first US manned flight after Gagarin's. References: 2.
1961 March 25 - 01:49 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas E. LV Configuration: Atlas E 16E. FAILURE: Failure. -
Research and development launch Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
1961 March 25 - 05:54 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K. LV Configuration: Vostok 8K72K E103-15. -
Korabl-Sputnik 5 Nation: USSR. Program: Vostok. Payload: Vostok 3KA s/n 2. Mass: 4,695 kg (10,350 lb). Class: Manned. Type: Spacecraft. Spacecraft: Vostok. Agency: RVSN. Perigee: 175 km (108 mi). Apogee: 175 km (108 mi). Inclination: 64.90 deg. Period: 88.00 min. COSPAR: 1961-Iota-1. USAF Sat Cat: 95. Duration: 0.0600 days. Decay Date: 1961-03-25. Flight: Vostok 1. Carried dog Zvezdochka and mannequin Ivan Ivanovich. Ivanovich was again ejected from the capsule and recovered by parachute, and Zvezdochka was successfully recovered with the capsule on March 25, 1961 7:40 GMT. Officially: Development of the design of the space ship satellite and of the systems on board, designed to ensure man's life functions during flight in outer space and return to Earth.
Additional Details: Korabl-Sputnik 5. References: 2, 6, 175, 376.
1961 March 25 - 15:17 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta. LV Configuration: Thor Delta 295/D4. -
Explorer 10 Nation: USA. Program: Explorer. Payload: P-14. Mass: 35 kg (77 lb). Class: Solar. Spacecraft: P-14. Agency: NASA. Perigee: 221 km (137 mi). Apogee: 181,100 km (112,500 mi). Inclination: 33.00 deg. Period: 5,013.90 min. COSPAR: 1961-Kappa-1. USAF Sat Cat: 98. Decay Date: 1961-06-30. Magnetic field data. Decay date suspect Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 2, 6.
1961 March 26 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5. LV Configuration: R-5 V-1000 target. -
Target mission Nation: USSR. Agency: OKB-30. Apogee: 300 km (180 mi). References: 2.
1961 March 26 - 16:54 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 300A. LV Configuration: Aerobee 300A NASA 06.04UI. -
UM ionospheric Ionosphere mission Nation: USA. Agency: NASA. Apogee: 386 km (239 mi). NASA Aerobee research rocket with University of Michigan payload shot to 406-km altitude from Wallops Station. References: 2.
1961 March 27 - 04:08 GMT - Launch Site: Akita. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8. LV Configuration: Kappa 8 K-8-5. -
Ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 172 km (106 mi). References: 2.
1961 March 28 - -
USAF/NASA Dynasoar review. Nation: USA. Class: Manned. Type: Spaceplane. Spacecraft: Dynasoar. USAF Dyna-Soar System Project Office personnel visited NASA headquarters for review of technical and management programs. References: 18.
1961 March 28 - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I AJ-14. -
Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi). References: 2.
1961 March 29-30 - -
Convair selects M-1 design for Apollo in preference to lenticular configuration Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. William W. Petynia of STG visited the Convair Astronautics Division of General Dynamics Corporation to monitor the Apollo feasibility study contract. A selection of the M-1 in preference to the lenticular configuration had been made by Convair. May 17 was set as the date for the final Convair presentation to NASA.
References: 16.
1961 March 30 - Launch Vehicle: Saturn I. Model: Saturn I RIFT. -
RIFT flight briefed to contractors. Nation: USA. Program: NERVA. Reactor-in-flight-test system (Rift) study, a part of the NASA-AEC program on nuclear rockets, was briefed by contractors at NASA headquarters. References: 18.
1961 March 30 - Launch Site: Offutt AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. -
Atlas SMS 566 operational. Nation: USA. Offutt AFB SMS 566 operational References: 4460.
1961 March 30 - 05:13 GMT - Launch Site: Vandenberg. Launch Complex: SLC10E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor DM-18A. LV Configuration: Thor DM-18A 243. -
Combat training launch Nation: USA. Agency: RAF. Apogee: 520 km (320 mi). References: 2.
1961 March 30 - 18:05 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 2-14-28. -
X-15A Alt., BCS, Aero test Nation: USA. Agency: NASA/USAF. Apogee: 51 km (31 mi). Maximum Speed - 4441 kph. Maximum Altitude - 51700 m. References: 2.
1961 March 30 - 20:34 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena B. LV Configuration: Thor Agena B 300 / Agena B 1105. FAILURE: Failure. -
Discoverer 22 Nation: USA. Payload: KH-2 9015. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-2. Agency: U.S. Air Force. COSPAR: F610330A. Decay Date: 1961-03-30. KH-2; Mission failed. References: 126.
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SRV 509 Nation: USA. Spacecraft: KH-2. Agency: USAF. COSPAR: F610330B. References: 279.
1961 March 31 - -
MHD / Thermal arc jet engine contracts. Nation: USA. NASA selected GE's Space Sciences Laboratory and Avco Corp. for negotiation of contracts to study feasibility of magneto gas dynamic electric rocket or thermal arc jet rocket engines. References: 18.
1961 March 31 - -
All stations of NASA's world-wide Mercury tracking network were classed as being operational. Nation: USA. Program: Mercury. An industrial team headed by the Western Electric Company turned over the $60,000,000 global network (figs. 48 and 49) to NASA in a formal ceremony later in the year. References: 483.
1961 March 31 - 19:42 GMT - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I AJ-15. FAILURE: Failure. -
Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 0 km ( mi). References: 2.
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