See also Born on this Day On this day in: 1801 - -
Guiseppe Piazzi's Discovery of the First Asteroid (Ceres) Nation: Italy.
1941 - Launch Vehicle: RCA Dragon. -
Aerial torpedo proposed. Nation: USA. RCA proposed to NDRC design and developoment of rocket-propelled, radio-controlled aerial torpedo with TV nose, which was given code name "Dragon." The National Bureau of Standards was assigned the task of developing a suitable airframe.
1942 - -
Declaration of United Nations signed in Washington Nation: International.
1944 - Launch Vehicle: Corporal. -
Private and Corporal missile development begun. Nation: USA. At request of Army Ordnance, Cal Tech's rocket laboratory started research and development program on long-range missiles, called Project ORDCIT, which resulted in development of Private "A" and Corporal missiles.
1949 -
1950 - Launch Vehicle: Buran, Burya, MKR.
1952 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Deacon. Model: Double Deacon. LV Configuration: Double Deacon Double Deacon. FAILURE: Failure. -
X-2 Model test flight Nation: USA. Agency: NACA. Apogee: 0 km ( mi).
1956 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-11. Model: R-11M. -
Test mission Nation: USSR. Agency: NII-88. Apogee: 150 km (90 mi).
1956 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M. -
Certification test Nation: USSR. Agency: NII-88. Apogee: 500 km (310 mi).
1956 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M. -
Certification test Nation: USSR. Agency: NII-88. Apogee: 500 km (310 mi).
1956 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M. -
Certification test Nation: USSR. Agency: NII-88. Apogee: 500 km (310 mi).
1956 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M.
1958 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
1958 - Launch Vehicle: Delta. Model: Thor.
1959 - Launch Vehicle: Saturn V.
1959 - -
Cuban President Batista resigns and flees - Castro takes over Nation: USA.
1961 -
1961 - -
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 - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Kisha Judi. -
Test mission Nation: USA. Agency: Sandia. Apogee: 100 km (60 mi).
1962 -
1964 - Launch Site: Barbados. Launch Complex: HARP. Launch Pad: -. Launch Vehicle: Martlet. Model: Martlet 2. -
Test mission Nation: Canada. Agency: HARP. Apogee: 80 km (49 mi).
1965 -
1965 -
1965 - Launch Vehicle: Spiral 50-50.
1965 -
1966 - -
Study grants for AAP astonomical instrumentation to be flown in the 1969-1975 period. Nation: USA. Spacecraft: Orbital Workshop. Homer E. Newell, Associate Administrator for Space Science and Applications, announced opportunities for study grants to competent astronomers for conceptual and preliminary design work leading to instrumentation to be flown in the 1969-1975 period. A description of the Apollo telescope mount was included.
1967 - Launch Vehicle: Soyuz. Model: Voskhod 11A57.
1971 -
1972 - Launch Vehicle: N1, RT-2. -
TsKBEM reorganised Nation: USSR. Program: Lunar L3, Soyuz, Almaz. Spacecraft: LK, Soyuz 7K-LOK, Soyuz 7K-TM, Soyuz 7K-T, Soyuz 7K-S, Soyuz 7K-OK, MKBS, Mars 5NM. TsKBEM was given a completely new structure as a result of the findings of the expert commissions on the disasters for the previous year, Mishin remained as the Chief Designer for the organisation, but each programme now had its own chief designer: - N1: Boris Dorofeyev
- 8K98P solid propellant ICBM: Igor Sadovskiy
- N1 payloads: Vladimir Brorov [check]
- Soyuz 7K-TM, or Soyuz M, for Soyuz-Apollo: Konstantin Bushuyev
- Soyuz 7K-T: Yuri Semenov
- Soyuz 7K-S or Soyuz VI: Yevgeni Shabarov
- Additional details.
1972 - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: RT-2. Model: RT-2P. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1972 - 07:05 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 24.0 N x 53.0 W. Launch Vehicle: MR-12. -
Aeronomy mission Nation: USSR. Apogee: 180 km (110 mi).
1972 - 08:02 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission Nation: USSR. Apogee: 180 km (110 mi).
1973 - Launch Vehicle: N1. Model: N1F-L3M.
1974 - Launch Site: Kapustin Yar. Launch Complex: LC107/1. Launch Pad: LC107/pad?. Launch Vehicle: Kosmos 3. Model: Vertikal-4. -
Ionosphere/Solar mission? Nation: USSR. Agency: RVSN. Apogee: 1,500 km (900 mi).
1974 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. -
LRL ACS 11 X-ray Astronomy mission Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).
1975 - Launch Vehicle: UR-700. LV Configuration: UR-700M. -
Chelomei presents plan for Mars mission Nation: USSR. Class: Manned. Type: Mars flyby. Spacecraft: MK-700. As the only remaining contender for the Aelita design competition, Chelomei proposes a Mars flyby using an MK-700 spacecraft. A crew of two would be sent on a two year mission in a single launch of a UR-700M booster. The spacecraft would have a mass of 250 tonnes in low earth orbit and be equipped with an RD-410 nuclear engine.
1975 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
1975 - Launch Vehicle: N1, RLA. -
Vulkan Lunar Base Nation: USSR. Program: Lunar L3. Spacecraft: LZhM, LZM, Lunokhod LEK, LEK. Mishin and Barmin, using budget provided by the Ministry of Defence, had designed a lunar base for launch by the N1 in 1969-1974. After the cancellation of the N1, Glushko pleaded with the Military-Industrial Commission for the work to be taken from Barmin and be given to NPO Energia. Glushko's alternative, Vulkan-launched base was elaborated within his bureau. Bushuyev developed spacecraft for the base. Prudnikova developed a modular lunar city, with living modules, factory modules, a nuclear reactor power module, and a lunar crawler with a 200 km radius of action. The project work was only finally cancelled after the Apollo-Soyuz flights.
1975 - Launch Vehicle: Energia, RLA.
1975 - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-310. LV Configuration: S-310-1. -
Test mission Nation: Japan. Agency: ISAS. Apogee: 200 km (120 mi).
1977 -
1978 -
1978 - Launch Vehicle: Energia, RLA. -
Vulkan Lunar Base rejected Nation: USSR. Spacecraft: LZhM, LZM, Lunokhod LEK, LEK. An expert commission led by Keldysh examines the plan for a lunar base launched by the Vulkan booster. The plan is completely rejected. NPO Energia was told to quit dreaming and devote itself only to projects with national economic importance, like Buran. This put a definitive end to Glushko's lunar base projects studied in 1976-1978. But he just waited and started design work again on a lunar base using the Energia launch vehicle after the first Buran launch in 1988.
1978 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100N. -
Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1978 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100N. -
Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1979 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
1980 -
1980 - Launch Site: Nenoksa. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-39. Model: Rif. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1980 - Launch Site: Nenoksa. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-39. Model: Rif. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1980 - Launch Site: Nenoksa. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-39. Model: Rif. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1980 - Launch Site: Nenoksa. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-39. Model: Rif. -
Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1982 - Launch Site: Nenoksa. Launch Complex: -. Launch Pad: -. Launch Vehicle: RT-23. Model: RT-23 15Zh44. LV Configuration: RT-23 15Zh44 15Zh44. -
Silo test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1984 - -
Space Command assumed resource management responsibility for Global Positioning System. Nation: USA.
1990 -
1990 - 00:07 GMT - Launch Site: Cape Canaveral. Launch Complex: LC40. Launch Pad: -. Launch Vehicle: Titan. Model: Commercial Titan 3. LV Configuration: Commercial Titan 3 CT-1. -
Skynet 4A Nation: UK. Program: Skynet. Payload: Skynet 4A [PAM-D2] / JCSat 2 [Orbus-7S]. Mass: 1,463 kg (3,225 lb). Class: Communications. Type: Military. Spacecraft: ECS/OTS. Agency: UK MoD. Perigee: 35,782 km (22,233 mi). Apogee: 35,790 km (22,230 mi). Inclination: 5.50 deg. Period: 1,436.10 min. COSPAR: 1990-001A. USAF Sat Cat: 20401. British military communications; 6 deg E. Military communications. Expected life approx 7 years. Owner/operator: Ministry of Defence, Main Building, Whitehall, London SW1A 2HB. Positioned in geosynchronous orbit at 6 deg E in 1990; 29 deg E in 1991; 65 deg E in 1991; 34 deg W in 1992-1999 As of 5 September 2001 located at 34.01 deg W drifting at 0.003 deg W per day. As of 2007 Mar 11 located at 63.46W drifting at 4.595W degrees per day.
1996 -
1996 -
1998 -
Born on this day in:
Died on this day in: . German Engineer.
- 1990 - James Wayne Wood. American Pilot Astronaut. Cause of Death: Natural causes.
- 1996 - Arthur Louis Hugo Rudolph. German Rocket engineer.
- 1996 - Arleigh A Burke. American Manager.
- 2005 - Heinz Ludwig Schnarowski. German Rocket engineer.
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