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1905 -

  • Charles Perrine's Discovery of Jupiter Moon Elara Nation: Argentina.

1917 -
  • Goddard receives grant for rocket research Nation: USA.

    Goddard receives US$ 5,000 Hodgkins Fund grant from Smithsonian, allowing him to continue development of the cartridge rocket.

1949 -
  • XS-1 Flight 104 Nation: USA. Payload: XS-1 # 1 flight 61. Class: Manned. Type: Rocketplane. Spacecraft: XS-1. Crew: Yeager.

    AF flight 39. Rocket takeoff from the ground.

1956 -
  • Institute of Mechanics founded in Beijing Nation: China.

    Tsien is director of the institute. It is equipped with mechanical desk calculators and only one telephone. Deputy Director is a Tsien protege, Dr Guo Yonghuai, who graduated with a doctorate in aeronatuical engineering from Caltech in 1946. The Director of Operations is Xu Guozhi, a systems analyst that Tsien met on the ship from America to China.

1959 -
  • Cosmonaut selection for Vostok flights authorised. Nation: USSR.

    Central Committee of the Communist Party and Council of Soviet Ministers Decree 22-10ss 'On biomedical preparations for human spaceflight' was issued.

1959 -
  • Mercury pilot selection qualifications Nation: USA. Program: Mercury.

    Qualifications were established for pilot selection in a meeting at the NASA Headquarters. These qualifications were as follows: age, less than 40; height, less than 5 feet 11 inches; excellent physical condition; bachelor's degree or equivalent; graduate of test pilot school; 1,500 hours flight time; and a qualified jet pilot.

1961 - 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.

1962 - Launch Vehicle: Saturn V.
  • Three-man Apollo spacecraft, Saturn C-5 launch vehicle announced Nation: USA. Program: Apollo. Spacecraft: Apollo Lunar Landing.

    NASA made public the drawings of the three-man Apollo spacecraft to be used in the lunar landing development program, On January 9, NASA announced its decision that the Saturn C-5 would be the lunar launch vehicle.

1962 - 15:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. LV Configuration: Minuteman 1A 407.
  • Research and development launch Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi).

1965 -
  • Study of manual control of the Apollo LEM Nation: USA. Program: Apollo. Spacecraft: Apollo LM.

    MSC's Guidance and Control Division conducted a pilot simulation study to determine whether a pilot could take over manual control of the LEM between 4,572 and 3,048 m (15,000 and 10,000 ft) above the lunar surface and satisfactorily land the vehicle. - Additional details.

1965 - Launch Vehicle: Titan. Model: Titan 2.
  • NASA Headquarters provided Flight Operations Division with preliminary data for revising the Gemini-Titan (GT) 3 flight plan to cover the possibility of retrorocket failure. Nation: USA. Flight: Gemini 3, Gemini 4.

    The problem was to ensure the safe reentry of the astronauts even should it become impossible to fire the retrorockets effectively. The Headquarters proposal incorporated three orbit attitude and maneuver system maneuvers to establish a fail-safe orbit from which the spacecraft would reenter the atmosphere whether the retrorockets fired or not. This proposal, as refined by Mission Planning and Analysis Division, became part of the flight plans for GT-3 and GT-4.

1966 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 461.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 -
  • Cosmonaut training status Nation: USSR. Program: Lunar L1, Soyuz, Almaz. Spacecraft: Voskhod, Soyuz 7K-OK, Soyuz 7K-L1, Almaz OPS, Soyuz VI.

    Crews are in training for Voskhod, Soyuz, Lunar L-1, Almaz, and 7K-VI missions. There will be 100 cosmonauts in training by February. Meanwhile the Americans have conducted 10 manned flights since the last Soviet manned flight in March 1965. The cosmonauts want Kamanin to be training 8 crews for L-1 translunar flights, but he only has 4 in training. He doesn't think it is worth to train more, since if one successful L-1 flight is conducted before the 50th Anniversary of the Soviet Union in November 1957, all subsequent flights will be cancelled.

    The cosmonauts are also pressing for a meeting with Brezhnev to discuss planned military experiments, the role of the pilot in spacecraft, and the mistakes of OKB-1 in spacecraft design. Kamanin thinks this would be too risky - unforeseen results could occur. Titov is assigned to the Spiral spaceplane programme. Kamanin thinks the project is risky and likely to be cancelled. But Titov enjoys being able to fly high performance MiG-21 aircraft, and has wanted out of the main cosmonaut program for a long time. There is constant high level pressure on Kamanin to assign OKB-1 engineer cosmonaut candidates to crews and fly them.

1968 -
  • Plan for lunar exploration by Apollo through the mid-1970s Nation: USA. Program: Apollo. Spacecraft: Apollo LM.

    Bellcomm engineers presented to NASA a proposed plan for lunar exploration during the period from the first lunar landing through the mid-1970s. The proposed program - based upon what the company termed "reasonable" assumptions concerning hardware capabilities, scientific objectives, launch rates, and relationships to other programs - was divided into four distinct phases:

    1. an Apollo phase using existing vehicles,
    2. a lunar exploration phase employing an extended LM with increased payload and longer staytime,
    3. a lunar orbital survey and exploration phase using remote sensors and photographic equipment on a polar orbit flight, and
    4. a lunar surface rendezvous and exploration phase using an unmanned LM to deposit the increased scientific equipment and expendables necessary to extend Apollo's manned lunar capability to two-week duration.
1968 -
  • NASA lunar exploration program developed for the period from the first lunar landing to the mid-1970s. Nation: USA. Spacecraft: Apollo LM Taxi, Apollo LM Truck, Apollo ATM, Apollo LMSS.

    A lunar exploration program had been developed which would cover the period from the first lunar landing to the mid-1970s. The program would be divided into four phases: (1) An Apollo phase employing Apollo hardware. (2) A lunar exploration phase untilizing an extended LM with increased landed payload weight and staytime capability. (3) A lunar orbital survey and exploration phase using the AAP-1A carrier or the LM/ATM to mount remote sensors and photographic equipment on a manned polar orbit mission. (4) A lunar surface rendezvous and exploration phase which would use a modified LM in an unmanned landing to provide increased scientific payload and expendables necessary to extend an accompanying manned LM mission to two weeks duration.

1969 - 06:28 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
  • Venera 5 Nation: USSR. Program: Venera. Payload: 2V (V-69) s/n 330. Mass: 1,128 kg (2,486 lb). Class: Planetary. Type: Venus. Spacecraft: Venera 2V (V-69). Agency: MOM. COSPAR: 1969-001A. USAF Sat Cat: 3642. Decay Date: 1969-05-16.

    Venera 5 is launched at 9:26 Moscow time from LC-31 in -23 deg C temperatures. All proceeds according to plan. Afterwards Kamanin meets Babakin. Venera 6 is planned for launch in 10 January. He also plans two moon landings in 1969 and two in 1970 of soil sample return spacecraft. Kamanin does not believe America can achieve a manned moon landing in 1969, and therefore that Babakin has a very good chance of stealing their thunder.

    Meanwhile Venera 5 was launched from its parking orbit towards Venus to obtain atmospheric data. The spacecraft was very similar to Venera 4 although it was of a stronger design. When the atmosphere of Venus was approached, a capsule weighing 405 kg and containing scientific instruments was jettisoned from the main spacecraft. During satellite descent towards the surface of Venus, a parachute opened to slow the rate of descent. For 53 min on May 16, 1969, while the capsule was suspended from the parachute, data from the Venusian atmosphere were returned. The spacecraft also carried a medallion bearing the coat of arms of the U.S.S.R. and a bas-relief of V.I. Lenin to the night side of Venus.

1971 -
  • VVS Reviews TsKBEM Facilities and Programs Nation: USSR. Program: Salyut, Lunar L3. Spacecraft: Salyut 1, Soyuz 7K-LOK.

    Two hour meeting between the VVS leadership and Mishin at TsKBEM. Mishin claims he will fly the N1 to orbit this year, and that it will have a payload of 95 to 100 tonnes to low earth orbit. He wants to make 4 to 5 unmanned launches in 1971-1972, followed by one unmanned lunar flyby, culminating in the first Soviet cosmonaut landing on the moon in March 1973. Afterwards the VVS leaders tour the L3 and DOS-7K mock-ups. Mishin asks - Why won't the VVS support his plan for an Indian Ocean landing for the L3? Why is the VVS against a 30-day duration for the first DOS flight? Why isn't the VVS training engineer-cosmonauts as pilots? Kutakhov replies that these are decisions that have to be made by aviation specialists, not by engineers or chief designers. The General Staff supports the VVS position.

1972 - 11:41 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Ionosphere mission Nation: USSR. Apogee: 186 km (115 mi).

1974 - 01:45 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.23UG-UP.
  • JHU UVS Kohoutek Optical / ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 233 km (144 mi).

1978 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.533UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 197 km (122 mi).

1984 - 20:00 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 14 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 120 km (70 mi).

1984 - 20:09 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47119-529.
  • Cosmos 1522 Nation: USSR. Program: Strela. Payload: Strela-1M no. 265. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,461 km (907 mi). Apogee: 1,493 km (927 mi). Inclination: 74.00 deg. Period: 115.50 min. COSPAR: 1984-001A. USAF Sat Cat: 14611.

    Eight satellites launched by a single carrier rocket.

  • Cosmos 1523 Nation: USSR. Program: Strela. Payload: Strela-1M no. 266. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,396 km (867 mi). Apogee: 1,462 km (908 mi). Inclination: 74.00 deg. Period: 114.40 min. COSPAR: 1984-001B. USAF Sat Cat: 14612.

  • Cosmos 1524 Nation: USSR. Program: Strela. Payload: Strela-1M no. 267. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,412 km (877 mi). Apogee: 1,462 km (908 mi). Inclination: 74.00 deg. Period: 114.60 min. COSPAR: 1984-001C. USAF Sat Cat: 14613.

  • Cosmos 1525 Nation: USSR. Program: Strela. Payload: Strela-1M no. 268. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,427 km (886 mi). Apogee: 1,462 km (908 mi). Inclination: 74.00 deg. Period: 114.80 min. COSPAR: 1984-001D. USAF Sat Cat: 14614.

  • Cosmos 1526 Nation: USSR. Program: Strela. Payload: Strela-1M no. 269. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,443 km (896 mi). Apogee: 1,462 km (908 mi). Inclination: 74.00 deg. Period: 114.90 min. COSPAR: 1984-001E. USAF Sat Cat: 14615.

  • Cosmos 1527 Nation: USSR. Program: Strela. Payload: Strela-1M no. 270. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,459 km (906 mi). Apogee: 1,462 km (908 mi). Inclination: 74.00 deg. Period: 115.10 min. COSPAR: 1984-001F. USAF Sat Cat: 14616.

  • Cosmos 1528 Nation: USSR. Program: Strela. Payload: Strela-1M no. 271. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,461 km (907 mi). Apogee: 1,477 km (917 mi). Inclination: 74.00 deg. Period: 115.30 min. COSPAR: 1984-001G. USAF Sat Cat: 14617.

  • Cosmos 1529 Nation: USSR. Program: Strela. Payload: Strela-1M no. 272. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,461 km (907 mi). Apogee: 1,512 km (939 mi). Inclination: 74.00 deg. Period: 115.70 min. COSPAR: 1984-001H. USAF Sat Cat: 14618.

1987 - 01:20 GMT - Launch Site: Plesetsk. Launch Complex: LC32. Launch Pad: LC32/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-3.
  • Meteor 2-15 Nation: USSR. Payload: Meteor-2 no. 15. Mass: 2,750 kg (6,060 lb). Class: Earth. Type: Weather. Spacecraft: Meteor-2. Agency: MO SSSR. Perigee: 939 km (583 mi). Apogee: 956 km (594 mi). Inclination: 82.50 deg. Period: 104.00 min. COSPAR: 1987-001A. USAF Sat Cat: 17290.

    Gathering meteorological information and data on penetrating radiation fluxes in circumterrestrial space.

1999 -
  • Energia Engineer Cosmonaut Training Group 14 Supplemental selected. Nation: Russia.


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