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On this day in:

1820 -

  • Royal Astronomical Society founded. Nation: UK.

1945 - Launch Site: Peenemuende. Launch Complex: -. Launch Pad: -. Launch Vehicle: V-2.
  • Arbeitstab Dornberger Nation: Germany.

    Speer puts Dornberger in charge of an office within the Munitions Ministry to oversee further development of the A4 and other rockets, drawing on staff from Peenemuende. Everyone knew the war would be over in a few months -- nothing could be accomplished. Kammler still made sure that Dornberger was only responsible for technical aspects. All further developments of the A4 had been on hold for years, and any further work was now impossible. Only simple things could be worked on, such as converting 6 cm smoke rockets to use as an air-to-air weapon. In the short turnaround typical of the times, the team drove to Kummersdorf and built a 21-cm diameter pipe that could fire a barrage of four smoke rockets. Two days later, it was reported back that the device was used successfully in combat, and it was put into production. It was first used against allied bombers over Schweinfurt in January 1945.

1948 -
  • Test vehicles reach 1,019 mph. Nation: USA.

    Northrop Aircraft Co. announced that rocket-powered test vehicles at Muroc Air Base, Calif., had attained a speed of 1,019 mph.

1955 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: R-7.
  • Tyuratam selected for ICBM test range. Nation: USSR.

    Council of Ministers selects Tyuratam for ICBM test site. The first 30 construction workers arrive at Tyuratam. The town founded at the rail staion is called Zarya (Dawn). The name will be changed to Leninsk in January 1958, but Zarya will remain the call sign of Soviet ground control.

1958 -
  • Special Committee on Space Technology established Nation: USA. Spacecraft: Apollo CSM.

    NACA established a Special Committee on Space Technology to study the problems of space flight. H. Guyford Stever of the Massachusetts Institute of Technology (MIT) was named Chairman. On November 21, 1957, NACA had authorized formation of the Committee.

1958 -
  • Eisenhower proposed to Russia that outer space should be used for peaceful purposes. Nation: USA.

    President Eisenhower, answering a December 10, 1957, letter from Soviet Premier Nikolai A. Bulganin regarding a summit conference on disarmament, proposed that Russia and the United States '. . . agree that outer space should be used for peaceful purposes.' This proposal was compared dedicate atomic energy to peaceful uses, an offer which The Soviets rejected.

1959 -
  • McDonnell awarded contract for Mercury project Nation: USA. Program: Mercury. Class: Manned. Type: Spacecraft. Spacecraft: Mercury.

    12 capsules to be built. Other leading contender was Grumman. Original schedule was for manned flights from January - August 1960.

1961 - 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 - 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).

1964 - 00:26 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.130IA.
  • ISRO 10.03? (Na) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 187 km (116 mi).

1965 -
  • Various designs for the extravehicular mobility unit Nation: USA. Program: Apollo. Spacecraft: Apollo LM.

    Grumman and Hamilton Standard were exploring various designs for the extravehicular mobility unit. On the basis of some early conclusions, the MSC Crew Systems Division (CSD) recommended that meteoroid and thermal protection be provided by a single garment. Preliminary hypervelocity tests placed the garment's reliability at 0.999. Each would weigh about 7.7 kg (17 lbs), about 2.3 kg (5 lbs) less than the two-garment design. CSD further recommended that the unit be stored either in the LEM's descent stage or in a jettisonable container in the ascent portion.

1965 - Launch Vehicle: Titan. Model: Titan 2.
  • Flight tests of the zero-gravity mock-up of the Gemini spacecraft began. Nation: USA. Flight: Gemini 4.

    The mock-up was installed in a KC-135 aircraft to provide astronauts with the opportunity to practice extravehicular activities under weightless conditions. The Gemini-Titan (GT) 3 flight crew participated in the opening exercises, which were duplicated the next day by the GT-4 flight crew.

1965 - Launch Vehicle: Tsiklon.
  • R-36 'sealed round' version development authorised. Nation: USSR.

    State Committee for Defence Technology (GKOT) Decree 'On Detailed Work on Ampulized R-36 and R-36-O Missiles--design work on the R-36 and R-36-O missiles' was issued.

1965 - 14:32 GMT - Launch Site: Vandenberg. Launch Complex: 576B1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 166D.
  • NTMP RMV-302 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).

1966 - 14:00 GMT - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Boosted Dart. LV Configuration: Boosted Dart EXAMETNET 1.
  • 04 CNAE 6601 Aeronomy mission Nation: USA. Agency: CNAE. Apogee: 60 km (37 mi).

1969 -
  • Soyuz 4/5 profile still not settled Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 4, Soyuz 5, Soyuz 4/5.

    At Baikonur, Ustinov and Afanasyev get into an argument with Mishin. They want Soyuz 4 and 5 to accomplish a completely automatic docking, as was done successfully by Cosmos 186/188 and Cosmos 212/213. Mishin categorically rejects this. He wants a manual docking, which was unsuccessful when attempted by Beregovoi on Soyuz 2/3. Meanwhile the Soyuz 4/5 crews hold a news conference.

1969 - 01:32 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.652.
  • AFGL TMA release Aeronomy mission Nation: USA. Agency: USAF. Apogee: 157 km (97 mi).

1969 - 05:10 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 10C. LV Configuration: Kappa 10C K-10C-1.
  • Stability test Aeronomy / solar ultraviolet / test Nation: Japan. Agency: ISAS. Apogee: 229 km (142 mi).

1969 - 12:10 GMT - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 263 Nation: USSR. Payload: Zenit-2 11F61 s/n 70. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 200 km (120 mi). Apogee: 325 km (201 mi). Inclination: 65.40 deg. Period: 89.70 min. COSPAR: 1969-003A. USAF Sat Cat: 3651. Duration: 8.00 days. Decay Date: 1969-01-20.

    Area survey photo reconnaissance satellite.

1970 -
  • Dale D Myers' appointed NASA Associate Administrator for Manned Space Flight Nation: USA. Program: Apollo.

    Dale D. Myers' appointment as NASA Associate Administrator for Manned Space Flight was announced effective January 12, to succeed Dr. George E. Mueller, who had joined General Dynamics Corp. in New York City as a Vice President. Before this appointment, Myers was Vice President and General Manager of the Space Shuttle Program, North American Rockwell Corp.

1971 - 07:50 GMT - Launch Site: Point Barrow. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.366GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 116 km (72 mi).

1971 - 09:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 390 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 196 km (121 mi). Apogee: 276 km (171 mi). Inclination: 65.00 deg. Period: 89.20 min. COSPAR: 1971-001A. USAF Sat Cat: 4845. Duration: 13.00 days. Decay Date: 1971-01-25.

    High resolution photo reconnaissance satellite; returned film capsule; maneuverable.

1971 - 20:53 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.373GM.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 133 km (82 mi).

1972 - 09:59 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 471 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 201 km (124 mi). Apogee: 316 km (196 mi). Inclination: 65.00 deg. Period: 89.70 min. COSPAR: 1972-001A. USAF Sat Cat: 5764. Duration: 13.00 days. Decay Date: 1972-01-25.

    High resolution photo reconnaissance satellite; returned film capsule; maneuverable.

1972 - 21:16 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.383AE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 197 km (122 mi).

1973 - 08:05 GMT - Launch Site: Green River. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. Model: Athena H. LV Configuration: Athena H H005.
  • RANT Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1973 - 10:05 GMT - Launch Site: Green River. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. Model: Athena H. LV Configuration: Athena H H009.
  • ABC-1 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1973 - 11:46 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 KP3.42.
  • X-ray astronomy mission Nation: USA. Agency: KPNO. Apogee: 229 km (142 mi).

1974 - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67.
  • DKh state trials flight Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 - 19:12 GMT - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: Skylark. Model: Skylark 4 AC. LV Configuration: Skylark 4 AC HRC 1.
  • DLR H-GR-58 X-ray astronomy mission Nation: Germany. Agency: DFVLR. Apogee: 246 km (152 mi).

1982 - 12:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1332 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MT. Agency: MOM. Perigee: 207 km (128 mi). Apogee: 251 km (155 mi). Inclination: 82.30 deg. Period: 89.00 min. COSPAR: 1982-002A. USAF Sat Cat: 13031. Duration: 13.00 days. Decay Date: 1982-01-25.

    Military topography satellite; returned film capsule; also performed mapping, geodesy.

1983 - 14:02 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65093-479.
  • Cosmos 1428 Nation: USSR. Mass: 810 kg (1,780 lb). Class: Navigation. Spacecraft: Parus. Agency: MO SSSR. Perigee: 952 km (591 mi). Apogee: 1,001 km (621 mi). Inclination: 82.90 deg. Period: 104.60 min. COSPAR: 1983-001A. USAF Sat Cat: 13757.

    Military navigation satellite. Replaced Cosmos 1333.

1983 - 19:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Honest John. Model: Taurus Orion. LV Configuration: Taurus Orion NASA 33.30UU.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1984 - 17:00 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 17 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 118 km (73 mi).

1986 - 11:55 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-32/61-C.
  • STS-61-C Nation: USA. Program: STS. Payload: Columbia F07 Satcom-K 1 [PAM-D2]. Mass: 14,724 kg (32,460 lb). Class: Manned. Type: Spaceplane. Spacecraft: Columbia. Agency: NASA JSC. Perigee: 331 km (205 mi). Apogee: 338 km (210 mi). Inclination: 28.50 deg. Period: 91.20 min. COSPAR: 1986-003A. USAF Sat Cat: 16481. Duration: 6.09 days. Decay Date: 1986-01-18. Crew: Bolden, Cenker, Chang-Diaz, Gibson, Hawley, Nelson, Nelson Bill. Flight: STS-61-C.

    Manned seven crew. Launched Satcom K1. Payloads: Deploy SATCOM (RCA-Satellite Communi-cations) Ku-1 with Payload Assist Module (PAM)-D II. Materials Science Laboratory, Comet Halley Active Monitoring Experiment (CHAMP), Hitchhiker (HH) Goddard (G)-1, thirteen getaway specials (GAS), student experiment, Initial Blood Storage Equipment (lBSE), Characterization of Space Motion Sickness (SMS).

  • Satcom K1 Nation: USA. Program: Satcom. Payload: Satcom-K 1 / PAM-D2. Mass: 1,923 kg (4,239 lb). Class: Communications. Spacecraft: AS 4000. Manufacturer: Lockheed Martin. Agency: RCA Amer. Perigee: 35,965 km (22,347 mi). Apogee: 36,016 km (22,379 mi). Inclination: 4.50 deg. Period: 1,446.50 min. COSPAR: 1986-003B. USAF Sat Cat: 16482. Completed Operations Date: 1997-07-02.

    Stationed at 81 deg W. Positioned in geosynchronous orbit at 85 deg W in 1986-1997; 87 deg W in 1997 As of 31 August 2001 located at 61.19 deg W drifting at 2.593 deg W per day. As of 2007 Mar 10 located at 125.55E drifting at 2.586W degrees per day.

  • MSL-2 Nation: USA. Program: STS. Agency: NASA. COSPAR: 1986-003xx. USAF Sat Cat: 16481. Decay Date: 1986-01-18.

  • GBA-1 Nation: USA. Program: STS. Payload: GAS Bridge. Agency: NASA. COSPAR: 1986-003xx. USAF Sat Cat: 16481. Decay Date: 1986-01-18.

1989 - 11:29 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1990 Nation: USSR. Program: Resurs. Mass: 6,300 kg (13,800 lb). Class: Earth. Type: Landsat. Spacecraft: Resurs F2. Agency: MOM. Perigee: 177 km (109 mi). Apogee: 227 km (141 mi). Inclination: 82.60 deg. Period: 88.50 min. COSPAR: 1989-002A. USAF Sat Cat: 19756. Duration: 30.00 days. Decay Date: 1989-02-11.

    Investigation of the natural resources of the earth in the interests of the national economy of the USSR and international cooperation; survey of seismically active regions of the country, including the Armenian SSR, in the interests of industrial and non -industrial construction.

1993 - 11:10 GMT - Launch Site: Plesetsk. Launch Complex: LC133/3. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53778-426.
  • Cosmos 2230 Nation: Russia. Payload: Tsikada. Mass: 825 kg (1,818 lb). Class: Navigation. Spacecraft: Tsikada. Agency: MO RF. Perigee: 969 km (602 mi). Apogee: 1,008 km (626 mi). Inclination: 82.90 deg. Period: 104.90 min. COSPAR: 1993-001A. USAF Sat Cat: 22307.

    Civilian navigation satellite. Positioned in plane 11 of constellation. TSIKADA type spacecraft. Determination of the position of ships of the merchant marine and fishing fleet in the world's oceans and seas as part of the Tsikada space navigation system.

1996 - 23:10 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: -. Launch Vehicle: Ariane. Model: Ariane 44L. LV Configuration: Ariane 44L-3 V82.
  • Panamsat 3R Nation: USA. Program: Panamsat. Payload: PAS K4. Mass: 2,900 kg (6,300 lb). Class: Communications. Spacecraft: HS 601. Agency: Panamsat. Perigee: 35,779 km (22,231 mi). Apogee: 35,796 km (22,242 mi). Inclination: 0.00 deg. Period: 1,436.20 min. COSPAR: 1996-002A. USAF Sat Cat: 23764.

    Geostationary at 43.0W. Positioned in geosynchronous orbit at 43 deg W in 1996-1999 As of 5 September 2001 located at 42.97 deg W drifting at 0.008 deg W per day. As of 2007 Mar 10 located at 42.99W drifting at 0.012W degrees per day.

  • Measat 1 Nation: Malaysia. Program: Measat. Mass: 1,450 kg (3,190 lb). Class: Communications. Spacecraft: HS 376. Agency: Binarian. Perigee: 35,783 km (22,234 mi). Apogee: 35,792 km (22,240 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 1996-002B. USAF Sat Cat: 23765.

    Geostationary at 91.4E. Positioned in geosynchronous orbit at 91 deg E in 1996-1999 As of 5 September 2001 located at 91.49 deg E drifting at 0.012 deg W per day. As of 2007 Mar 11 located at 91.50E drifting at 0.009W degrees per day.

1997 - 09:27 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39B. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-81.
  • STS-81 Nation: USA. Program: Mir. Payload: Atlantis F18 / Spacehab Double Module. Class: Manned. Type: Spaceplane. Spacecraft: Atlantis. Agency: NASA JSC. Perigee: 343 km (213 mi). Apogee: 380 km (230 mi). Inclination: 51.70 deg. Period: 91.80 min. COSPAR: 1997-001A. USAF Sat Cat: 24711. Duration: 10.20 days. Decay Date: 1997-01-22. Crew: Baker Mike, Jett, Wisoff, Grunsfeld, Ivins, Linenger. Flight: Mir NASA-2, Mir EO-22, STS-81, Mir NASA-3.

    After a night launch of Space Shuttle Atlantis, the Shuttle docked with Mir at 03:55 GMT on January 14. STS-81 transferred 2,715 kg of equipment to and from the Mir, the largest transfer of items to that date. During the docked phase, 640 kg of water, 515 kg of U.S. science equipment, 1,000 kg of Russian logistics, and 120 kg of miscellaneous material were transferred to Mir. Returned to Earth aboard Atlantis were 570 kg of U.S. science material, 405 kg of Russian logistics and 98 kg of miscellaneous material. At 02:16 GMT January 19, Atlantis separated from Mir after picking up John Blaha, who had arrived aboard STS-79 on September 19, 1996, and dropping off Jerry Linenger, who was to stay aboard Mir for over four months. The Shuttle backed off along the -RBAR (i.e. toward the Earth) to a distance of 140 m before beginning a flyaround at 02:31 GMT. Most of the flyaround was at a distance from Mir of 170 m. The first 'orbit' around Mir was complete at 03:15, and the second was completed at 04:02 GMT. Then the Orbiter fired its jets to drift away from the orbit of Mir. NASA's first Shuttle mission of 1997 came to a close with a landing at the Kennedy Space Center at 14:22 GMT on January 22 (after the first opportunity was waved off due to cloud cover at the Cape).

  • Spacehab Double Module Nation: USA. Program: Mir. Class: Manned. Type: Spacelab. Spacecraft: Spacehab. Agency: NASA. COSPAR: 1997-001xx. USAF Sat Cat: 24711. Decay Date: 1997-01-22.

  • External Airlock/ODS Nation: USA. Program: Mir. Payload: EAL/ODS. Agency: NASA. COSPAR: 1997-001xx. USAF Sat Cat: 24711. Decay Date: 1997-01-22.

2005 - 18:47 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: SLC17B. Launch Vehicle: Delta. Model: Delta 7925-9.5. LV Configuration: Delta 7925-9.5 D311.
  • Deep Impact Nation: USA. Program: Discovery. Payload: Discovery 7. Mass: 601 kg (1,324 lb). Class: Planetary. Type: Comet. Spacecraft: Deep Impact. COSPAR: 2005-001A. USAF Sat Cat: 28517.

    Launched into a 0.981 AU x 1.628 AU solar orbit inclined 0.6 deg to the ecliptic. Deep Impact was to fly by Comet 9P/Tempel-1 on 3 July 2005. An impacter it released was to hit the comet on 4 July at 10.2 km/s, producing a crater and ejecta plume that would allow the flyby spacecraft to determine the composition and structure of the comet's nucleus.


Born on this day in:
  • 1942 - Vladimir Sergeyevich Kozelsky.  Russian Pilot Cosmonaut. Birth City: Aleksandrovskoye. Birth State: Stavropol Kray. Birth Country: Russia.
  • 1954 - Sergey Ivanovich Moshchenko.  Russian Engineer Cosmonaut. Birth City: Krekshino state farm. Birth State: Moscow. Birth Country: Russia.
  • 1966 - Sergey Nikolayevich Revin.  Russian Engineer Cosmonaut. Birth City: Moscow. Birth State: Moscow. Birth Country: Russia.

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