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1939 - Launch Vehicle: JATO.

  • JATO project funded. Nation: USA.

    National Academy of Sciences sponsored a $10,000 research program at Cal Tech Rocket Research Project for development of rockets suitable to assist Air Corps planes in takeoffs, the first U.S. rocket program.

1940 -
  • Rocket ordnance research begun. Nation: USA.

    National Defense Research Committee established Jet Propulsion Research Committee under Section H of Division A, at Naval Powder Factory, Indian Head, Md., to conduct fundamental research on rocket ordnance. C. N. Hickman, who had worked with Goddard during World War I, was named as head.

1945 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -.
  • First launch from Wallops Island. Nation: USA.

    First launching of a two-stage rocket-propelled research model, the Tiamat missile, which employed six rockets as boosters, had automatic stabilization, its maneuvers were programed, and its testing was the first research program of the NACA's Wallops Island Station.

1946 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: FFAR.
  • RM-5 Model test flight Nation: USA. Agency: NACA. Apogee: 5.00 km (3.10 mi).

1947 - Launch Vehicle: Atlas.
  • MX-774 cancelled. Nation: USA.

    Contract with Convair for the MX-774 "Upper Air Test Vehicle," predecessor of the Atlas ICBM, was cancelled by the AAF. However the service approves Convair use of unexpended MX-774 funds to launch the MX-774 test vehicles already built. The decision made to move Vultee operations to San Diego.

1953 -
  • Ministry of Medium Machine Building formed. Nation: USSR.

    Council of Soviet Ministers (SM) Decree 'On unification of the First and Third Chief Directorates of Council of Ministers into the new Ministry of Medium Machine Building' was issued.

1953 - 17:52 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 39.
  • AF / Utah Ionosphere 4 Ionosphere mission Nation: USA. Agency: ARDC. Apogee: 138 km (85 mi).

    Ionosphere research. Launched at 1052 local time. Reached 138.4 km.

1954 - Launch Site: Edwards. Launch Complex: -. Launch Pad: -. Launch Vehicle: Navaho. Model: Navaho X-10. LV Configuration: X-10 s/n 2 GM-19308.
  • Navaho X-10 flight 7 Nation: USA. Program: Navaho.

    Vehicle crashed and burned after 8 minutes of flight when a fire developed aboard.

1954 - Launch Vehicle: Atlas. Model: Atlas A.
  • Western Development Division (WDD) established by USAF Nation: USA.

    Western Development Division (WDD) established by AF under ARDC to manage Atlas development; Rocketdyne put on contract for propulsion system

1954 - Launch Vehicle: Atlas. Model: Atlas A.
  • Rocketdyne put on contract for Atlas engines. Nation: USA.

    Western Development Division (WDD) established by AF under ARDC to manage Atlas development;

1955 - Launch Vehicle: Jupiter.
  • Jupiter IRBM proposed. Nation: USA.

    Huntsville proposes Jupiter 1500 miles range/2500 lb payload. AF proposes Thor. Both authorized. Jupiter also ship-launch capable.

1955 - Launch Vehicle: Rockoon.
  • Rockoon launches. Nation: USA.

    Instrumented Loki I and Deacon rockets were successfully balloon launched (Rockoons) from shipboard off the coast of Greenland in cosmic-ray studies by State University of Iowa research group. Army Ordnance supplied JPL-developed Loki rockets and ONR sponsored the project.

1955 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-11. Model: R-11FM.
  • Test mission Nation: USSR. Agency: NII-88. Apogee: 150 km (90 mi).

1955 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-2. Model: R-2.
  • Test mission Nation: USSR. Agency: NII-88. Apogee: 150 km (90 mi).

1955 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-11. Model: R-11FM.
  • Test mission Nation: USSR. Agency: NII-88. Apogee: 150 km (90 mi).

1955 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-11. Model: R-11FM.
  • Test mission Nation: USSR. Agency: NII-88. Apogee: 150 km (90 mi).

1955 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M.
  • State trials missile 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. LV Configuration: R-5M M-5RD.
  • R-7 component test Nation: USSR. Agency: MVS. Apogee: 500 km (310 mi).

1957 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D.
  • First Atlas wing activated at Cooke AFB. Nation: USA.

    Air Research and Development Command activated the 704th Strategic Missile Wing (Atlas) at Cooke AFB.

1957 - Launch Vehicle: Aerobee.
  • Aerobee completes 165th flight. Nation: USA.

    Aerobee upper air research rocket developed by the Applied Physics Laboratory of Johns Hopkins, and first fired on September 25, 1947, completed 165 successful firings to date.

1958 -
  • Korolev letter to Politburo Nation: USSR. Program: Vostok. Class: Manned. Type: Spacecraft. Spacecraft: Vostok.

    First explanation to leadership of advantages of manned spaceflight.

1958 - Launch Vehicle: Kappa.
  • Kappa-6tw rocket reaches 30 miles. Nation: Japan.

    Japanese Kappa-6tw two-stage rocket flown to 30-mile altitude over Michikawa Rocket Center, Japan.

1958 - Launch Site: San Clemente. Launch Complex: -. Launch Pad: -. Launch Vehicle: X-17. LV Configuration: X-17 Winder 2. FAILURE: Failure.
  • Argus test Nation: USA. Agency: USN. Apogee: 10 km (6 mi).

1958 - Launch Site: San Clemente. Launch Complex: -. Launch Pad: -. Launch Vehicle: X-17. LV Configuration: X-17 Winder 3. FAILURE: Failure.
  • Argus test Nation: USA. Agency: USN. Apogee: 0 km ( mi).

1959 -
  • Mercury astronaut MASTIF training. Nation: USA. Program: Mercury.

    Project Mercury astronauts completed disorientation flights on three-axis space-flight simulator, the MASTIF (Multiple Axis Space Test Inertia Facility), at NASA Lewis Research Center.

1959 - Launch Vehicle: Saturn C-3, Saturn I, Saturn V.
  • Kiwi-A first experimental nuclear rocket tested. Nation: USA. Program: NERVA.

    The first experimental reactor (Kiwi-A) in the nuclear space rocket program operated successfully at full temperature and duration at Jackass Flats, Nev.

1959 - Launch Vehicle: Jupiter.
  • Jupiter launch vehicles in Project Mercury canceled Nation: USA. Program: Mercury. Spacecraft: Mercury.

    The order for Jupiter launch vehicles in support of Project Mercury was canceled because the same or better data could be obtained from Atlas flights.

1960 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
  • Major expansion of Pacific Missile Range Nation: USA.

    Major expansion of Pacific Missile Range with acquisition of Eniwetok and Kwajalein Atolls in the Marshall Islands by the United States Navy for instrumentation complexes (in support of Air Force launches from Vandenberg AFB).

1960 - 14:35 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 AA3.107.
  • Meteorites mission Nation: USA. Agency: USAF. Apogee: 162 km (100 mi).

1960 - 17:29 GMT - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I J-2. FAILURE: Destroyed 90 m above pad.
  • Mk 4 re-entry vehicle test Nation: USA. Agency: USAF. Apogee: 1.00 km (0.60 mi).

    Titan 1 J (Mk 4 RV)

1962 -
  • Kennedy Space Center founded. Nation: USA.

1962 - Launch Site: Fort Wingate. Launch Complex: -. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 1017.
  • Nation: USA. Agency: USA. Apogee: 90 km (55 mi).

    Successful missile test. Missed aimpoint by 390 m.

1963 -
  • Vostok 5/6 international press conference Nation: USSR. Spacecraft: Vostok. Flight: Vostok 6, Vostok 5.

    Big international press conference with the cosmonauts, beginning at 13:00. The session goes 1 hour and 45 minutes and all answers given by the cosmonauts are acceptable. After this conference they disappear from public view for seven days of medical examinations and monitoring.

1963 - Launch Site: White Sands. Launch Complex: LC38. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Test mission Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1963 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9a Sandia 152-3.
  • Nitehawk-9 test Nation: USA. Agency: Sandia. Apogee: 250 km (150 mi).

1963 - Launch Site: Cape Canaveral. Launch Complex: LC32B. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 431.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -.
  • Point Arguello transferred to Air Force Nation: USA.

    Point Arguello (nearly 20,000 acres) transferred from the Navy to the Air Force and annexed to Vandenberg AFB.

1964 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U.
  • Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1964 - 11:16 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 T15000-04.
  • Cosmos 34 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: NII-88. Perigee: 201 km (124 mi). Apogee: 342 km (212 mi). Inclination: 64.90 deg. Period: 89.90 min. COSPAR: 1964-034A. USAF Sat Cat: 822. Duration: 8.00 days. Decay Date: 1964-07-09.

    High resolution photo reconnaissance satellite; returned film capsule

1965 -
  • Apollo Site Selection Board Nation: USA. Program: Apollo.

    Within its Office of Manned Space Flight, NASA organized an Apollo Site Selection Board. As an advisory body to the Associate Administrator for Manned Space Flight, George E. Mueller, the group would recommend landing sites for Apollo.

1965 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Interceptor mission Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1965 - Launch Site: Barbados. Launch Complex: HARP. Launch Pad: -. Launch Vehicle: Martlet. Model: Martlet 2.
  • Ionosphere mission Nation: Canada. Agency: HARP. Apogee: 150 km (90 mi).

1965 - 01:45 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL106.
  • Solar X-rays / Ionosphere Ionosphere / solar x-rays mission Nation: Australia. Agency: WRE/RAE. Apogee: 130 km (80 mi).

1965 - 09:54 GMT - Launch Site: Vandenberg. Launch Complex: 576B1. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 59D.
  • NTMP KX-32 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 -
  • Three additional backup Apollo missions studied Nation: USA. Program: Apollo. Flight: Apollo 8.

    Director of Flight Operations Christopher C. Kraft, Jr., said that MSC had been directed by NASA OMSF to outline technical problems and both cost and schedule impact of adding three backup Apollo missions to the planned flight schedule. The missions to be evaluated would be AS-207/208 or AS-206/207; AS-503D; and AS-503F. Each of these missions would provide alternate means of obtaining primary program objectives in the event of flight contingencies during tests or of major schedule adjustments. - Additional details.

1966 - Launch Site: Kapustin Yar. Launch Complex: PL87. Launch Pad: -. Launch Vehicle: RT-2.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1966 - 16:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta E1. LV Configuration: Thor Delta E1 467/D39.
  • Explorer 33 Nation: USA. Program: Explorer. Payload: AIMP D. Mass: 93 kg (205 lb). Class: Earth. Type: Magnetosphere. Spacecraft: IMP. Agency: NASA GSF. Perigee: 265,679 km (165,084 mi). Apogee: 480,762 km (298,731 mi). Inclination: 24.10 deg. Period: 38,792.40 min. COSPAR: 1966-058A. USAF Sat Cat: 2258.

    Intended to enter lunar orbit. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).

1966 - 19:02 GMT - Launch Site: Mud Lake DZ. Launch Complex: -. Launch Pad: 37.9 N x 117.1 W. Launch Vehicle: X-15. LV Configuration: X-15 2-45-81. FAILURE: Erroneous failure indication results in emergency landing at Mud Lake.
  • X-15A-2 External Tank test Nation: USA. Agency: NASA/USAF. Apogee: 13 km (8 mi).

    First flight with fueled external tanks. Engine shutdown at 34.6 seconds due to fuel flow anomalies. Maximum Speed - 1646 kph. Maximum Altitude - 13720 m.

1967 - Launch Vehicle: Tsiklon. Model: Tsyklon 2.
  • Tsiklon-2 launch vehicle authorised. Nation: USSR. Spacecraft: US-A, IS-A, Meteor.

    Council of Soviet Ministers (SM) Decree 'On use of the R-36-based launcher for the Kosmos and Meteor satellites' was issued.

1967 - 13:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3C. LV Configuration: Titan IIIC 3C-14.
  • IDCSP 3-1 Nation: USA. Payload: IDCSP 16. Mass: 45 kg (99 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,030 km (20,520 mi). Apogee: 33,515 km (20,825 mi). Inclination: 11.90 deg. Period: 1,309.60 min. COSPAR: 1967-066A. USAF Sat Cat: 2862.

    Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • IDCSP 3-2 Nation: USA. Payload: IDCSP 17. Mass: 45 kg (99 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,046 km (20,533 mi). Apogee: 33,517 km (20,826 mi). Inclination: 11.90 deg. Period: 1,310.00 min. COSPAR: 1967-066B. USAF Sat Cat: 2863.

    Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • IDCSP 3-3 Nation: USA. Payload: IDCSP 18. Mass: 45 kg (99 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,079 km (20,554 mi). Apogee: 33,547 km (20,845 mi). Inclination: 11.90 deg. Period: 1,311.60 min. COSPAR: 1967-066C. USAF Sat Cat: 2864.

    Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • IDCSP 3-4 Nation: USA. Payload: IDCSP 19/DATS. Mass: 68 kg (149 lb). Class: Communications. Type: Military. Spacecraft: IDCSP. Agency: USAF. Perigee: 33,145 km (20,595 mi). Apogee: 33,560 km (20,850 mi). Inclination: 11.90 deg. Period: 1,313.50 min. COSPAR: 1967-066D. USAF Sat Cat: 2865.

    Antenna tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • LES 5 Nation: USA. Mass: 194 kg (427 lb). Class: Technology. Type: Comsat. Spacecraft: LES. Agency: USAF. Perigee: 33,196 km (20,626 mi). Apogee: 33,609 km (20,883 mi). Inclination: 12.00 deg. Period: 1,316.00 min. COSPAR: 1967-066E. USAF Sat Cat: 2866.

    Experimental commsat. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • DODGE 1 Nation: USA. Mass: 102 kg (224 lb). Class: Technology. Type: Gravity gradient. Spacecraft: DODGE. Agency: USN NASC. Perigee: 33,257 km (20,664 mi). Apogee: 33,670 km (20,920 mi). Inclination: 12.00 deg. Period: 1,319.10 min. COSPAR: 1967-066F. USAF Sat Cat: 2867.

    Gravity gradient experiments. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

1969 -
  • Borman arrival in Russia delayed Nation: USSR.

    Borman was to arrive with his wife and two sons (ages 15 and 17). There is lots of high-level interest in the visit and meetings. They are unsure -- is Borman just a visiting astronaut or an official representative of the American aggressors? Borman's plane makes an emergency landing in Canada when an engine fails en route. His late arrival wrecks Kamanin's carefully-laid out schedule for his trip. Kamanin notes that in June 1968 the VVS suffered four times the accident rate as a year earlier. Two An-12's, one An-12 and an Il-14, and two Tu-22's were lost in three midair collisions, costing 131 lives.

1969 - Launch Site: Jiuquan. Launch Complex: -. Launch Pad: -. Launch Vehicle: T-7. Model: T-7A.
  • FSW satellite technology test Nation: China. Agency: CAST. Apogee: 100 km (60 mi).

1969 - 04:36 GMT - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1282.
  • FOT GT38B Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1969 - 18:15 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 141 km (87 mi).

1969 - 22:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.888.
  • Mass spectrometer Aeronomy mission Nation: USA. Agency: USAF. Apogee: 137 km (85 mi).

1970 - 17:02 GMT - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy/Ionosphere mission Nation: USSR. Apogee: 149 km (92 mi).

1971 -
  • Soyuz 11 capsule evaluated at landing site. Nation: USSR. Program: Salyut. Spacecraft: Soyuz 7KT-OK. Flight: Soyuz 11.

    At 05:00 specialists arrive from Moscow to the Soyuz 11 landing site to test the hermetic seal of the cabin. By 08:00 the pressure tests of the cabin show a slight loss, but it takes 1.5 hours for the cabin to fully depressurise. There are no cracks or holes in the cabin. Therefore the only cause could be the two air valves. The medical experts have already determined that the cosmonauts died from depressurisation of the spacecraft. The crew have haemorrhages in their brains, blood in their lungs, and nitrogen in their blood. The flight recorder shows that four seconds after the depressurisation began Dobrovolsky's breathing rate went to 48/minute (normally 16/minute), asphyxiation began, and 20 to 30 seconds later he was dead. By 19:30 Kamanin is in Moscow, and he sees the bodies laying in state at 21:40. They are cremated at 22:00.

1973 - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Temp-2S.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100N.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1973 - 10:15 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 50.0 N x 30.0 W. Launch Vehicle: MR-12. LV Configuration: MR-12 B-37.
  • Ionosphere mission Nation: USSR. Apogee: 175 km (108 mi).

1974 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100N.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1975 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: Pioner.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi).

1975 - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-11.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 - Launch Site: Baikonur. Launch Complex: LC177. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1976 -
  • Smithsonian National Air and Space Museum founded. Nation: USA.

1976 - Launch Site: Sea-launched. Launch Complex: -. Launch Pad: UNKPL. Launch Vehicle: R-27. Model: Zyb.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi).

1976 - 08:06 GMT - Launch Site: Plesetsk. Launch Complex: LC43/4. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. FAILURE: Fourth stage failure.
  • Cosmos 837 Nation: USSR. Program: Molniya. Payload: Molniya-2 s/n 27. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-2. Agency: MOM. Perigee: 438 km (272 mi). Apogee: 936 km (581 mi). Inclination: 62.80 deg. Period: 98.50 min. COSPAR: 1976-062A. USAF Sat Cat: 8927. Decay Date: 1983-11-18.

    Failed Molniya.

1977 - 11:52 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53749-162.
  • Cosmos 923 Nation: USSR. Program: Strela. Mass: 750 kg (1,650 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 781 km (485 mi). Apogee: 800 km (490 mi). Inclination: 74.00 deg. Period: 100.70 min. COSPAR: 1977-059A. USAF Sat Cat: 10120.

1979 - Launch Site: Biscarosse. Launch Complex: -. Launch Pad: -. Launch Vehicle: MSBS. Model: MSBS M20.
  • Operational test Nation: France. Agency: DMA. Apogee: 600 km (370 mi).

1980 - 07:12 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47182-416.
  • Cosmos 1190 Nation: USSR. Program: Strela. Mass: 750 kg (1,650 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 777 km (482 mi). Apogee: 792 km (492 mi). Inclination: 74.00 deg. Period: 100.60 min. COSPAR: 1980-056A. USAF Sat Cat: 11869.

1981 - 09:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1279 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-6U. Agency: MOM. Perigee: 206 km (128 mi). Apogee: 364 km (226 mi). Inclination: 70.40 deg. Period: 90.20 min. COSPAR: 1981-062A. USAF Sat Cat: 12571. Duration: 14.00 days. Decay Date: 1981-07-15.

    Photo surveillance; returned film capsule; maneuverable.

1983 - 12:17 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-SOL.
  • Prognoz 9 Nation: USSR. Payload: SO-M s/n 509. Mass: 1,060 kg (2,330 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Prognoz. Agency: MOM. Perigee: 380 km (230 mi). Apogee: 720,000 km (440,000 mi). Inclination: 1.30 deg. Period: 38,448.00 min. COSPAR: 1983-067A. USAF Sat Cat: 14163.

    Investigation of residual radiation from the Big Bang and gamma flares in deep space, and solar corpuscular and electromagnetic radiation plasma flows and magnetic fields in circumterrestrial space to determine the effects of solar activity on the interpl anetary medium and the earth's magnetosphere. In addition to Soviet scientific apparatus, carried instruments built in Czechoslovakia and France.

1987 - 19:35 GMT - Launch Site: Plesetsk. Launch Complex: LC32. Launch Pad: LC32/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-3.
  • Cosmos 1862 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 62. Mass: 1,600 kg (3,500 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MO SSSR. Perigee: 602 km (374 mi). Apogee: 636 km (395 mi). Inclination: 82.50 deg. Period: 97.10 min. COSPAR: 1987-055A. USAF Sat Cat: 18152.

1987 - 21:08 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A FALLING SPHERE.
  • MAC-SINE S-F12 Aeronomy mission Nation: USA. Agency: DLR. Apogee: 112 km (69 mi).

1987 - 23:05 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A FALLING SPHERE.
  • MAC-SINE S-F13 Aeronomy mission Nation: USA. Agency: DLR. Apogee: 113 km (70 mi).

1991 -
  • Warsaw Pact dissolved Nation: USSR.

1991 -
  • Responsibility for USAF astronauts transferred from Air Force District of Washington to HQ Air Force Space Command. Nation: USA.

1991 - Launch Site: Chiha-ri. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-17. Model: Hwasong 6.
  • Test mission Nation: Korea North. Agency: DPRK. Apogee: 200 km (120 mi).

1991 - 21:53 GMT - Launch Site: Baikonur. Launch Complex: LC200/39. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 373-01.
  • Gorizont 23 Nation: USSR. Payload: Gorizont s/n 34L. Mass: 2,125 kg (4,684 lb). Class: Communications. Spacecraft: Gorizont . Agency: MOM. Perigee: 36,158 km (22,467 mi). Apogee: 36,188 km (22,486 mi). Inclination: 6.80 deg. Period: 1,455.90 min. COSPAR: 1991-046A. USAF Sat Cat: 21533. Completed Operations Date: 1992-06-24.

    Stationed at 103 deg E. Maintenance of telephone and telegraph radio communications and transmission of television broadcasts. Positioned in geosynchronous orbit at 103 deg E in 1991-1992 As of 5 September 2001 located at 159.68 deg E drifting at 4.917 deg W per day. As of 2007 Mar 10 located at 0.82W drifting at 4.909W degrees per day.

1992 - Launch Site: Hama-Allepo. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-17. Model: Hwasong 6.
  • Test mission Nation: Syria. Agency: SYRIA. Apogee: 200 km (120 mi).

1992 - 02:20 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper 09PA.
  • Operational test Nation: USA. Agency: USAF ACC. Apogee: 1,000 km (600 mi).

1992 - 20:16 GMT - Launch Site: Plesetsk. Launch Complex: LC133/3. Launch Pad: LC133/3?. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65072-427.
  • Cosmos 2195 Nation: Russia. Mass: 825 kg (1,818 lb). Class: Navigation. Spacecraft: Parus. Agency: MO RF. Perigee: 956 km (594 mi). Apogee: 1,010 km (620 mi). Inclination: 82.90 deg. Period: 104.80 min. COSPAR: 1992-036A. USAF Sat Cat: 22006.

    Military navigation satellite. Positioned in plane 1 of constellation. Replaced Cosmos 2135. Failed after 12 months in orbit.

1993 -
  • Air Force Space Command assumed responsibility for intercontinental ballistic missile (ICBM) mission from Air Combat Command (ACC), and gained F.E. Warren AFB, Wyoming. Nation: USA.

1993 - 14:32 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2.
  • Soyuz TM-17 Nation: Russia. Program: Mir. Payload: Soyuz TM 11F732 s/n 66. Mass: 7,150 kg (15,760 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TM. Agency: MOM. Perigee: 388 km (241 mi). Apogee: 397 km (246 mi). Inclination: 51.60 deg. Period: 92.40 min. COSPAR: 1993-043A. USAF Sat Cat: 22704. Duration: 196.74 days. Decay Date: 1994-02-14. Crew: Haignere, Serebrov, Tsibliyev. Flight: Mir EO-14, Mir Altair, Mir EO-13.

    Mir Expedition EO-14. Carried Vasili Tsibliyev, Alexander Serebrov, Jean-Pierre Haignere to Mir; returned Serebrov, Tsibliyev to Earth. Progress M-18 undocked from Mir's front port at around 17:25 GMT on July 3, and Soyuz TM-17 docked at the same port only 20 minutes later at 17:45 GMT.

1993 -
  • Landing of STS-57 Nation: USA. Flight: STS-57.

    STS-57 landed at 12:51 GMT.

1994 -
  • Air Force Space Command gained Malmstrom AFB, Montana. Nation: USA.

1994 - 12:24 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U2.
  • Soyuz TM-19 Nation: Russia. Program: Mir. Payload: Soyuz TM 11F732 s/n 68. Mass: 7,150 kg (15,760 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TM. Agency: MOM. Perigee: 396 km (246 mi). Apogee: 397 km (246 mi). Inclination: 51.60 deg. Period: 92.49 min. COSPAR: 1994-036A. USAF Sat Cat: 23139. Duration: 125.95 days. Decay Date: 1994-11-04. Crew: Malenchenko, Musabayev. Flight: Mir EO-16, Mir EO-15, Mir LD-4.

    Mir Expedition EO-16. Soyuz TM-19 docked at the rear port of the Kvant module (vacated by Progress M-23 on July 2) at 13:55:01 GMT on July 3.

1995 - Launch Site: Taiyuan. Launch Complex: -. Launch Pad: -. Launch Vehicle: DF-21.
  • Test mission Nation: China. Agency: PRC. Apogee: 500 km (310 mi).

1997 - 18:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-94.
  • STS-94 Nation: USA. Program: STS. Payload: Columbia F23 / Spacelab LM Unit 1 / EDO. Class: Manned. Type: Spaceplane. Spacecraft: Columbia. Manufacturer: Daimler-Benz Aerospace, Bremen (formerly ERNO). Agency: NASA JSC. Perigee: 296 km (183 mi). Apogee: 300 km (180 mi). Inclination: 28.50 deg. Period: 90.50 min. COSPAR: 1997-032A. USAF Sat Cat: 24849. Duration: 15.70 days. Decay Date: 1997-07-17. Crew: Halsell, Kilrain, Voss Janice, Gernhardt, Thomas, Crouch, Linteris. Flight: STS-94.

    STS-94 was the reflight, with the same equipment and crew, of the curtailed STS-83 mission. Cargo Bay Payloads:

    • MSL-1: The Microgravity Science Laboratory included the first test of the International Space Station’s EXPRESS Rack. MSL-1 also contained numerous other experiment payloads to test materials and combustion processes in zero gravity.
    • CRYOFD: The Cryogenic Flexible Diode (CRYOFD) heat pipe was a Hitchhiker payload.
    • OARE: The Orbital Acceleration Research Experiment was a self-calibrating instrument that monitored extremely small accelerations and vibrations experienced during orbit of the Shuttle.
    In-Cabin Payloads: SAREX, MSX

    The mission this time went for its full two week duration and the crew completed the full list of experiments. The deorbit burn was on July 17, 1997 at 09:44 GMT and Columbia landed on KSC's Runway 33 at 10:46:34 GMT.

  • Spacelab MSL-1R Nation: USA. Program: Spacelab. Payload: Spacelab Long Module. Class: Manned. Type: Spacelab. Spacecraft: Spacelab. Manufacturer: Daimler-Benz Aerospace, Bremen (formerly ERNO). Agency: NASA JSC. Perigee: 296 km (183 mi). Apogee: 300 km (180 mi). Inclination: 28.50 deg. Period: 90.50 min. COSPAR: 1997-032xx. USAF Sat Cat: 24849. Decay Date: 1997-07-17.

    Remained attached to OV-102

  • EDO Nation: USA. Program: STS. Agency: NASA. COSPAR: 1997-032xx. USAF Sat Cat: 24849. Decay Date: 1997-07-17.

1998 - 00:48 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
  • Molniya-3-49 Nation: Russia. Program: Molniya. Payload: Molniya-3 s/n 61. Class: Communications. Spacecraft: Molniya-3. Manufacturer: NPO Prikladnoi Mekhaniki, Zhelenogorsk. Agency: MOM. Perigee: 501 km (311 mi). Apogee: 39,850 km (24,760 mi). Inclination: 62.80 deg. Period: 717.70 min. COSPAR: 1998-040A. USAF Sat Cat: 25379.

1999 - 1999 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Malemute. LV Configuration: Malemute TMBD Target.
  • Malemute II Slugger Target mission Nation: USA. Agency: USN. Apogee: 120 km (70 mi).

2000 - Launch Site: Barking Sands. Launch Complex: POA. Launch Pad: -. Launch Vehicle: Standard-ER. Model: Standard SM-3. LV Configuration: SM-3 FTR-1. FAILURE: Failure.
  • Aegis LEPI test Nation: USA. Agency: USN. Apogee: 100 km (60 mi).

2002 - 23:56 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Orion. LV Configuration: Terrier Orion NASA 41.032GE.
  • MM-MW-08 MacWAVE Plasma mission Nation: USA. Agency: NASA GSFC. Apogee: 130 km (80 mi).

2003 -
  • 2060 Chiron Closest Approach To Earth (11.183 AU)

2006 - 06:39 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Improved Orion. LV Configuration: Terrier Improved Orion NASA 41.056UO.
  • ESPRIT (SPIRIT 3) Ionosphere / plasma mission Nation: Norway. Agency: NASA GSFC. Apogee: 200 km (120 mi).


Born on this day in:
  • 1908 - Cai Jintao.  Chinese Engineer. Birth City: Nantong. Birth State: Jiangsu. Birth Country: China.
  • 1930 - Frank Marshall.  American Engineer. Birth City: Johnstown. Birth State: Pennsylvania. Birth Country: USA.
  • 1961 - Dr Kalpana Chawla.  American Mission Specialist Astronaut. Birth City: Karnal. Birth Country: India.
  • 1963 - Dr Edward Tsang Lu.  American Mission Specialist Astronaut. Birth City: Springfield. Birth State: Massachusetts. Birth Country: USA.

Died on this day in:
  • 1977 - Oskar Morgenstern.  German American Manager.
  • 1986 - Melvin Sherman Day.  American Manager.
  • 1987 - Charles Stark Draper.  American Engineer.
  • 1990 - Ivan Aleksandrovich Serov.  Russian Government Official.
  • 1993 - Werner Voss.  German Engineer.

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