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1947 -

  • XS-1 Flight 27 Nation: USA. Payload: XS-1 # 1 flight 11. Class: Manned. Type: Rocketplane. Spacecraft: XS-1. Crew: Goodlin.

    Bell flight 11. Glide flight and stall check. At Muroc Dry Lake, California.

1952 - Launch Site: Cape Canaveral. Launch Complex: LA. Launch Pad: -. Launch Vehicle: Lark. LV Configuration: Lark 602. FAILURE: Failure.
  • Test mission Nation: USA. Agency: USAF. Apogee: 0 km ( mi).

1953 -
  • X-1A Flight 5 Nation: USA. Payload: X-1A flight 5. Class: Manned. Type: Rocketplane. Spacecraft: X-1A. Crew: Ziegler.

    Bell flight 5. Pilot noted low-frequency elevator buzz at mach 0.93, did not proceed above this speed, pending buzz investigation.

1954 - Launch Vehicle: R-5. Model: R-5M.
  • OKB-586 founded and nuclear-tipped R-5M IRBM development authorised. Nation: USSR.

    Council of Soviet Ministers (SM) Decree 'On approval of work on the R-5M missile and on establishment of OKB-586 at Dnepropetrovsk Plant No. 586' was issued. Sadoviy and Kozlov were named to lead the project. Based substantially on the R-5, it used the 8U25 launch portable launch stand.

1959 -
  • Mercury escape-motor canting-angle tests completed at Wallops Island. Nation: USA. Program: Mercury. Spacecraft: Mercury.

    Escape-motor canting-angle tests were completed at Wallops Island. Tests were conducted in 5 degree increments between 10 degrees to 30 degrees, and visually it appeared stability was better at the larger angle.

1963 -
  • Link to build Apollo lunar mission simulators Nation: USA. Program: Apollo. Spacecraft: Apollo CSM.

    North American awarded a $9.5 million letter contract to the Link Division of General Precision, Inc., for the development and installation of two spacecraft simulators, one at MSC and the other at the Launch Operations Center. Except for weightlessness, the trainers would simulate the entire lunar mission, including sound and lighting effects.

1963 - 20:33 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-14. FAILURE: Failure.
  • Test mission Nation: USA. Agency: USN. Apogee: 0 km ( mi).

1964 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: RAM. Model: RAM B. LV Configuration: RAM B RAM B-3.
  • RAM B-3 re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).

1964 - 06:30 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.121GE.
  • Auroral emissions Aurora mission Nation: USA. Agency: NASA. Apogee: 172 km (106 mi).

1965 - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78. LV Configuration: Molniya 8K78 R103-26. FAILURE: Stage 3's engine 8D715K failed due to depressurization of the nitrogen pipeline of the LOX tank pressurization system of Block I.
  • Luna failure - stage 3 engine failure. Nation: USSR. Program: Luna. Payload: E-6 s/n 8. Class: Planetary. Type: Lunar. Spacecraft: Luna E-6. Agency: RVSN. COSPAR: F650410A. Decay Date: 1965-04-10.

    The upper stages fell apart on re-entry into the atmosphere..

1965 - 08:10 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1150.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1966 - Launch Vehicle: Proton. Model: Proton 8K82K. LV Configuration: Proton 8K82K.
  • Cosmonaut training for lunar flights announced Nation: USSR. Program: Lunar L1. Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-L1.

    Leonov announces that cosmonauts are in training for lunar missions.

1967 - 10:51 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL118.
  • X-ray survey / airglow X-ray astronomy mission Nation: Australia. Agency: WRE/RAE. Apogee: 167 km (103 mi).

1967 - 20:14 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.331IE.
  • DLR K-NA-4 Aurora / barium release mission Nation: USA. Agency: NASA. Apogee: 230 km (140 mi).

1967 - 21:00 GMT - Launch Site: Point Barrow. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.227GM.
  • Grenade Aeronomy mission Nation: USA. Agency: NASA. Apogee: 120 km (70 mi).

1968 -
  • Cosmonauts occupied with Gagarin crash investigation Nation: USSR. Program: Soyuz.

    No cosmonauts will be sent to witness the next series of unmanned Soyuz flights beginning on 14 April. All cosmonaut staff efforts are concentrated on the Gagarin crash investigation. Kamanin notes the flight of Apollo 6. According to his information the first manned Apollo flight will take place in May-October 1968, and the first American moon landing by the end of 1969.

1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1411.
  • ST Olympic T. B-2 operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1970 -
  • Documentary film on the Soyuz 6-7-8 missions Nation: USSR. Program: Soyuz. Flight: Soyuz 6, Soyuz 7, Soyuz 8.

    Kamanin previews the documentary film 'Launch after Launch' on the Soyuz 6-7-8 missions.

1970 - 16:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3E. FAILURE: Failure.
  • Operational test Nation: USA. Agency: USN. Apogee: 10 km (6 mi).

1971 -
  • Old Comrades toast Gagarin's memory. Nation: USSR.

    -6 deg C at Baiknur, 5 m/s wind. A party of the 'old comrades' is held in Leninsk to commemorate the tenth anniversary of Gagarin's launch.

1973 - 06:59 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.91DG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 198 km (123 mi).

1974 - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3D. LV Configuration: Titan IIID 23D-9.
  • KH-9 no. 08 Capsule Nation: USA. Payload: P 73-7. Mass: 60 kg (132 lb). Class: Surveillance. Type: Military. Spacecraft: KH-9. Agency: U.S. Air Force. Perigee: 786 km (488 mi). Apogee: 830 km (510 mi). Inclination: 94.60 deg. Period: 101.10 min. COSPAR: 1974-020xx. USAF Sat Cat: 7244.

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

  • KH-9 no. 08 Nation: USA. Mass: 13,300 kg (29,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-9. Agency: NRO/CIA. Perigee: 153 km (95 mi). Apogee: 285 km (177 mi). Inclination: 94.50 deg. Period: 88.90 min. COSPAR: 1974-020A. USAF Sat Cat: 7242. Decay Date: 1974-07-28.

    KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

  • OPS 4547 Nation: USA. Payload: SSF-B No. 25. Mass: 60 kg (132 lb). Class: Sigint. Spacecraft: SSF. Agency: NRO/USAF. Perigee: 503 km (312 mi). Apogee: 531 km (329 mi). Inclination: 94.00 deg. Period: 95.00 min. COSPAR: 1974-020C. USAF Sat Cat: 7247. Decay Date: 1980-02-22.

    Radar monitoring.

  • S73-7 Cal Balloon Nation: USA. Spacecraft: S73-7 Cal Balloon. Agency: USAF AFSC. COSPAR: 1974-020xx. USAF Sat Cat: 7242. Decay Date: 1974-07-28.

1975 - 04:40 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170A. LV Configuration: Aerobee 170A NASA 13.88GG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 176 km (109 mi).

1975 - 09:54 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.302-3.
  • AEOLUS Release, Sphere Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 216 km (134 mi).

1975 - 09:54 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.302-4.
  • AEOLUS Release Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 219 km (136 mi).

1975 - 10:00 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.403-3.
  • AEOLUS Mass Spectrometer Aeronomy mission Nation: USA. Agency: USAF CRL. Apogee: 211 km (131 mi).

1979 -
  • Ferry flight, MSFC to KSC Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise.

    Ferry flight, shuttle carrier aircraft/Enterprise (OV-101) from MSFC to KSC (1 hour, 52 minutes)

1979 - Launch Vehicle: Shuttle.
  • Shuttle Enterprise delivered to Kennedy Space Centre Nation: USA.

    The decision was taken not to convert the Enterprise to a flight orbiter due to the numerous structural design changes made since its construction. Static test article OV-099 would be used for that instead. So Enterprise became a pathfinder vehicle at Cape Canaveral to verify fit and handling of ground facilities in the Vertical Assembly Building and LC39.

1979 - 17:34 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Soyuz 33 Nation: USSR. Program: Salyut 6. Payload: Soyuz 7K-T s/n 49. Mass: 6,860 kg (15,120 lb). Class: Manned. Type: Spacecraft. Spacecraft: Soyuz 7K-T. Agency: MOM. Perigee: 194 km (120 mi). Apogee: 261 km (162 mi). Inclination: 51.60 deg. Period: 89.00 min. COSPAR: 1979-029A. USAF Sat Cat: 11324. Duration: 1.96 days. Decay Date: 1979-04-12. Crew: Ivanov Georgi, Rukavishnikov. Flight: Salyut 6 EP-5-1, Salyut 6 EO-3.

    Manned two crew. Flight under the Intercosmos programme of an international team consisting of N N Rukavishnikov (USSR) and G I Ivanov (Bulgaria). Unsuccessful mission. Failed to rendezvous with Salyut 6.

1980 - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B.
  • ABRES STREP-4 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1982 - 06:47 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 3910/PAM. LV Configuration: Delta 3910/PAM 647/D161.
  • Insat 1A Nation: India. Program: Insat. Mass: 1,152 kg (2,539 lb). Class: Communications. Spacecraft: Insat 1. Agency: ISRO. Perigee: 35,734 km (22,204 mi). Apogee: 35,829 km (22,263 mi). Inclination: 13.30 deg. Period: 1,435.80 min. COSPAR: 1982-031A. USAF Sat Cat: 13129. Completed Operations Date: 1982-09-04.

    Also carried transponders for domestic communications. Operational multipurpose satellite for telecommunications, meteorological, imaging and data relay, radio and television programme distribution and direct television broadcasting for community reception. Geosynchronous orbit longitude 74 E. A/AC.105/INF.391 was reissued as ST/SG/SER.E/79. Also registered by the United States as 1982-31A in ST/SG/SER.E/67, with category C and orbital parameters 1416.7 min, 35032 x 35783 km x 0.5 deg. Positioned in geosynchronous orbit at 73 deg E in 1982 As of 29 August 2001 located at 82.99 deg E drifting at 0.337 deg W per day. As of 2007 Mar 10 located at 39.55E drifting at 0.205W degrees per day.

1983 - 07:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 10. LV Configuration: Black Brant X NASA 35.005UG.
  • Astronomy mission Nation: USA. Agency: NASA. Apogee: 667 km (414 mi).

1984 - 14:00 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1548 Nation: USSR. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-4K1. Agency: MOM. Perigee: 165 km (102 mi). Apogee: 331 km (205 mi). Inclination: 67.20 deg. Period: 89.50 min. COSPAR: 1984-036A. USAF Sat Cat: 14902. Duration: 45.00 days. Decay Date: 1984-05-25.

    High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission.

1989 - 08:21 GMT - Launch Site: Kiruna. Launch Complex: MRL. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX MASER 3.
  • MASER 3 Microgravity mission Nation: Sweden. Agency: SSC. Apogee: 297 km (184 mi).

1992 - 03:20 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925 D208.
  • USA 80 Nation: USA. Program: Navstar. Payload: GPS 2A-13 / GPS SVN 28. Mass: 1,816 kg (4,003 lb). Class: Navigation. Spacecraft: GPS Block 2 and 2A. Manufacturer: Boeing North American, Seal Beach (formerly Rockwell). Agency: USAF. Perigee: 20,082 km (12,478 mi). Apogee: 20,277 km (12,599 mi). Inclination: 54.50 deg. Period: 717.90 min. COSPAR: 1992-019A. USAF Sat Cat: 21930.

    Global Positioning System. Retired 15 August 1997.

1992 - 06:30 GMT - Launch Site: Zingst. Launch Complex: -. Launch Pad: -. Launch Vehicle: MMR-06.
  • MMR06-M Zingst launch 62 Nation: Russia. Agency: GMS?. Apogee: 67 km (41 mi).

    Successful. Earth impacted at 4054 seconds. Reached 66.7 km.

2002 -
  • Yuji Hyakutake Dies At 51 Nation: Japan.


Born on this day in:
  • 1919 - John C Houbolt.  American Engineer. Birth City: Altoona. Birth State: Iowa. Birth Country: USA.
  • 1945 - Eric Edward Sundberg.  American Manned Spaceflight Engineer Astronaut. Birth City: Tonopah. Birth State: Nevada. Birth Country: USA.

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