March 24

See also Born on this Day
On this day in:

1939 -

  • Goddard Series P Section B rocket tests Nation: USA.

    Series P section B was a series of tests by Goddard in development of a gas generator to run turbines. Through April 28 a series of eleven static tests (Pa-k) of a new gas generator was made near the shop. The best form developed ran steadily for 10 sec at 180 psi for 250-psi tank pressures, with the rate of flow of oxygen at 0.49 lb/sec.

1946 - Launch Vehicle: Navaho X-10, Navaho G-26, Navaho G-38, Navaho SSM-A-2.
  • MX-770 strategic missile study contract awarded Nation: USA. Program: Navaho.

    North American received W33-038-ac-1491, a $500,000 letter contract, for study of the MX-770, an 800 km range, supersonic guided missile with a 900 kg nuclear warhead.

1950 - Launch Site: Wallops Island.
  • Ramjet test. Nation: USA.

    First successful ramjet research model flown at Wallops Island by NACA Langely's PARD.

1951 - Launch Vehicle: Buran.
  • Central Committee decree created the OKB-23 Myasishchev design bureau. Nation: USSR. Program: Navaho.

    Myasishchev was tasked with building an intercontinental jet-powered bomber, something veteran aircraft designer Tupolev said was impossible. Myasishchev managed to complete the first prototype 103M (called M-4 Bear in the West) bomber ten months after go-ahead. Myasishchev would later play a key role in Soviet spaceplane development.

1955 - Launch Site: Edwards. Launch Vehicle: Navaho X-10. LV Configuration: X-10 s/n 1 GM-19307.
  • Navaho X-10 flight 15 Nation: USA. Program: Navaho.

    Successful test of automated landing system, certifying the X-10 for operation from the Cape Canaveral skid strip.

1956 -
  • X-2 Flight 6 Nation: USA. Payload: X-2 # 1 flight 6. Class: Manned. Type: Rocketplane. Spacecraft: X-2 . Crew: Everest.

    Second powered flight, mach 0.91.

1958 - Launch Vehicle: Burya.
  • Further development of Burya authorised. Nation: USSR. Program: Navaho.

    State Committee for Defence Technology (GKOT) Decree 'On the Creation of the Burya Winged Missile--course of work on 40 Burya' was issued.

1958 - 18:30 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun OB6.08.
  • Nike-Cajun Aeronomy mission Nation: USA. Agency: USAF. Apogee: 119 km (73 mi).

1958 - 22:00 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AM6.38.
  • Nike-Cajun Aeronomy mission Nation: USA. Agency: USAF. Apogee: 137 km (85 mi).

1959 - Launch Site: Wallops Island.
  • 3,300th launch from Wallops. Nation: USA.

    NASA announced that Wallops Station had made over 3,300 rocket firings since 1945.

1960 - Launch Site: Wallops Island. Launch Vehicle: Sergeant 5-stage.
  • Sergeant 5-stage Mercury model test flight Nation: USA. Agency: NASA. Apogee: 34 km (21 mi).

1960 - 02:06 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Vehicle: R-7A.
  • R-7A I-5 Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1961 -
  • Mercury MR-3A (cancelled) Nation: USA. Program: Mercury. Payload: Mercury SC7. Spacecraft: Mercury. Location of Spacecraft: U.S. Naval Academy, College of Medicine, Anapolis, MD. Crew: Shepard. Flight: Mercury MR-3A.

    After booster problems on the Mercury MR-2 chimp test flight, Von Braun insisted on a further unmanned booster test flight, against the wishes of Shepard and others at NASA. A Mercury boilerplate capsule was launched on a flawless test on 24 March. If NASA had overruled Von Braun, the manned Freedom 7 capsule would have flown instead. Shepard would have been the first man in space (though not in orbit), beating Gagarin's flight by three weeks.

1961 -
  • Mercury MR-BD Nation: USA. Program: Mercury. Spacecraft: Mercury.

    After analyzing launch vehicle behavior in the Mercury-Redstone 1A (MR-1A) and Mercury-Redstone 2 (MR-2), officials at the Marshall Space Flight Center and the Space Task Group were of the opinion that there were a number of problems that needed to be corrected prior to the advent of manned flight. The problems to be resolved included jet-vane vibration, instrumentation compartment vibration, failure of the thrust-controller system, and several other areas that needed attention. Many of these problems were studied by the personnel of engineering activities and proposed solutions were formulated. It was felt, however, that flight was necessary to verify the corrections and the Mercury-Redstone Booster Development test was scheduled and flown. All test objectives were met; as a result of this test, the launch vehicle was man-rated for the planned suborbital flights.

1961 - 17:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC5. Launch Vehicle: Redstone. Model: Redstone Mercury. LV Configuration: Redstone MRLV-5.
  • Redstone Mercury MR-BD Nation: USA. Program: Mercury. Payload: Mercury Boilerplate. Class: Manned. Type: Spacecraft. Spacecraft: Mercury. Agency: NASA. Apogee: 181 km (112 mi).

    Suborbital test of Redstone modifications using a boilerplate Mercury capsule. The test was done at von Braun's insistence against Shepard's wishes, thereby putting the first US manned flight after Gagarin's.

1962 - 00:39 GMT - Launch Site: Vandenberg. Launch Complex: 576. Launch Pad: 576B2. Launch Vehicle: Atlas D. LV Configuration: Atlas D 134D.
  • Atlas D Demonstration and shakedown operations launch Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).

    President John F. Kennedy visited Vandenberg AFB and witnessed the launch of Atlas 134D.

1963 -
  • VVS Chief of Staff Malinovskiy says that manned flights should be cut back due to safety considerations. Nation: USSR.

    Kamanin considers this a strange attitude - many die every day in auto or aircraft accidents, but not one death will be tolerated in the conquest of space. The whole plan for the next Vostok missions are thrown back for reconsideration. Many meetings occur over the next week - the basic question, was the MO / RVSN / VVS interested in manned space flight or not? Finally the decision was made to continue - a 180 degree reversal from the original position.

1963 - 00:29 GMT - Launch Site: Vandenberg. Launch Complex: 576. Launch Pad: 576E. Launch Vehicle: Atlas F. LV Configuration: Atlas F 52F. FAILURE: Failure.
  • Atlas F OT TALL TREE 4 operational test launch Nation: USA. Agency: USAF SAC. Apogee: 10 km (6 mi).

1964 - 01:42 GMT - Launch Site: Cape Canaveral. Launch Complex: LC15. Launch Pad: LC-15. Launch Vehicle: Titan 2. Model: Titan II. LV Configuration: Titan 2 s/n N-33 / 61-1868.
  • Titan 2 Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 - 04:23 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.118GE.
  • Nike Apache Auroral mission Nation: USA. Agency: NASA. Apogee: 188 km (116 mi).

1964 - 12:15 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17. Launch Pad: LC17B. Launch Vehicle: Thor DSV-2G. LV Configuration: Thor DSV-2G 240. FAILURE: Second stage fired, then shut down, repeating the sequence several times.
  • Thor DSV-2G ASSET 2 re-entry vehicle test flight Nation: USA. Payload: ASSET-ASV 2. Class: Manned. Type: Spaceplane. Spacecraft: Asset. Agency: USAF. Apogee: 55 km (34 mi).

    Suborbital test of small scale spaceplane model to test materials for the X-20 Dynasoar. Aero-thermodynamic structural test vehicle (ASV) for heat shield tests. Good first stage burn, but the second stage fired, then shut down, repeating the sequence several times. The spacecraft separated, and began to maneuver in a 60 degree bank to recover course, when the self-destruct package blew it apart. The debris impacted the Atlantic 800 km downrange near San Salvador Island.

1964 - 22:22 GMT - Launch Site: Point Arguello. Launch Complex: LC1-1. Launch Pad: LC1-1. Launch Vehicle: Thor Agena D. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 396 / Agena D 1175. FAILURE: Failure.
  • KH-4A 1003 Nation: USA. Payload: KH-4A s/n 1003. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: U.S. Air Force. COSPAR: F640324AA. Decay Date: 1964-03-24.

    KH-4A. Mission failed.

  • SRV 631 Nation: USA. Payload: SRV 1003-1. Spacecraft: KH-4A. Agency: USAF. COSPAR: F640324AB.

  • SRV 630 Nation: USA. Payload: SRV 1003-2. Spacecraft: KH-4A. Agency: USAF. COSPAR: F640324AC.

  • ORBIS 1 Nation: USA. Payload: ORBIS 1. Spacecraft: KH-4A. Agency: USAF. COSPAR: F640324AD.

1965 - 06:40 GMT - Launch Site: Fort Churchill. Launch Vehicle: Black Brant. Model: Black Brant II. LV Configuration: Black Brant II AA-2A-53.
  • Black Brant Aeronomy/Ionosphere/Fields mission Nation: Canada. Agency: NRCC. Apogee: 166 km (103 mi).

1965 - 16:34 GMT - Launch Complex: CVE-25 U. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.174GE.
  • Nike Apache Plasma mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

    Launched at 1965 Croatan MRF Expedition LP22 - - Latitude: 11.83 S - Longitude: 78.33 W.

1965 - 17:07 GMT - Launch Complex: CVE-25 U. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.180GI.
  • Nike Apache Ionosphere mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

    Launched at 1965 Croatan MRF Expedition LP23 - - Latitude: 11.40 S - Longitude: 78.42 W.

1966 - Launch Vehicle: Titan 2.
  • Gemini launch vehicle 9 was removed from storage and erected at complex 19. Nation: USA. Flight: Gemini 9.

    The vehicle was inspected and umbilicals connected by March 28. Power was applied March 29, and the Subsystems Reverification Test (SSRT) began March 30. SSRT concluded April 11. The Prespacecraft Mate Verification Combined Systems Test was completed April 12.

1966 - Launch Site: Baikonur. Launch Complex: LC41. Launch Pad: LC41/4. Launch Vehicle: R-16. Model: R-16U.
  • R-16 Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1966 - 13:30 GMT - Launch Site: Thumba. Launch Vehicle: Nike Apache.
  • Nike Apache ISRO 10.07 TERLS-39 Aeronomy mission Nation: India. Agency: ISRO. Apogee: 201 km (124 mi).

1966 - 15:31 GMT - Launch Site: Sonmiani. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.180IM.
  • Nike-Cajun Rehbar 11 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 135 km (83 mi).

1966 - 16:45 GMT - Launch Site: Thumba. Launch Vehicle: Centaure. LV Configuration: Centaure C101 TERLS-40.
  • Centaure ISRO 15.04 Aeronomy mission Nation: India. Agency: ISRO. Apogee: 163 km (101 mi).

1966 - 17:02 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Vehicle: Veronique 61. Model: Veronique 61M. LV Configuration: Veronique 61M VA80.
  • Veronique 61 Test mission Nation: France. Agency: CNES. Apogee: 209 km (129 mi).

    FU155 Technology mission.

1966 - 21:00 GMT - Launch Site: Thumba. Launch Vehicle: Centaure. LV Configuration: Centaure C102 TERLS-41.
  • Centaure ISRO 15.05 Aeronomy mission Nation: India. Agency: ISRO. Apogee: 159 km (98 mi).

1966 - 21:00 GMT - Launch Site: Baikonur. Launch Complex: LC81. Launch Pad: LC81/23. Launch Vehicle: Proton 8K82. Model: UR-500. LV Configuration: UR-500 211. FAILURE: Second stage malfunction.
  • N-4 s/n 3 Nation: USSR. Program: Proton. Payload: N-4. Mass: 8,300 kg (18,200 lb). Class: Astronomy. Spacecraft: N-4. Agency: RVSN. COSPAR: F660324A. Decay Date: 1966-03-24.

1967 - 05:55 GMT - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Vehicle: Veronique 61. Model: Veronique 61M. LV Configuration: Veronique 61M VA86.
  • Veronique 61 Ionosphere/Plasma mission Nation: France. Agency: FR. Apogee: 366 km (227 mi).

    FU156 Ionosphere + Biology mission.

1967 - 11:50 GMT - Launch Site: Baikonur. Launch Complex: LC41. Launch Pad: LC41/15. Launch Vehicle: Kosmos 11K65. Model: Kosmos 11K65.
  • Cosmos 151 Nation: USSR. Program: Strela. Mass: 875 kg (1,929 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2. Agency: MO SSSR. Perigee: 384 km (238 mi). Apogee: 399 km (247 mi). Inclination: 56.00 deg. Period: 92.40 min. COSPAR: 1967-027A. USAF Sat Cat: 2720. Decay Date: 1991-05-06.

    Possible test flight.

1968 - 12:45 GMT - Launch Site: Natal. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.270GM.
  • Nike-Cajun Aeronomy mission Nation: USA. Agency: NASA. Apogee: 120 km (70 mi).

1969 -
  • Apollo 10 would be a lunar orbit mission Nation: USA. Program: Apollo. Spacecraft: Apollo LM. Flight: Apollo 10, Apollo 9.

    NASA announced that Apollo 10, scheduled for launch May 18, would be a lunar orbit mission during which two astronauts would descend to within 15,240 meters of the moon's surface. - Additional details.

1969 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 791.
  • Minuteman 1 FOT GT33B Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1969 - 10:01 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12.
  • MR-12 Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 181 km (112 mi).

1969 - 10:10 GMT - Launch Site: Baikonur. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57.
  • Cosmos 274 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 206 km (128 mi). Apogee: 300 km (180 mi). Inclination: 65.00 deg. Period: 89.60 min. COSPAR: 1969-028A. USAF Sat Cat: 3833. Duration: 8.00 days. Decay Date: 1969-04-01.

    High resolution photo reconnaissance satellite; returned film capsule; also carried science package.

1970 -
  • Only nine of 16 cosmonaut-finalists cleared by the KGB and Communist Party Nation: USSR.

    Kamanin reports that only nine of 16 cosmonaut-candidates that completed the arduous selection process have been cleared by the KGB and Communist Party for actual acceptance for cosmonaut training. He feels this makes the whole time-consuming selection process a waste of time. The VVS is reluctant to submit officers as cosmonaut candidates, fearing that if they fail the vestibular table tests they will not only be rejected as cosmonauts, but be unable to return to flight duty with the Air Force. The result is a final selection of dullards, who are not intellectual, or literary, or sports enthusiasts, who are poor readers and not really interested in spaceflight or cosmonautics. The final decree has been issued reorganising TsUKOS as GUKOS.

1970 - 19:17 GMT - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3 C3XT-22.
  • Poseidon Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1970 - 22:00 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL802.
  • Skylark UK SL802 X-ray Astronomy mission Nation: UK. Agency: BAC. Apogee: 179 km (111 mi).

1971 -
  • Gagarin film Nation: USSR.

    Gagarin Centre management are away at various sites. Kamanin enjoys the television film on Gagarin, 'About my friend', broadcast from Leningrad.

1971 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3.
  • Polaris A3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3.
  • Polaris A3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3.
  • Polaris A3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3.
  • Polaris A3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3.
  • Polaris A3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3.
  • Polaris A3 Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 - 05:26 GMT - Launch Site: Fort Churchill. Launch Vehicle: Black Brant. Model: Black Brant VC. LV Configuration: Black Brant VC CRL A18.006-3.
  • Black Brant Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 366 km (227 mi).

1971 - 18:32 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S87/2.
  • Skylark ESRO S87/2 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 190 km (110 mi).

1971 - 21:05 GMT - Launch Site: Vandenberg. Launch Complex: SLC3. Launch Pad: SLC3W. Launch Vehicle: Thorad Agena D SLV-2H. Model: Thorad SLV-2H Agena D. LV Configuration: Thorad SLV-2H Agena D 538 / Agena D 1660.
  • KH-4B 1114 Nation: USA. Payload: KH-4B s/n 1114 / Agena D 1660. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4B. Agency: NRO/CIA. Perigee: 156 km (96 mi). Apogee: 245 km (152 mi). Inclination: 81.50 deg. Period: 88.40 min. COSPAR: 1971-022A. USAF Sat Cat: 5059. Decay Date: 1971-04-12.

    KH-4B. The overall image quality is good and comparable to the best of past missions. On-board program failed

1972 - 08:46 GMT - Launch Site: Vandenberg. Launch Complex: SLC10. Launch Pad: SLC10W. Launch Vehicle: Thor Burner. Model: Thor Burner 2A. LV Configuration: Thor Burner 2A 153.
  • DMSP-Block-5B F2 Nation: USA. Program: DMSP. Payload: DMSP 5528. Mass: 195 kg (429 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 5B. Agency: USAF. Perigee: 781 km (485 mi). Apogee: 858 km (533 mi). Inclination: 98.90 deg. Period: 101.30 min. COSPAR: 1972-018A. USAF Sat Cat: 5903.

    Defense Meteorological Satellite Program.

1972 - 09:44 GMT - Launch Site: Fort Churchill. Launch Vehicle: Black Brant. Model: Black Brant VB. LV Configuration: Black Brant VB AED-VB-28.
  • Black Brant Aeronomy/Ionosphere mission Nation: Canada. Agency: NRCC. Apogee: 193 km (119 mi).

1972 - 23:31 GMT - Launch Site: Salto di Quirra. Launch Vehicle: Skylark. Model: Skylark 2. LV Configuration: Skylark 2 S75/1.
  • Skylark ESRO S75/1 Ionosphere mission Nation: Europe. Agency: ESRO. Apogee: 136 km (84 mi).

1973 - 03:35 GMT - Launch Site: White Sands. Launch Vehicle: Aerobee 170. Model: Aerobee 170A. LV Configuration: Aerobee 170A NASA 13.64UG.
  • Aerobee 170 Astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1973 - 10:31 GMT - Launch Site: Poker Flat. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.205-2.
  • Paiute Tomahawk ICECAP 73A Auroral mission Nation: USA. Agency: USAF CRL. Apogee: 213 km (132 mi).

1974 - Launch Site: Wake Island. Launch Vehicle: Athena H.
  • Athena H HAVE MILL 3 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1975 -
  • Mariner 10 deactivated Nation: USA. Spacecraft: Mariner 10.

    The vehicle was turned off after its onboard fuel was depleted.

1976 - 00:40 GMT - Launch Site: Thumba. Launch Vehicle: Centaure. Model: Centaure 2B. LV Configuration: Centaure 2B ISRO 5.30.
  • Centaure ISRO 5.30 Ionosphere/Fields mission Nation: India. Agency: ISRO. Apogee: 142 km (88 mi).

1977 - 11:51 GMT - Launch Site: Plesetsk. Launch Vehicle: Molniya 8K78M. Model: Molniya 8K78M.
  • Molniya 1-36 Nation: USSR. Program: Molniya. Payload: Molniya-1T. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-1T. Agency: MOM. Perigee: 2,288 km (1,421 mi). Apogee: 38,042 km (23,638 mi). Inclination: 63.70 deg. Period: 717.30 min. COSPAR: 1977-021A. USAF Sat Cat: 9880.

    Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programmes to stations in the Orbita and participating international networks (international cooperation scheme). Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T.

1977 - 13:10 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12.
  • MR-12 Ionosphere/Plasma/Fields mission Nation: USSR. Apogee: 160 km (90 mi).

1977 - 20:47 GMT - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Poseidon.
  • Poseidon Operational Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1977 - 20:47 GMT - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Poseidon.
  • Poseidon Operational Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1977 - 22:11 GMT - Launch Site: Plesetsk. Launch Complex: LC132. Launch Pad: LC132/2. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53749-159.
  • Cosmos 899 Nation: USSR. Program: Tselina. Mass: 900 kg (1,980 lb). Class: Sigint. Spacecraft: Tselina-O. Agency: MO SSSR. Perigee: 503 km (312 mi). Apogee: 547 km (339 mi). Inclination: 74.10 deg. Period: 95.20 min. COSPAR: 1977-022A. USAF Sat Cat: 9883. Decay Date: 1980-10-19.

    Replaced Cosmos 437. Possible ELINT satellite.

1979 -
  • Ferry flight, Eglin AFB to KSC Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Columbia.

    Ferry flight, shuttle carrier aircraft/Columbia (OV-102) from Eglin AFB to KSC (1 hour, 33 minutes)

1979 - 11:04 GMT - Launch Site: Poker Flat. Launch Vehicle: Taurus Tomahawk. LV Configuration: Taurus Tomahawk NASA 12.1003UE.
  • Taurus Tomahawk Plasma mission Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).

1981 - 03:00 GMT - Launch Site: White Sands. Launch Vehicle: Black Brant. Model: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.55UH.
  • Black Brant Extreme ultraviolet Astronomy mission Nation: USA. Agency: NASA. Apogee: 261 km (162 mi).

1981 - 03:31 GMT - Launch Site: Plesetsk. Launch Complex: LC41. Launch Pad: LC41/1. Launch Vehicle: Molniya 8K78M. Model: Molniya 8K78M.
  • Molniya 3-15 Nation: USSR. Program: Molniya. Payload: Molniya-3 s/n 24. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-3. Agency: MOM. Perigee: 201 km (124 mi). Apogee: 40,052 km (24,887 mi). Inclination: 63.90 deg. Period: 715.70 min. COSPAR: 1981-030A. USAF Sat Cat: 12368. Decay Date: 1992-10-19.

    Replace Molniya 3-11. Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programmes to stations in the Orbita and participating international networks (international cooperation scheme).

1982 - 00:12 GMT - Launch Site: Plesetsk. Launch Complex: LC41. Launch Pad: LC41/1. Launch Vehicle: Molniya 8K78M. Model: Molniya 8K78M.
  • Molniya 3-18 Nation: USSR. Program: Molniya. Payload: Molniya-3 s/n 29. Mass: 1,600 kg (3,500 lb). Class: Communications. Spacecraft: Molniya-3. Agency: MOM. Perigee: 121 km (75 mi). Apogee: 38,589 km (23,978 mi). Inclination: 63.90 deg. Period: 684.70 min. COSPAR: 1982-023A. USAF Sat Cat: 13107. Decay Date: 1992-06-23.

    Replaced Molniya 3-15. Operation of the long-range telephone and telegraph radio communications system in the USSR; transmission of USSR Central Television programmes to stations in the Orbita network and within the framework of international cooperation.

1982 - 19:47 GMT - Launch Site: Plesetsk. Launch Complex: LC132. Launch Pad: LC132/1. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53767-253.
  • Cosmos 1344 Nation: USSR. Mass: 810 kg (1,780 lb). Class: Navigation. Spacecraft: Parus. Agency: MO SSSR. Perigee: 967 km (600 mi). Apogee: 1,007 km (625 mi). Inclination: 82.90 deg. Period: 104.80 min. COSPAR: 1982-024A. USAF Sat Cat: 13110.

    Military navigation satellite. Replaced Cosmos 1244.

1983 - 20:55 GMT - Launch Site: Plesetsk. Launch Complex: LC132. Launch Pad: LC132/2. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53739-548.
  • Cosmos 1447 Nation: USSR. Payload: Tsikada-Kospas. Mass: 810 kg (1,780 lb). Class: Navigation. Spacecraft: Nadezhda. Agency: MO SSSR. Perigee: 954 km (592 mi). Apogee: 1,011 km (628 mi). Inclination: 82.90 deg. Period: 104.80 min. COSPAR: 1983-021A. USAF Sat Cat: 13916.

    Carried COSPAS transponder; replaced Cosmos 1226. Investigation of the upper atmosphere and outer space; testing of systems for locating the position of ships and aircraft in difficulties (COSPAS-SARSAT system).

1987 - Launch Site: Sriharikota. Launch Complex: SLV. Launch Pad: SLV. Launch Vehicle: ASLV. Model: ASLV. LV Configuration: ASLV ASLV-D1. FAILURE: Second stage failed to ignite.
  • SROSS A Nation: India. Mass: 150 kg (330 lb). Class: Earth. Type: Magnetosphere. Spacecraft: SROSS. Agency: ISRO. Apogee: 10 km (6 mi). COSPAR: F870324A. Decay Date: 1987-03-24.

1987 - 18:30 GMT - Launch Site: Wallops Island. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.62UE.
  • Nike Orion Plasma mission Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1988 - 14:10 GMT - Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
  • Cosmos 1935 Nation: USSR. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-4K1. Agency: MOM. Perigee: 166 km (103 mi). Apogee: 330 km (200 mi). Inclination: 67.20 deg. Period: 89.50 min. COSPAR: 1988-025A. USAF Sat Cat: 19011. Duration: 15.00 days. Decay Date: 1988-04-08.

    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 - 13:38 GMT - Launch Site: Plesetsk. Launch Complex: LC132. Launch Pad: LC132/2. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65011-232.
  • Cosmos 2008 Nation: USSR. Program: Strela. Payload: Strela-1M no. 329. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,393 km (865 mi). Apogee: 1,471 km (914 mi). Inclination: 74.00 deg. Period: 114.50 min. COSPAR: 1989-025A. USAF Sat Cat: 19902.

    Eight satellites launched by a single carrier rocket.

  • Cosmos 2009 Nation: USSR. Program: Strela. Payload: Strela-1M no. 330. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,408 km (874 mi). Apogee: 1,472 km (914 mi). Inclination: 74.00 deg. Period: 114.70 min. COSPAR: 1989-025B. USAF Sat Cat: 19903.

  • Cosmos 2010 Nation: USSR. Program: Strela. Payload: Strela-1M no. 331. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,424 km (884 mi). Apogee: 1,472 km (914 mi). Inclination: 74.00 deg. Period: 114.80 min. COSPAR: 1989-025C. USAF Sat Cat: 19904.

  • Cosmos 2011 Nation: USSR. Program: Strela. Payload: Strela-1M no. 332. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,439 km (894 mi). Apogee: 1,472 km (914 mi). Inclination: 74.00 deg. Period: 115.00 min. COSPAR: 1989-025D. USAF Sat Cat: 19905.

  • Cosmos 2012 Nation: USSR. Program: Strela. Payload: Strela-1M no. 333. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,456 km (904 mi). Apogee: 1,472 km (914 mi). Inclination: 74.00 deg. Period: 115.20 min. COSPAR: 1989-025E. USAF Sat Cat: 19906.

  • Cosmos 2013 Nation: USSR. Program: Strela. Payload: Strela-1M no. 334. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,465 km (910 mi). Apogee: 1,480 km (910 mi). Inclination: 74.00 deg. Period: 115.40 min. COSPAR: 1989-025F. USAF Sat Cat: 19907.

  • Cosmos 2014 Nation: USSR. Program: Strela. Payload: Strela-1M no. 335. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,470 km (910 mi). Apogee: 1,491 km (926 mi). Inclination: 74.00 deg. Period: 115.60 min. COSPAR: 1989-025G. USAF Sat Cat: 19908.

  • Cosmos 2015 Nation: USSR. Program: Strela. Payload: Strela-1M no. 336. Mass: 40 kg (88 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-1M. Agency: MO SSSR. Perigee: 1,469 km (912 mi). Apogee: 1,510 km (930 mi). Inclination: 74.00 deg. Period: 115.80 min. COSPAR: 1989-025H. USAF Sat Cat: 19909.

1989 - 21:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17. Launch Pad: LC17B. Launch Vehicle: Delta 3000. Model: Delta 3920-8. LV Configuration: Delta 3920-8 D183.
  • USA 36 Nation: USA. Payload: Delta Star. Class: Military. Type: SDI. Spacecraft: SDI. Agency: SDIO. Perigee: 307 km (190 mi). Apogee: 312 km (193 mi). Inclination: 47.70 deg. Period: 90.70 min. COSPAR: 1989-026A. USAF Sat Cat: 19911. Decay Date: 1992-06-23.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

1990 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4.
  • Trident C-4 CINC Evaluation Test launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1990 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Vehicle: Minuteman 3.
  • Minuteman 3 FOT GT138GM Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1990 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4.
  • Trident C-4 CINC Evaluation Test launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1990 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4.
  • Trident C-4 CINC Evaluation Test launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1990 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4.
  • Trident C-4 CINC Evaluation Test launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1992 - 13:13 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39. Launch Pad: LC39A. Launch Vehicle: Shuttle. Model: Space Shuttle. LV Configuration: Space Shuttle STS-45.
  • STS-45 Nation: USA. Program: STS. Payload: Atlantis F11 / Atlas 1 Fwd. Mass: 8,020 kg (17,680 lb). Class: Manned. Type: Spaceplane. Spacecraft: Atlantis. Agency: NASA JSC. Perigee: 282 km (175 mi). Apogee: 294 km (182 mi). Inclination: 57.00 deg. Period: 90.30 min. COSPAR: 1992-015A. USAF Sat Cat: 21915. Duration: 8.92 days. Decay Date: 1992-04-02. Crew: Bolden, Duffy, Foale, Frimout, Leestma, Lichtenberg, Sullivan. Flight: STS-45.

    Manned seven crew. Carried ATLAS-1 experimental package. Payloads: Atmospheric Laboratory for Applications and Science (ATLAS)-1, Shuttle Solar Backscat-ter Ultraviolet (SSBUV)-4, Getaway Special Experiment G-229, Space Tissue Loss (STL)-1, Radiation Monitoring Equipment (RME)-lIl, Visual Function Tester (VFT)-lI, Cloud Logic To Opti-mize Use of Defense Systems (CLOUDS)-1A, Investigations Into Polymer Membrane Process-ing (IPMP), Shuttle Amateur Radio Experiment (SAREX)-Il, Ultraviolet Plume Instrument (UVPl).

  • Atlas 1 Aft Nation: USA. Program: STS. Agency: NASA. COSPAR: 1992-015xx. USAF Sat Cat: 21915. Decay Date: 1992-04-02.

  • Atlas 1 Fwd Nation: USA. Program: STS. Agency: NASA. COSPAR: 1992-015xx. USAF Sat Cat: 21915. Decay Date: 1992-04-02.

1995 - Launch Site: Vandenberg.
  • Final launch of an Atlas E booster from Vandenberg Nation: USA.

    Final launch of an Atlas E booster from Vandenberg AFB (first launch on 7 June 1961).

1995 - 14:05 GMT - Launch Site: Vandenberg. Launch Complex: SLC3. Launch Pad: SLC3W. Launch Vehicle: Atlas E. Model: Atlas E. LV Configuration: Atlas E 45E / Star-37S-ISS.
  • USA 109 Nation: USA. Program: DMSP. Payload: DMSP 24547/Star 37S / DMSP F13. Mass: 750 kg (1,650 lb). Class: Earth. Type: Weather. Spacecraft: DMSP Block 5D-2. Agency: USAF. Perigee: 845 km (525 mi). Apogee: 854 km (530 mi). Inclination: 98.80 deg. Period: 101.90 min. COSPAR: 1995-015A. USAF Sat Cat: 23533.

    Last successful Atlas E space launch.

1998 - 01:46 GMT - Launch Site: Kourou. Launch Complex: ELA2. Launch Pad: ELA2. Launch Vehicle: Ariane 4. Model: Ariane 40. LV Configuration: Ariane 40 V107.
  • SPOT 4 Nation: France. Program: SPOT. Mass: 2,755 kg (6,073 lb). Class: Earth. Type: Landsat. Spacecraft: SPOT-4. Manufacturer: Matra Marconi Space-France, Toulouse. Agency: CNES. Perigee: 824 km (512 mi). Apogee: 826 km (513 mi). Inclination: 98.70 deg. Period: 101.40 min. COSPAR: 1998-017A. USAF Sat Cat: 25260.

    Developed by Matra Marconi Space/Toulouse for CNES, the satellite provided 10-m resolution images with a wide field of view. SPOT 4 also carried a wide field 'vegetation' imager and a laser communications experiment. Launch was by an Arianespace Ariane 40 rocket, the base Ariane 4 model with no strap-on boosters. The liquid hydrogen fuelled third stage of the Ariane 40 entered an 800 km sun-synchronous orbit together with SPOT 4.

2006 - Launch Site: Kwajalein. Launch Complex: Omelek. Launch Vehicle: Falcon I. FAILURE: Fuel leak at T+25 seconds caused a fire in the first stage engine area.
  • Falconsat-2 Nation: USA. Mass: 20 kg (44 lb). Class: Technology. Manufacturer: USAFA. Agency: USAFA. COSPAR: F20060324.

    The satellite fell through the roof of SpaceX's machine shop on the atoll.


Born on this day in:
  • 1932 - Dr Lodewijk van den Berg.  American Payload Specialist Astronaut. Birth City: Sluiskil. Birth Country: Netherlands.
  • 1957 - Dr Scott Jay (Doc) Horowitz.  Jewish American Pilot Astronaut. Birth City: Philadelphia. Birth State: Pennsylvania. Birth Country: USA.

Died on this day in:
  • 2002 - Thomas J Kelly.  American Engineer.
 
 
 
 
 
 
 
 
 

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