Encyclopedia Astronautica
March 19


March 19 Chronology


1915 March 19 - .
  • Birth of Norman H Horowitz - . Nation: USA. Summary: American biologist, at Caltech from 1940, worked at JPL on the Viking Mars lander program..

1920 March 19 - .
  • Goddard's dreams of space flight - . Nation: USA. Related Persons: Goddard. Goddard receives a grant of $ 3,500 from Clark University to continue rocket research. In a letter to the fund supervisor, he lays out his advanced concepts - Lox/LH2 liquid rockets, use of solar thermal and ion engines for interplanetary travel, constant-thrust 7.13 week trajectories to Mars. But publicly and practically, he continues his work on cartridge rockets.

1923 March 19 - .
  • US Navy discontinues contract with Goddard - . Nation: USA. Related Persons: Goddard. Summary: During the previous three years, at a total cost of $ 2,000, Goddard had developed a rocket-propelled depth charge and anti-ship missile with an armour-piercing warhead. The Navy sees no future potential in the work..

1940 March 19 - . LV Family: V-2. Launch Vehicle: V-2.
  • A4 rocket development removed from priority list. - . Nation: Germany. Related Persons: Hitler. After the military success in Poland, Hitler believes development of expensive 'wonder weapons' are unnecessary to win the war. The A4 and other rocket projects are removed from the priority list, making acquisition of necessary materials and engineers difficult.

1945 March 19 - . 13:28 GMT - . Launch Site: V-2 Battery SS Abt 500. LV Family: V-2. Launch Vehicle: V-2.
  • V-2 combat launch from Hellendoorn to Brasschaat - . Nation: Germany. Summary: Hellendoorn, Eelerberg, rocket fired, impacted Brasschaat..

1946 March 19 - . LV Configuration: Word Circling Space Ship.
  • Project RAND - . Nation: USA. Summary: The Army Air Forces established Project RAND, which in part included the study of satellite applications..

1946 March 19 - . Launch Site: Kapustin Yar. Launch Vehicle: RNII Sounding Rocket. FAILURE: Failure.
  • Test mission - . Nation: USSR. Agency: FIAN. Apogee: 1.00 km (0.60 mi).

1948 March 19 - . 23:10 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 39. FAILURE: Failure.
  • Blossom IIA Aeronomy / fields mission - . Nation: USA. Agency: USA; GE. Apogee: 5.00 km (3.10 mi). Summary: Launched 16:10 local time. Reached 5.5 km. Carried Magnetic field, composition, winds, temperature (Signal Corps Engineering Lab, University of Michigan) experiments for General Electric..

1951 March 19 - .
  • Julius and Ethel Rosenberg sentenced to death for passing atomic secrets to Russians - . Nation: USSR.

1952 March 19 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Double Deacon.
  • Navaho Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1953 March 19 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1 8A11. LV Configuration: R-1 8A11 No 820.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1954 March 19 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1374T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1955 March 19 - . LV Family: Vanguard. Launch Vehicle: Vanguard.
  • Plan for a United States satellite in the International Geophysical Year - . Nation: USA. Related Persons: Eisenhower. Spacecraft: Vanguard 2. Summary: Dr. Alan T. Waterman of the National Science Foundation presented President Dwight Eisenhower with a plan to implement the United States' portion of the International Geophysical Year satellite experiment..

1955 March 19 - . 06:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-N-10. LV Configuration: Aerobee RTV-N-10 NRL 26.
  • Airglow Aeronomy mission - . Nation: USA. Agency: NRL. Apogee: 115 km (71 mi). Summary: Night airglow research. Launched at 2300 local time. Reached 114.3 km..

1958 March 19 - . 01:12 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee. LV Configuration: Aerobee USAF-93.
  • NO / O2 composition Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).

1959 March 19 - . LV Family: X-17. Launch Vehicle: X-17.
  • X-17s used for rocket launch of nuclear tests. - . Nation: USA. Summary: Deputy Secretary of Defense Quarles announced that three atomic blasts were secretly fired in space (Project Argus) in 1958, using modified X-17 rockets..

1959 March 19 - . 00:59 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC12. LV Family: Atlas. Launch Vehicle: Atlas C. LV Configuration: Atlas C 7C. FAILURE: Failure. Failed Stage: 1.
  • RVX-2 re-entry vehicle research and development mission - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1960 March 19 - .
  • Mercury tracking agreements with foreign countries - . Nation: USA. Program: Mercury. Summary: United States-Spanish agreement on Project Mercury tracking station in Canary Islands was announced (1 of 16 similar agreements with other nations)..

1961 March 19 - .
  • Vostok launch delay - . Nation: USSR. Related Persons: Gusev; Feoktistov; Yazdovskiy; Karpov; Gagarin; Nelyubov; Titov. Program: Vostok. Flight: Vostok 1. Spacecraft: Vostok. The launch has been delayed to 24-25 March due to problems with L I Gusev's radio system aboard the spacecraft. A meeting of the cosmonauts at 10:00 reviews landing contingency plans that will bring the capsule down on the territory of the USSR. The best chances for such a landing are on orbits 1, 2, and 16, but it is also possible on orbits 4, 5, 6, and 7. A map will be aboard the capsule to show where and when to ignite the TDU retrorocket for each landing opportunity. Feoktistov was a great help in developing this visual aid. For about an hour Kamanin, Korolev, Yazdovskiy, Karpov, and Azbiyevich discuss long-range plans. Korolev is interested in the VVS position that they should be responsible for all military space activities. The reconnaissance satellite version of Vostok is discussed. Korolev says he plans to send a cosmonaut to the moon by 1965.

    Afterwards the cosmonauts develop the radio communications plan for the flight. During the 710-second ascent to orbit, and after landing, they are to use the UHF radio. The HF and UHF radios can be used from orbit, but only over the USSR. Plans for filming the cosmonaut in flight are also discussed.


1962 March 19 - . 11:04 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 2. LV Configuration: Skylark-2 SL161.
  • Grenades / Chaff Aeronomy mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 140 km (80 mi).

1962 March 19 - . 23:28 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC10E. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 229.
  • Combat training launch - . Nation: USA. Agency: RAF. Apogee: 520 km (320 mi).

1963 March 19 - .
  • Chamberlin reassigned from Manager of Project Gemini. - . Nation: USA. Related Persons: Gilruth; Chamberlin. Program: Gemini. Spacecraft: Gemini. James A Chamberlin was reassigned from Manager of Project Gemini to Senior Engineering Advisor to Robert R Gilruth, Director of Manned Spacecraft Center. Charles W Mathews was reassigned from Chief, Spacecraft Technology Division, to Acting Manager of Project Gemini.

1963 March 19 - . 16:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3X-11.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1964 March 19 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • The Air Force Systems Command weekly report (inaugurated in September 1963) summarizing actions taken to resolve Titan II development problems would no longer be issued. - . Nation: USA. Related Persons: Mueller. Summary: George E. Mueller, NASA Associate Administrator for Manned Space Flight, informed Associate Administrator Robert C. Seamans, Jr., that the launch vehicle 'no longer appears to be the pacing item in the Gemini program.'.

1964 March 19 - . 11:13 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta B. LV Configuration: Thor Delta B 391/D24. FAILURE: Insufficient third stage thrust.. Failed Stage: 3.
  • Explorer (20) - . Payload: Beacon Explorer A. Mass: 54 kg (119 lb). Nation: USA. Agency: NASA. Program: Explorer. Class: Earth. Type: Magnetosphere satellite. Spacecraft: BE. Decay Date: 1964-03-19 . COSPAR: F640319A. Summary: Also known as Explorer S-66..

1964 March 19 - . 15:42 GMT - . Launch Site: Andoya. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache Ferdinand 8.
  • Ferdinand 8 Ionosphere / plasma / solar mission - . Nation: Norway. Agency: NDRE. Apogee: 139 km (86 mi).

1965 March 19 - . 03:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.57GG.
  • Ultraviolet spectra Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 155 km (96 mi).

1965 March 19 - . 06:24 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2. LV Configuration: Black Brant II AA-2A-52.
  • Fields mission - . Nation: Canada. Agency: NRCC. Apogee: 168 km (104 mi).

1965 March 19 - . 18:09 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 12.05/18.01GA.
  • Thermosphere probe Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 315 km (195 mi).

1965 March 19 - .
  • Landing of Voskhod 2 - . Return Crew: Belyayev; Leonov. Nation: USSR. Related Persons: Korolev; Belyayev; Leonov; Voronin. Program: Voskhod. Flight: Voskhod 2. Spacecraft: Voskhod. On re-entry the primary automatic retrorocket system failed. A manually controlled retrofire was accomplished one orbit later (evidently using the primary engine, not the backup solid rocket retropack on the nose of spacecraft). The service module failed to separate completely, leading to wild gyrations of the joined reentry sphere - service module before connecting wires burned through. Vostok 2 finally landed near Perm in the Ural mountains in heavy forest at 59:34 N 55:28 E on March 19, 1965 9:02 GMT. The crew spent two nights in deep woods, surrounded by wolves. Recovery crews had to chop down trees to clear landing zones for helicopter recovery of the crew, who had to ski to the clearing from the spacecraft. Only some days later could the capsule itself be removed. Additional Details: Landing of Voskhod 2.

1966 March 19 - . 12:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 304D.
  • NTMP KX-43 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 March 19 - . 12:31 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LC-A. LV Family: Javelin. Launch Vehicle: Nike Javelin.
  • HITAB 1 Technology test - . Nation: USA. Agency: USN. Apogee: 130 km (80 mi).

1968 March 19 - .
  • Further development of Lox/LH2 rocket engines authorised. - . Nation: USSR. Summary: Ministry of General Machine Building (MOM) Decree 88 'On use of liquid hydrogen in the space program' was issued..

1968 March 19 - . 16:15 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.202NT.
  • SPARCS test - . Nation: USA. Agency: NASA. Apogee: 159 km (98 mi).

1968 March 19 - . 18:20 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 176 km (109 mi).

1968 March 19 - . 19:05 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 178 km (110 mi).

1969 March 19 - . 21:30 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Ionosphere/Plasma mission - . Nation: USSR. Agency: AN. Apogee: 181 km (112 mi).

1969 March 19 - . 21:38 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Delta. Launch Vehicle: Thorad Agena D SLV-2G. LV Configuration: Thorad SLV-2G Agena D 541 / Agena D 1651.
  • KH-4A 1050 - . Payload: KH-4A s/n 1050 / Agena D 1651 / OPS 3722. Mass: 2,000 kg (4,400 lb). Nation: USA. Agency: NRO; CIA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-4A. Decay Date: 1969-03-24 . USAF Sat Cat: 3829 . COSPAR: 1969-026A. Apogee: 252 km (156 mi). Perigee: 165 km (102 mi). Inclination: 82.9000 deg. Period: 88.60 min. Summary: KH-4A. Due to abnormal rotational rates after revolution 22, the mission was terminated after a total of three days collecting photography..
  • OPS 2285 - . Payload: EHH B14. Nation: USA. Agency: USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1971-12-06 . USAF Sat Cat: 3830 . COSPAR: 1969-026xx. Apogee: 168 km (104 mi). Perigee: 168 km (104 mi). Inclination: 83.0000 deg. Period: 87.90 min.
  • SRV 737 - . Payload: SRV 1050-1 / OPS 2285. Mass: 60 kg (132 lb). Nation: USA. Agency: NRO; USAF. Spacecraft: KH-4A. Decay Date: 1971-12-06 . USAF Sat Cat: 3830 . COSPAR: 1969-026B. Apogee: 515 km (320 mi). Perigee: 502 km (311 mi). Inclination: 83.1000 deg. Period: 94.70 min. Summary: Radar monitoring..

1970 March 19 - .
  • Cosmonaut tours - . Nation: USSR. Related Persons: Leonov; Shatalov. Summary: Leonov is going on a propaganda tour to Japan, and Shatalov to Cuba..

1970 March 19 - .
  • X-24 Flight 10 - . Crew: Gentry. Payload: X-24A flight 10. Nation: USA. Related Persons: Gentry. Class: Manned. Type: Manned spaceplane. Spacecraft: X-24A. Summary: First powered flight. Maximum Speed - 919 kph. Maximum Altitude - 13533 m. Flight Time - 424 sec..

1970 March 19 - . 02:30 GMT - . Launch Site: Kiruna. LV Family: Skua. Launch Vehicle: Skua 2. LV Configuration: Skua 2 RTG SSK3/1 (K70/01).
  • Aeronomy / ionosphere mission - . Nation: UK. Agency: RTG. Apogee: 108 km (67 mi).

1970 March 19 - . 03:19 GMT - . Launch Site: Thumba. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.425GI.
  • ISRO 10.33 / 17.04 Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1970 March 19 - . 03:23 GMT - . Launch Site: Kiruna. LV Family: Skua. Launch Vehicle: Skua 2. LV Configuration: Skua 2 RTG SSK3/2 (K70/02).
  • Aeronomy / ionosphere mission - . Nation: UK. Agency: RTG. Apogee: 108 km (67 mi).

1970 March 19 - . 03:56 GMT - . Launch Site: Kiruna. LV Family: Skua. Launch Vehicle: Skua 2. LV Configuration: Skua 2 RTG SSK3/3 (K70/03?).
  • Aeronomy / ionosphere mission - . Nation: UK. Agency: RTG. Apogee: 101 km (62 mi).

1970 March 19 - . 04:28 GMT - . Launch Site: Kiruna. LV Family: Skua. Launch Vehicle: Skua 2. LV Configuration: Skua 2 RTG SSK3/4 (K70/04?).
  • Aeronomy / ionosphere mission - . Nation: UK. Agency: RTG. Apogee: 105 km (65 mi).

1970 March 19 - . 05:18 GMT - . Launch Site: Kiruna. LV Family: Skua. Launch Vehicle: Skua 2. LV Configuration: Skua 2 RTG SSK3/5 (K70/05?).
  • Aeronomy / ionosphere mission - . Nation: UK. Agency: RTG. Apogee: 105 km (65 mi).

1970 March 19 - . 10:01 GMT - . Launch Site: Thumba. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.372GI.
  • ISRO 10.35 / 17.06 Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 196 km (121 mi).

1970 March 19 - . 15:18 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 3 AC. LV Configuration: Skylark 3 AC SL401.
  • Ultraviolet Schmidt Objective Prism Ultraviolet astronomy mission - . Nation: UK. Agency: BAC. Apogee: 181 km (112 mi).

1971 March 19 - .
  • State Commission for Launch of DOS#1. - . Nation: USSR. Related Persons: Mishin. Program: Salyut. Flight: Soyuz 10; Soyuz 11; Soyuz 12 / DOS 1. Spacecraft: Salyut 1. Summary: The VVS insists that the Soyuz 10 crew land in daylight. Mishin says that in order that the crew can land in daylight at the end of the 30-day mission, the spacecraft must be launched at 03:00 at night. Kamanin believes this also to be unsafe..

1971 March 19 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 659. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 March 19 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 659. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 March 19 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 659. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 March 19 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 659. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 March 19 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 659. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 March 19 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 659. LV Family: Polaris. Launch Vehicle: Polaris A3.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 March 19 - . Launch Site: Hall Beach. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.128GE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 250 km (150 mi).

1971 March 19 - . Launch Site: Hall Beach. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.123GE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1971 March 19 - . 12:05 GMT - . Launch Site: Poker Flat. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.94UA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1971 March 19 - . 12:38 GMT - . Launch Site: Poker Flat. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk.
  • Ionosphere / aurora mission - . Nation: USA. Agency: Sandia. Apogee: 270 km (160 mi).

1972 March 19 - . 12:00 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 91 km (56 mi).

1973 March 19 - .
  • Second Skylab-B program between considered to fill late 1970's gap between the Apollo-Soyuz Test Project and the Space Shuttle. - . Nation: USA. Program: Skylab. Flight: Skylab B. Consideration was being given to the feasibility of a second set of Skylab missions (designated Skylab-B) during the interval between the Apollo-Soyuz Test Project in 1975 and the start of Space Shuttle operations late in 1979. The inherent worth of a Skylab-B was recognized, but officials were reluctant to recommend it, on the premise that it would be unwise to allow it to delay or displace the development of the Space Shuttle and other programs already included in the FY 1974 budget.

1974 March 19 - . 17:30 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy/Chemical release/Plasma mission - . Nation: USSR. Apogee: 146 km (90 mi).

1975 March 19 - . 09:21 GMT - . Launch Site: Thumba. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P185T/C.
  • ISRO-18.19 Ionosphere mission - . Nation: UK. Agency: SRC. Apogee: 107 km (66 mi).

1976 March 19 - . 19:31 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-34 - . Payload: Molniya-1T. Mass: 1,600 kg (3,500 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1T. Decay Date: 1985-05-14 . USAF Sat Cat: 8762 . COSPAR: 1976-026A. Apogee: 39,722 km (24,682 mi). Perigee: 617 km (383 mi). Inclination: 62.7000 deg. Period: 717.40 min. 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).

1977 March 19 - . 06:06 GMT - . Launch Site: Fort Churchill. LV Family: Astrobee. Launch Vehicle: Astrobee F. LV Configuration: Astrobee F NASA 25.25UE.
  • Auroral Oxides Plasma mission - . Nation: USA. Agency: NASA. Apogee: 195 km (121 mi).

1978 March 19 - .
  • Aft payload bay doors on dock, Palmdale, Columbia - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Columbia.

1979 March 19 - . 22:57 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna A. Launch Vehicle: Aries. LV Configuration: Aries NASA 24.05IE.
  • DLR K-AR-92 Porc. F3 Magnetospheric mission - . Nation: USA. Agency: NASA. Apogee: 460 km (280 mi).

1980 March 19 - . 07:59 GMT - . Launch Site: Poker Flat. LV Family: Tomahawk Sandia. Launch Vehicle: Taurus Tomahawk. LV Configuration: Taurus Tomahawk NASA 34.01UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 596 km (370 mi).

1981 March 19 - . 16:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1982 March 19 - . 18:00 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 91 km (56 mi).

1983 March 19 - . 06:29 GMT - . Launch Site: Poker Flat. LV Family: Super Chief. Launch Vehicle: Talos Castor. LV Configuration: Talos Castor GL A51.971.
  • ELIAS Aeronomy / aurora mission - . Nation: USA. Agency: USAF GL. Apogee: 305 km (189 mi).

1984 March 19 - . 17:00 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 644. Launch Vehicle: Poseidon.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1985 March 19 - . 20:00 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 64 km (39 mi).

1986 March 19 - . 10:08 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2.
  • Progress 25 - . Payload: Progress s/n 134. Mass: 7,270 kg (16,020 lb). Nation: USSR. Agency: MOM. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Mir EO-1. Spacecraft: Progress. Duration: 32.61 days. Completed Operations Date: 1986-04-21 00:48:05 . Decay Date: 1986-04-21 00:48:05 . USAF Sat Cat: 16645 . COSPAR: 1986-023A. Apogee: 251 km (155 mi). Perigee: 183 km (113 mi). Inclination: 51.7000 deg. Period: 88.80 min. Unmanned supply vessel transporting sundry cargoes to the Mir orbital station. Docked with Mir on 21 Mar 1986 11:16:02 GMT. Undocked on 20 Apr 1986 19:24:08 GMT. Destroyed in reentry on 21 Apr 1986 00:48:30 GMT. Total free-flight time 2.27 days. Total docked time 30.34 days.

1987 March 19 - . 03:54 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 323-01.
  • Raduga 20 - . Payload: Raduga s/n 31L. Mass: 1,965 kg (4,332 lb). Nation: USSR. Agency: MOM. Class: Communications. Type: Military communications satellite. Spacecraft: Raduga . Completed Operations Date: 1991-12-01 . USAF Sat Cat: 17611 . COSPAR: 1987-028A. Apogee: 37,159 km (23,089 mi). Perigee: 36,922 km (22,942 mi). Inclination: 5.1000 deg. Period: 1,500.60 min. Stationed at 85 deg E. Provision of telephone and telegraph radiocommunications and television broadcasting. Positioned in geosynchronous orbit at 85 deg E in 1987-1991 As of 30 August 2001 located at 6.40 deg W drifting at 15.515 deg W per day. As of 2007 Mar 10 located at 6.61W drifting at 15.520W degrees per day.

1987 March 19 - . 10:00 GMT - . Launch Site: Kiruna. LV Family: Black Brant. Launch Vehicle: Black Brant 9B. LV Configuration: Black Brant IXB MASER 1.
  • Microgravity mission - . Nation: Sweden. Agency: SSC. Apogee: 295 km (183 mi).

1989 March 19 - . 17:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-18.
  • 7 Mk 21 RVs to KMR - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1990 March 19 - .
  • Hiten, Moon Flyby (Japan) - . Nation: Japan. Spacecraft: Hiten.

1991 March 19 - . Launch Site: WTR Launch Area. Launch Platform: SSBN ?. LV Family: Trident. Launch Vehicle: Trident C-4.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1991 March 19 - . Launch Site: WTR Launch Area. Launch Platform: SSBN ?. LV Family: Trident. Launch Vehicle: Trident C-4.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1991 March 19 - . 13:05 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 R15000-049.
  • Progress M-7 - . Payload: Progress M s/n 208. Mass: 7,307 kg (16,109 lb). Nation: USSR. Agency: MOM. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Mir EO-8. Spacecraft: Progress M. Duration: 49.18 days. Completed Operations Date: 1991-05-07 17:21:50 . Decay Date: 1991-05-07 17:21:50 . USAF Sat Cat: 21188 . COSPAR: 1991-020A. Apogee: 213 km (132 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg. Period: 88.50 min. Unmanned resupply vessel to Mir. Attempted to dock with Mir on 21 March 1998 14:28 GMT, but missed the station by 500 m. Docking attempted again on 23 March but at 50 meters the docking was aborted; the Progress missed hitting the station by five meters. Thereafter it was placed in a station-keeping co-orbit with Mir while the problem was diagnosed. Finally docked with Mir on 28 Mar 1991 12:02:28 GMT. On 12 and 14 Apr 1998 two burns of the engine of Progress M-7 raised the station's orbit from a 360 x 377 km orbit to a 370 x 382 km orbit. Undocked on 6 May 1991 22:59:36 GMT. Destroyed in reentry on 7 May 1991 17:20:05 GMT. Total free-flight time 9.72 days. Total docked time 39.46 days.

1991 March 19 - . 14:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53448-417.
  • Cosmos 2137 - . Mass: 1,000 kg (2,200 lb). Nation: USSR. Agency: MO. Class: Military. Type: Radar calibration target. Spacecraft: Taifun-1Yu. Decay Date: 1995-04-03 . USAF Sat Cat: 21190 . COSPAR: 1991-021A. Apogee: 364 km (226 mi). Perigee: 356 km (221 mi). Inclination: 65.8000 deg. Period: 91.70 min. Summary: Radar calibration mission..

1992 March 19 - . 16:10 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.088DE.
  • HIRAAS 2 Airglow mission - . Nation: Canada. Agency: NASA. Apogee: 300 km (180 mi).

1995 March 19 - . 15:00 GMT - . Launch Site: White Sands. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.112UU.
  • CWAS 37 Aeronomy mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 140 km (80 mi).

1997 March 19 - . Launch Site: Bigen Island. LV Family: R-17. Launch Vehicle: R-17. LV Configuration: Scud FMA.
  • Willow Dune Target mission - . Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1998 March 19 - .
  • Beijing Space Conference - . Nation: China. Spacecraft: Shenzhou. Chinese papers at the meeting sketched details of future planned missions. China was likely to begin its manned flights with a single orbit around Earth, and later launch its lunar 'quest'. Existing Chinese launchers had the capability to send scientific devices, but not humans, to the moon -- it could take up to eight years to design a lunar spacecraft. Feasibility studies on trips to the moon and Mars had begun. Participants called for greater international cooperation in space and the lifting of an apparent freeze on China's participation in major joint projects. They resented China's exclusion from the International Space Station.

2000 March 19 - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-200.
  • Atmospheric Waves Aeronomy mission - . Nation: India. Agency: ISRO. Apogee: 70 km (43 mi).

2001 March 19 - . Launch Site: Kodiak. Launch Vehicle: Aries. LV Configuration: Aries QRLV-1.
  • Target mission - . Nation: USA. Agency: USAF SM. Apogee: 163 km (101 mi).

2002 March 19 - .
  • Progress M1-7 leaves ISS. - . Nation: Russia. Program: ISS. Flight: ISS EO-4. The Expedition 4 crew finished loading the Progress M1-7 craft, and it undocked from Zvezda's aft port at 1743 UTC. The Kolibri-2000 microsatellite was ejected from the Progress cargo compartment at 2228 UTC; Progress fired its engines to deorbit over the Pacific at about 0127 UTC on Mar 20.

2002 March 19 - . 22:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz FG. LV Configuration: Soyuz-FG F15000-002 / ISS-6P.
  • Kolibri - . Mass: 21 kg (46 lb). Nation: Russia. Agency: RAKA. Class: Technology. Type: Navigation technology satellite. Spacecraft: Kolibri. Decay Date: 2002-05-04 . USAF Sat Cat: 27394 . COSPAR: 2001-051C. Apogee: 388 km (241 mi). Perigee: 385 km (239 mi). Inclination: 51.6000 deg.

2004 March 19 - .
  • International Space Station Status Report #04-14A - . Nation: USA. Related Persons: Foale; Kaleri. Program: ISS. Flight: ISS EO-8. Heading into the homestretch of their 61/2-month mission aboard the International Space Station, Expedition 8 Commander Michael Foale and Flight Engineer Alexander Kaleri spent the week conducting biomedical experiments and performing maintenance on a key Station component. Additional Details: International Space Station Status Report #04-14A.

2005 March 19 - . Launch Site: Sonmiani. LV Family: DF-15. Launch Vehicle: Shaheen 2.
  • Shaheen 2 test - . Nation: Pakistan. Apogee: 300 km (180 mi).

2006 March 19 - .
  • Cassini, Titan Flyby - . Nation: USA. Spacecraft: Cassini.

2008 March 19 - .
  • Death of Arthur C Clarke - . Nation: UK. Related Persons: Clarke. Summary: British writer. Leading science fiction writer, also wrote key books popularizing space travel in 1950's and 1960's. Created concept of geosynchronous communications satellite in 1946. Wrote 2001: A Space Odyssey..

2008 March 19 - . 22:48 GMT - . Launch Site: Kiritimati. Launch Pad: 0.0 N x 154.0 W. Launch Platform: ODYSSEY. LV Family: Zenit. Launch Vehicle: Zenit-3SL. LV Configuration: Zenit-3SL s/n SL32.
  • DirecTV 11 - . Mass: 5,920 kg (13,050 lb). Nation: USA. Agency: DirecTV. Manufacturer: Boeing. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 32729 . COSPAR: 2008-013A. Apogee: 35,788 km (22,237 mi). Perigee: 35,787 km (22,236 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Placed in orbital slot 99.2 W Longitude. In combination with DirecTV 10, the satellite would allow the parent company to direct broadcast local HDTV to 90 percent of its customers in North America. The Ka-band satellite was equipped with 28 active and 8 spare TWTAs for direct broadcast to the continental United States and Alaska; 4 active and 4 spare for broadcast to the 48 stages and Hawaii; and 55 active and 15 spares for spot transmissions. Total power was 18 kW / 16 kW at beginning/end of life. Propulsion was provided by 445 N liquid apogee engine and four XIPS 35-cm ion thrusters. Mass at launch was 6060 kg and 3700 kg after on-board propellants were consumed to place the satellite in its operational geosynchronous orbit.

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