April 1 home
topic index

See also Born on this Day
On this day in:

1924 - Launch Vehicle: GIRD-09.

  • GiRD established. Nation: USSR.

    Central Committee for the Study of Rocket Propulsion (GIRD) established in the Soviet Union.

1945 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -.
  • Wallops Island authorized. Nation: USA.

    Supplemental appropriation passed by Congress authorized expanded research on guided missiles at NACA Langley Laboratory, including establishment of a rocket launch facility at Wallops Island, Va.

1945 - Launch Vehicle: Private.
  • Private F rockets tested. Nation: USA.

    17 JPL Private F rockets were fired at Hueco Range, Fort Bliss, Tex.

1945 - Launch Vehicle: V-1, V-2.
  • The end of the V-weapons. Nation: Germany.

    The V-weapon launch corps remained in service until the end of March. Then Kammler went to the Harz Mountains, to command a planned final effort to use the weapons to prevent a link-up of the American and Soviet forces - a plan that came to nothing. In all, 9,300 V-1's had been fired at Great Britain in its seven months of service, of which 6,000 reached the coast. 4,300 V-2's had been launched in combat, 1,500 at London, and 2,100 at Antwerp. 20% of these used the radio guidance system. The V-1's range had been extended in test models to 370 km, although only a few of these modifications had reached the front. On the other hand, the range of the V-2 had been extended to 350 km, and this was the version provided to the front-line troops in the last months. But at the end of March 1945 the Germans evacuated the V-weapon firing areas in Holland.

1947 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Deacon. Model: Deacon.
  • Test launch Nation: USA. Agency: NACA. Apogee: 10 km (6 mi).

    First Deacon rocket launched at Wallops Island, which achieved a velocity of 4,200 feet per second.

1947 - 20:10 GMT - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: V-2. LV Configuration: V-2 22.
  • Solar ultraviolet / chemical release mission Nation: USA. Agency: USA/APL. Apogee: 129 km (80 mi).

    Launched 13:10 local time. Reached 129.5 km. Carried cosmic and solar radiation, photo experiments for Applied Physics Lab, John Hopkins University.

1951 - Launch Site: Vernon. Launch Complex: -. Launch Pad: -. Launch Vehicle: Veronique. Model: Veronique P2. LV Configuration: Veronique P2 P2.
  • Test mission Nation: France. Agency: FR. Apogee: 0 km ( mi).

1952 - Launch Vehicle: Redstone.
  • Contractor to build Redstone rocket. Nation: USA.

    The Office, Chief of Ordnance (OCO) disapproved Redstone Arsenal's proposed development plan for what would become the Redstone missile. The arsenal had intended to implement the manufacturing program for these missiles by creating an assembly line in its own development shops. The OCO, however, required that the development effort be done by a prime contractor. Nonetheless, delays in the acquisition of production facilities for the prime contractor caused Redstone Arsenal to fabricate and assemble the first 12 Redstone missiles along with missiles 18 through 29.

1953 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5.
  • Phase I state trials launch Nation: USSR. Agency: NII-88. Apogee: 300 km (180 mi).

    Of the 8 rockets of the first production lot fired, 6 reached the target area.

1954 -
  • Bell contract for an advanced, bomber-reconnaissance weapon system. Nation: USA. Spacecraft: Dynasoar, Bomi.

    The Air Force and the Bell Aircraft Company arranged a contract for the study of an advanced, bomber-reconnaissance weapon system.

1954 - Launch Site: Edwards. Launch Complex: -. Launch Pad: -. Launch Vehicle: Navaho. Model: Navaho X-10. LV Configuration: X-10 s/n 1 GM-19307.
  • Navaho X-10 flight 4 Nation: USA. Program: Navaho.

    First supersonic flight; reached Mach 1.47.

1955 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M.
  • ZI test Nation: USSR. Agency: NII-88. Apogee: 500 km (310 mi).

1955 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M.
  • ZI test Nation: USSR. Agency: NII-88. Apogee: 500 km (310 mi).

1957 -
  • Van Allen heads research panel. Nation: USA.

    Upper Atmosphere Rocket Research Panel was renamed the Rocket and Satellite Research Panel. Its chairman was James A. Van Allen of the State university of Iowa.

1957 - Launch Site: Kapustin Yar. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-11. Model: R-11M.
  • Test mission Nation: USSR. Agency: NII-88. Apogee: 200 km (120 mi).

1958 -
  • Lunar photographic atlas begun Nation: USA. Program: Lunex.

    A $61,000 contract was signed by the Yerkes Observatory, University of Chicago, and the Air Force. Gerard P. Kuiper, principal investigator, was to produce a new lunar photographic atlas. The moon's visible surface would be divided into 44 areas, and each would be represented by at least four photographs taken under varying lighting conditions. - Additional details.

1958 - Launch Vehicle: R-11.
  • R-11M accepted into military service. Nation: USSR.

    Decree 'On adoption of the R-11M into armaments' was issued.

1959 -
  • Two-man Mercury capsule proposed. Nation: USA. Spacecraft: Gemini.

    H. Kurt Strass of the Space Task Group (STG) at Langley Field, Virginia described some preliminary ideas of STG planners regarding a follow-on to Mercury: (1) an enlarged Mercury capsule to place two men in orbit for three days; (2) a two-man Mercury capsule and a large cylindrical structure to support a two-week mission. (In its 1960 budget, NASA had requested $2 million to study methods of constructing a manned orbiting laboratory or converting the Mercury spacecraft into a two-man laboratory for extended space missions.) - Additional details.

1959 - Launch Vehicle: Soyuz. Model: R-7A.
  • R-7A ICBM production approved. Nation: USSR.

    Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On production of the R-7A missile at Plant No. 1001 at Krasnoyarsk-26 and establishment of a branch' was issued.

1960 -
  • Mercury astronauts complete centrifuge training. Nation: USA. Program: Mercury.

    Seven Mercury astronauts completed training session at the Navy Aviation Medical Acceleration Laboratory, Johnsville, Pa.

1960 -
  • Mercury first production spacecraft delivered to NASA Nation: USA. Program: Mercury. Spacecraft: Mercury.

    The first McDonnell production spacecraft was delivered to NASA at Wallops Island for the beach-abort test.

1960 -
  • USAF Dynasoar Astronaut Training Group selected. Nation: USA.

    The group was selected to provide pilots for X-20A Dyna-Soar spaceplane flights.. Qualifications: Assigned from pool of active USAF and NASA Test Pilots.. Ten test pilots (7 USAF, 3 NASA) underwent physical examinations in August 1959. Seven were secretly selected in April 1960.

1960 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Shotput. LV Configuration: Shotput 4.
  • E60 Echo spacecraft test Nation: USA. Agency: NASA LaRC. Apogee: 400 km (240 mi).

1960 - 11:40 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Able II. LV Configuration: Thor Able II-M1 148.
  • Tiros 1 Nation: USA. Program: Tiros. Payload: Tiros A (A-1). Mass: 120 kg (260 lb). Class: Earth. Type: Weather. Spacecraft: Tiros. Agency: NASA. Perigee: 656 km (407 mi). Apogee: 696 km (432 mi). Inclination: 48.40 deg. Period: 98.30 min. COSPAR: 1960-Beta-2. USAF Sat Cat: 29.

    TV and Infrared Observation Satellite; returned 22952 cloud cover photos. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).

1961 - 03:25 GMT - Launch Site: Akita. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9L. LV Configuration: Kappa 9L K-9L-1.
  • Test mission Nation: Japan. Agency: ISAS. Apogee: 350 km (210 mi).

1963 - Launch Vehicle: Titan. Model: Titan 2.
  • POGO problems in the Titan II. Nation: USA.

    The Titan II-Gemini Coordination Committee was established to direct efforts to reduce longitudinal vibration (POGO) in the Titan II and to improve engine reliability. Air Force Space Systems Division (SSD) and Aerospace had presented to NASA and the Air Force a series of briefings on the POGO problem that culminated in a briefing to the Gemini Program Planning Board. The main problem was that POGO level satisfactory in the weapon system was too high to meet NASA standards for the Gemini program, and further reduction in the POGO level required a much more elaborate and extensive analytic and experimental program than had so far been considered necessary. The board approved the SSD/Aerospace proposals and established a committee to oversee work toward a POGO remedy. The high-level committee was composed of officials from Air Force Ballistic Systems Division, SSD, Space Technology Laboratories, and Aerospace.

1963 - Launch Site: Kerguelen. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure.
  • Ionosphere mission Nation: France. Agency: CNES. Apogee: 130 km (80 mi).

1963 - 23:01 GMT - Launch Site: Vandenberg. Launch Complex: SLC1E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena D. LV Configuration: Thor Agena D 376 / Agena D 1160.
  • KH-4 9053 Nation: USA. Payload: KH-4 s/n 9053 / Agena D 1160. Mass: 1,150 kg (2,530 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4. Agency: NRO/CIA. Perigee: 198 km (123 mi). Apogee: 408 km (253 mi). Inclination: 74.90 deg. Period: 90.50 min. COSPAR: 1963-007A. USAF Sat Cat: 562. Decay Date: 1963-04-26.

    KH-4; film capsule recovered 3.1 days later. Best imagery to date.

1964 -
  • Contract for 27 prototype Apollo space suits Nation: USA. Program: Apollo. Spacecraft: A7L.

    MSC negotiated a cost-plus-incentive-fee contract, valued at $1.65 million, with Hamilton Standard for 27 prototype Apollo space suits and 12 pairs of gloves.

1964 -
  • Barmin's design bureau named lead for all space launch pad designs. Nation: USSR.

    Decree 'On appointing KB TM as main space launch pad design organization' was issued.

1964 - Launch Site: Little Carter Bay. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 HITAB.
  • TSRA-2 Infrared Astronomy/Ultraviolet Astronomy mission Nation: USA. Agency: NOTS. Apogee: 200 km (120 mi).

1964 - 03:10 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8L. LV Configuration: Kappa 8L K-8L-3.
  • Aeronomy / fields mission Nation: Japan. Agency: ISAS. Apogee: 100 km (60 mi).

1964 - 20:22 GMT - Launch Site: Cape Canaveral. Launch Complex: LC11. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 137F.
  • ABRES WAC-2 / Pod 2 Reentry test / plume mission Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1965 -
  • All-battery electrical power system for the Apollo LEM Nation: USA. Program: Apollo. Spacecraft: Apollo LM.

    Grumman presented to MSC its recommendations for an all-battery electrical power system for the LEM:

    • Two batteries in the ascent stage
    • Four batteries in the descent stage
    • A new power distribution system
    • Active cooling for the descent batteries and electrical control assemblies
    Following a review of cost and resources proposals, MSC approved Grumman's configuration, and on April 15 gave the LEM manufacturer a go-ahead. - Additional details.
1965 - Launch Vehicle: Saturn I. Model: Saturn IB.
  • First stage of the Saturn IB first static firing at MSFC Nation: USA. Program: Apollo.

    The first stage of the Saturn IB booster (the S-IB-1) underwent its first static firing at Huntsville, Alabama. The stage's eight uprated H-1 engines produced about 71,168-kilonewtons (1.6 million lbs) thrust. On April 23, Marshall and Rocketdyne announced that the uprated H-1 had passed qualification testing and was ready for flight.

1965 - Launch Vehicle: HY-1.
  • HY missile development Nation: China.

    Shenguan is authorised to develop and produce a missile based on the Soviet P-15 ('Styx') cruise missile (later designated Haiyang).

1965 - Launch Site: Mountain Home AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1.
  • Last Titan I ICBM taken off alert status at Mountain Home AFB Nation: USA.

1965 - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sonda. Model: Sonda 1. LV Configuration: Sonda 1 1.
  • Test mission Nation: Brazil. Agency: IAE. Apogee: 65 km (40 mi).

1965 - 02:07 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.132NA.
  • Airglow Aeronomy mission Nation: USA. Agency: NASA. Apogee: 139 km (86 mi).

1966 -
  • Voskhod 4 to 6 in jeopardy Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 4, Voskhod 5, Voskhod 6.

    In a meeting of Soviet Ministers, it is revealed that Voskhod s/n 7, 8, and 9 will likely not be completed. Kamanin objects - he wants these flights to be used for manned test of military equipment in space. He does not trust waiting even further for the availability of the untested and unflown 7K-OK spacecraft.

1966 - Launch Site: Cape Canaveral. Launch Complex: LC31B. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 462.
  • Research and development launch Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 - 13:57 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Arcas. Model: Sidewinder-Arcas.
  • AC30.752 Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 103 km (64 mi).

1967 -
  • Manual docking for Soyuz 1/2 Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 1, Soyuz 2A.

    Ustinov reviews the cosmonauts. Kamanin urges that a manual docking be allowed on the Soyuz 1/2 mission - he had argued the same point with Korolev before his death. Komarov say he can accomplish a manual docking from 350 km range (once the Igla automatic system has brought him there from 23 km range). There follows a discussion of an all-female flight. Four female cosmonauts would be assigned to the mission, and Kamanin would need 5 to 6 months to complete there training. The mission is designated 'Voskhod-6'.

1967 - Launch Site: Nenoksa. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-27. Model: Zyb.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 500 km (310 mi).

1967 - Launch Site: Ile du Levant. Launch Complex: -. Launch Pad: CERES. Launch Vehicle: Belenos.
  • Weather mission Nation: France. Agency: SECT. Apogee: 100 km (60 mi).

1967 - 03:40 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.204GG.
  • Ultraviolet stellar photom Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 139 km (86 mi).

1968 - 03:26 GMT - Launch Site: Kerguelen. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 2B. LV Configuration: Dragon 2B D-253.
  • FU-171 VLF / Ions Ionosphere mission Nation: France. Agency: CNES. Apogee: 416 km (258 mi).

1969 - 04:38 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB ADD-VB-23.
  • VUV auroral Aurora mission Nation: Canada. Agency: NRCC. Apogee: 372 km (231 mi).

1969 - 09:54 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 5C. LV Configuration: Skylark-5C SL724.
  • X-ray Survey X-ray astronomy mission Nation: UK. Agency: BAC. Apogee: 192 km (119 mi).

1969 - 19:30 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12.
  • Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 181 km (112 mi).

1971 - 02:57 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta E1. LV Configuration: Thor Delta E1 491/D84.
  • Isis 2 Nation: Canada. Payload: Isis B. Mass: 264 kg (582 lb). Class: Earth. Type: Magnetosphere. Spacecraft: Isis. Agency: CRC. Perigee: 1,358 km (843 mi). Apogee: 1,424 km (884 mi). Inclination: 88.20 deg. Period: 113.60 min. COSPAR: 1971-024A. USAF Sat Cat: 5104.

    Ionospheric research. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B).

1971 - 08:40 GMT - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2.
  • OT GT82M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 - 11:29 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 402 Nation: USSR. Program: RORSAT. Mass: 3,800 kg (8,300 lb). Class: Surveillance. Type: Naval Radarsat. Spacecraft: US-A. Agency: MO SSSR. Perigee: 965 km (599 mi). Apogee: 1,011 km (628 mi). Inclination: 65.00 deg. Period: 104.90 min. COSPAR: 1971-025B. USAF Sat Cat: 5107. Decay Date: 1971-05-06.

    Ocean surveillance; probably used chemical batteries.

1972 - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Temp-2S.
  • Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1972 - 03:47 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NRL NB3.254.
  • Astronomy mission Nation: USA. Agency: NRL. Apogee: 200 km (120 mi).

1972 - 05:05 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.27CG.
  • X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1974 - 22:37 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P174H.
  • Atomic oxygen Atmospheric mission Nation: UK. Agency: SRC. Apogee: 142 km (88 mi).

1974 - 22:56 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P178H.
  • Atomic oxygen Atmospheric mission Nation: UK. Agency: SRC. Apogee: 134 km (83 mi).

1975 - 12:30 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8A92M.
  • Meteor 1-21 Nation: USSR. Payload: Meteor M no. 21. Mass: 3,800 kg (8,300 lb). Class: Earth. Type: Weather. Spacecraft: Meteor M. Agency: MOM. Perigee: 853 km (530 mi). Apogee: 884 km (549 mi). Inclination: 81.20 deg. Period: 102.30 min. COSPAR: 1975-023A. USAF Sat Cat: 7714.

    Acquisition of meteorological information needed for use by the weather service.

1976 - 08:05 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Sounding Rocket. LV Configuration: Sergeant IC630.02-1A.
  • ICECAP 76 HIRIS Auroral mission Nation: USA. Agency: DNA/AFCRL. Apogee: 130 km (80 mi).

1976 - 09:28 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Hydac. LV Configuration: HJ Hydac ARPA WS650.27-1.
  • Ballistics test Nation: USA. Agency: ARPA. Apogee: 150 km (90 mi).

1977 -
  • Lower forward fuselage on dock, Palmdale (STA-099) Nation: USA. Program: STS.

1979 -
  • Intercosmos Cosmonaut Training Group selected. Nation: Vietnam.

    Training group of potential Vietnamese 'guest cosmonauts' for propaganda flights to the Salyut space station. The 'guests', from states allied to the Soviet Union, would be flown on Soyuz lifeboat changeout missions to the station.

1979 - 10:31 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Taurus Tomahawk. LV Configuration: Taurus Tomahawk NASA 12.1004UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).

1980 - Launch Vehicle: Shuttle.
  • Shuttle ejection seat tests Nation: USA.

    Another series of tests of the shuttle ejection seat are held at Holloman AFB in support of the first shuttle orbital flights.

1980 - 08:00 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1170 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MKM. Agency: MOM. Perigee: 178 km (110 mi). Apogee: 379 km (235 mi). Inclination: 70.40 deg. Period: 90.10 min. COSPAR: 1980-025A. USAF Sat Cat: 11747. Duration: 11.00 days. Decay Date: 1980-04-12.

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

1980 - 12:36 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4.
  • OT-2 Operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1981 - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 3.
  • FOT GT75GM-2 Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1981 - 09:04 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Taurus Tomahawk. LV Configuration: Taurus Tomahawk NASA 34.04UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 500 km (310 mi).

1981 - 09:10 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4.
  • DASO-7? demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1983 -
  • Strategic Air Command (SAC) transferred Peterson AFB, Colorado, to Space Command. Nation: USA.

1984 - Launch Site: Gitdaeryung. Launch Complex: -. Launch Pad: -. Launch Vehicle: R-17. Model: Hwasong 5.
  • Test mission Nation: Korea North. Agency: DPRK. Apogee: 200 km (120 mi).

1984 - 07:19 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 10. LV Configuration: Black Brant X NASA 35.008GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 954 km (592 mi).

1985 - 16:57 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Orion. LV Configuration: Nike Orion NASA 31.47GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1986 - 08:17 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 10. LV Configuration: Black Brant X NASA 35.015GE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 912 km (566 mi).

1988 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1988 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1988 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1988 - 20:19 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon.
  • Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1992 - 14:18 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 2182 Nation: Russia. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-4K1. Agency: MOM. Perigee: 166 km (103 mi). Apogee: 284 km (176 mi). Inclination: 67.10 deg. Period: 89.00 min. COSPAR: 1992-016A. USAF Sat Cat: 21920. Duration: 59.00 days. Decay Date: 1992-05-30.

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

1993 - 18:57 GMT - Launch Site: Plesetsk. Launch Complex: LC133/3. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47178-431.
  • Cosmos 2239 Nation: Russia. Mass: 825 kg (1,818 lb). Class: Navigation. Spacecraft: Parus. Agency: MO RF. Perigee: 966 km (600 mi). Apogee: 997 km (619 mi). Inclination: 82.90 deg. Period: 104.70 min. COSPAR: 1993-020A. USAF Sat Cat: 22590.

    Military navigation satellite. Positioned in plane 4 of constellation. Replaced Cosmos 2173.

1994 -
  • Energia Engineer Cosmonaut Training Group 12 selected. Nation: Russia.

1995 - 09:33 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.104UL.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 156 km (96 mi).

1998 - 13:35 GMT -
  • EVA Mir EO-25-2 Nation: Russia. Program: Mir. Class: Manned. Type: Space station. Spacecraft: Mir. Crew: Musabayev, Budarin. Flight: Mir NASA-6, Mir EO-25. EVA Duration: 0.28 days.

    The Kvant-2 hatch had been fixed from within and was used for the EVA. Objective was to repair the damaged Spektr solar panel. Handrails were installed near the panel but the crew could not complete the work before the scheduled time ran out.

1999 - Launch Site: Barents Sea Launch Area. Launch Complex: -. Launch Pad: 69.5 N x 34.2 E. Launch Vehicle: R-29. Model: Volna.
  • Operational test Nation: Russia. Agency: VMF RF. Apogee: 1,000 km (600 mi).

2002 - 22:07 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Cosmos 2388 Nation: Russia. Mass: 1,900 kg (4,100 lb). Class: Early Warning. Spacecraft: Oko. Manufacturer: NPO Lavochkin. Agency: KVR. Perigee: 519 km (322 mi). Apogee: 39,178 km (24,344 mi). Inclination: 62.93 deg. COSPAR: 2002-017A. USAF Sat Cat: 27409.

    The Blok-I upper stage and Oko satellite were placed in a 231 x 490 km x 62.8 deg parking orbit. Following the stage burn the Lavochkin US-KS (Oko) elliptical orbit early warning satellite built by Lavochkin was not tracked immediately, but later was reported to be in the correct standard orbit.

2004 -
  • Genesis, End of Science Collection Nation: USA. Spacecraft: Genesis.


Born on this day in:
  • 1911 - Ernst Helmut Merk.  German Rocket engineer. Birth City: Berlin. Birth Country: Germany.
  • 1914 - Mortimer Rosenbaum.  American Engineer. Birth City: Plainfield. Birth State: New Jersey. Birth Country: USA.
  • 1946 - Dr William Frederick Fisher.  American Mission Specialist Astronaut. Birth City: Dallas. Birth State: Texas. Birth Country: USA.

Died on this day in:
  • 1967 - Holger N Toftoy.  American Manager.
  • 1969 - Kurt Paul Erich Patt.  German Rocket engineer.
  • 1973 - Bruno Heusinger.  German Rocket engineer.

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2008 except where otherwise noted.