Encyclopedia Astronautica
May 09


May 09 Chronology


1913 May 9 - .
  • Birth of Albert Franz Zeiler - . Nation: Germany; USA. Summary: German-American engineer in WW2, member of the Rocket Team in the United States thereafter. German expert in guided missiles during WW2. As of January 1947, working at Fort Bliss, Texas. Died in Florida..

1914 May 9 - .
  • Birth of Werner Tiller - . Nation: Germany; USA. Summary: German engineer in WW2, member of the Rocket Team in the United States thereafter..

1914 May 9 - .
  • Birth of Ernst E Klaus - . Nation: Germany; USA. Summary: German engineer in WW2, member of the Rocket Team in the United States thereafter..

1915 May 9 - .
1931 May 9 - .
  • Birth of Vance DeVoe Brand - . Nation: USA. Summary: American test pilot astronaut. Flew on Apollo (ASTP), STS-5, STS-41-B, STS-35..

1937 May 9 - . Launch Vehicle: ARS.
  • Pierce rocket reaches 80 m - . Nation: USA. Apogee: 0.0800 km (0.0497 mi). Summary: H. F. Pierce of the American Rocket Society launched a liquid propellant rocket to 80-m altitude at Old Ferris Point, N.Y..

1944 May 9 - . Launch Site: Heidelager. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 17333. FAILURE: Failed.
1945 May 9 - . Launch Vehicle: V-3.
  • V-3 complex at Mimoyecques blown up by British Forces - . Nation: Germany. Summary: The action was taken to prevent the French from using the facility against Britain at some future date..

1949 May 9 - .
1949 May 9 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Wac. Launch Vehicle: WAC B. LV Configuration: WAC B 9B.
  • Test mission - . Nation: USA. Agency: USA OR. Apogee: 40 km (24 mi).

1951 May 9 - . LV Family: R-1. Launch Vehicle: R-1.
  • Plant 586 in Dnepropetrovsk to convert to missile production (future NPO Yuzhnoye). - . Nation: USSR. Summary: Decree 'On the Transfer of the Dnepropetrovsk Automobile Plant From the Ministry of Automobile and SM Tractor Industry to the Ministry of Armaments--transfer of Dnepropetrovsk Plant No. 586 into the Ministry of Armaments for missile production' was issued.

1954 May 9 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1342T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1955 May 9 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1600T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1956 May 9 - . Launch Site: Wallops Island. LV Family: Nike. Launch Vehicle: Nike.
  • Avro Arrow Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1957 May 9 - . Launch Site: Vandenberg.
  • Start of new construction. - . Nation: USA. Summary: Start of new construction and major rehabilitation at Camp Cooke..

1959 May 9 - . LV Family: Atlas. Launch Vehicle: Atlas Vega.
  • High-resolution photographs of the moon using Vega rocket - . Nation: USA. Related Persons: Rosen, Milton. Program: Apollo. Spacecraft: Lunar Orbiter. Milton W. Rosen of NASA Headquarters proposed a plan for obtaining high-resolution photographs of the moon. A three-stage Vega would place the payload within a 500-mile diameter circle on the lunar surface. A stabilized retrorocket fired at 500 miles above the moon would slow the instrument package sufficiently to permit 20 photographs to be transmitted at a rate of one picture per minute. Additional Details: High-resolution photographs of the moon using Vega rocket.

1959 May 9 - . 18:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: R-7. LV Configuration: R-7 No. IZ-21. FAILURE: Failure.
  • GCh No. 17 (III) test - . Nation: USSR. Agency: MVS. Apogee: 1,000 km (600 mi). Summary: R-7 development test flight. (GCh No. 17 (III)).

1960 May 9 - .
  • Mercury Pad Abort 1 - . Nation: USA. Program: Mercury. Spacecraft: Mercury; Mercury Escape Tower. McDonnell's first production spacecraft, with its escape rocket serving as the propulsion force, was launched from Wallops Island. Designated the beach-abort test, the objectives were a performance evaluation of the escape system, the parachute and landing system, and recovery operations in an off-the-pad abort situation. The test was successful.

1960 May 9 - .
  • Elektron satellite approved. - . Nation: USSR. Spacecraft: Elektron-A; Elektron-B. Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On approval of work on the Elektron scientific satellite' was issued. The two spacecraft were designed to be deployed in a single launch of a Vostok booster. The spacecraft had the specific task of mapping the Van Alen radiation belts at higher inclinations than that achieved by US satellites of the time (60 degrees vs 30 degrees latitude). Design work began in July 1960.

1960 May 9 - . Launch Site: Wallops Island.
  • Beach Abort 1 - . Nation: USA. Program: Mercury. Class: Manned. Type: Manned spacecraft. Spacecraft: Mercury. First production model of Project Mercury spacecraft was successfully launched from NASA Wallops Station to test escape, landing, and recovery systems. Known as the "beach abort" shot, the Mercury capsule reached 775 m before parachute landing and pickup by Marine helicopter returned it to Wallops' hangar 17 minutes after launch.

1961 May 9 - . LV Family: Redstone. Launch Vehicle: Redstone MRLV.
  • Kennedy decision to allow MR-3 flight defended. - . Nation: USA. Related Persons: Kennedy. Program: Mercury. Flight: Mercury MR-3. Senator Robert S. Kerr, chairman of the Senate Aeronautical and Space Sciences Committee, told a group at the National Radio and Television Convention that President Kennedy accepted the views of NASA and congressional leaders in approving the manned Mercury-Redstone flight of May 5.

1961 May 9 - . LV Family: Arcas. Launch Vehicle: Arcas-Robin.
  • Arcas-Robin sounding rocket launches. - . Nation: USA. Summary: Twenty-four Arcas-Robin weather sounding rockets fired within 24 hours by AFPGC at Eglin Air Force Base, Fla..

1961 May 9 - . 11:53 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.29GA.
  • Grenade Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 117 km (72 mi).

1961 May 9 - . 12:07 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA5B. LV Family: Black Knight. Launch Vehicle: Black Knight 201/C. LV Configuration: Black Knight-201/C BK.14. FAILURE: Failure.
  • Gaslight Re-entry Vehicle test - . Nation: UK. Agency: RAE. Apogee: 415 km (257 mi).

1962 May 9 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Belier. Launch Vehicle: Belier I. LV Configuration: Belier B02. FAILURE: Failure.
  • Test mission - . Nation: France. Agency: CNES. Apogee: 0 km ( mi).

1963 May 9 - .
  • Cosmonauts Tour Glushko Factory - . Nation: USSR. Related Persons: Glushko; Korolev; Komarov; Khrunov; Alekseyev, Semyon. Flight: Vostok 5. Spacecraft: Sokol SK-1. Victory Day Holiday in the Soviet Union. The cosmonauts toured Glushko's engine factory. Glushko has 11,000 employees at four locations. The resentment between Glushko and Korolev, going back to their time in the Gulag, is apparent. Korolev calls during the tour but Glushko does not return his call. Later Alekseyev contacts Kamanin and proposes that Komarov be the back-up cosmonaut for Vostok 5 rather than Khrunov - because he hasn't finished the suit yet for Khrunov!

1963 May 9 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-14. FAILURE: Failure.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi). Summary: Mk 6 re-entry vehicle..

1963 May 9 - . 18:02 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.97II.
  • CSIRO VLF Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 203 km (126 mi).

1963 May 9 - . 20:06 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 119D / Agena B S01 1206.
  • Midas 7 - . Payload: Midas / Agena TV 1206. Mass: 2,000 kg (4,400 lb). Nation: USA. Agency: USAF. Class: Military. Type: Early warning satellite. Spacecraft: Midas. USAF Sat Cat: 574 . COSPAR: 1963-014A. Apogee: 3,680 km (2,280 mi). Perigee: 3,609 km (2,242 mi). Inclination: 87.3000 deg. Period: 166.40 min. Summary: MIDAS 7 was the first operational MIDAS mission and the first equipped with the W-37 sensor. During its six weeks of operation, MIDAS 7 recorded nine US ICBM launches, including the first missile launch ever detected from space..
  • TRS 2 - . Payload: ERS 5. Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Navigation technology satellite. Spacecraft: TRS. Decay Date: 1973-07-31 . USAF Sat Cat: 579 . COSPAR: 1963-014B. Apogee: 4,902 km (3,045 mi). Perigee: 2,269 km (1,409 mi). Inclination: 87.2000 deg. Period: 165.00 min. Summary: Solar cells damage data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • Dash 1 - . Nation: USA. Agency: USAF. Class: Technology. Type: Military technology satellite. Spacecraft: Dash. USAF Sat Cat: 589 . COSPAR: 1963-014D. Apogee: 3,724 km (2,313 mi). Perigee: 3,558 km (2,210 mi). Inclination: 87.3000 deg. Period: 166.30 min.
  • TRS 3 - . Payload: ERS 6. Mass: 1.00 kg (2.20 lb). Nation: USA. Agency: USAF. Class: Technology. Type: Navigation technology satellite. Spacecraft: TRS. USAF Sat Cat: 608 . COSPAR: 1963-014C. Apogee: 3,691 km (2,293 mi). Perigee: 3,591 km (2,231 mi). Inclination: 87.3000 deg. Period: 166.40 min. Summary: Solar cells damage data. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1965 May 9 - . 07:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M U103-30.
  • Luna 5 - . Payload: E-6 s/n 10. Mass: 1,474 kg (3,249 lb). Nation: USSR. Agency: MOM. Program: Luna. Class: Moon. Type: Lunar probe. Spacecraft: Luna E-6. Decay Date: 1965-05-12 . USAF Sat Cat: 1366 . COSPAR: 1965-036A. Apogee: 219 km (136 mi). Perigee: 159 km (98 mi). Inclination: 64.8000 deg. Period: 88.27 min. Summary: Soft lunar landing attempt. The retrorocket system failed, and the spacecraft impacted the lunar surface at the Sea of Clouds. Western observers, among them England's Sir Bernard Lovell, correctly speculated that the craft's mission was a soft landing..

1966 May 9 - . 15:20 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.106NP.
  • Radar test - . Nation: USA. Agency: NASA. Apogee: 174 km (108 mi). First radar for science purposes launched into space and successfully recovered. Besides testing the engineering and special techniques for space flight, the data showed that the echo characteristics of the earth were similar to those of Venus and the Moon.

1967 May 9 - . 07:20 GMT - . Launch Site: Point Barrow. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.230GM.
  • Grenade Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 120 km (70 mi).

1967 May 9 - . 21:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.192DS.
  • NRL ND3.199 XUV-H3? Solar optical / extreme ultraviolet mission - . Nation: USA. Agency: NRL; NASA. Apogee: 182 km (113 mi).

1967 May 9 - . 21:50 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1E. LV Family: Delta. Launch Vehicle: Thorad Agena D SLV-2G. LV Configuration: Thorad SLV-2G Agena D 508 / Agena D SS-01B 1634. FAILURE: Failure of the booster cut-off switch.. Failed Stage: 1.
  • KH-4A 1041 - . Payload: KH-4A s/n 1041 / Agena D 1634 / OPS 4696. Mass: 2,000 kg (4,400 lb). Nation: USA. Agency: NRO; CIA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-4A. Decay Date: 1967-07-13 . USAF Sat Cat: 2779 . COSPAR: 1967-043A. Apogee: 791 km (491 mi). Perigee: 183 km (113 mi). Inclination: 85.0000 deg. Period: 94.30 min. Summary: KH-4A. Due to the failure of the booster cut-off switch, the satellite went into a highly eccentric orbit. Significant image degradation..
  • OPS 1967 - . Payload: EHH B7. Nation: USA. Agency: USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1993-03-14 . USAF Sat Cat: 2780 . COSPAR: 1967-043xx. Apogee: 145 km (90 mi). Perigee: 131 km (81 mi). Inclination: 84.9000 deg. Period: 87.20 min.
  • SRV 731 - . Payload: SRV 1041-1 / OPS 1967. Mass: 60 kg (132 lb). Nation: USA. Agency: NRO; USAF. Spacecraft: KH-4A. Decay Date: 1993-03-14 . USAF Sat Cat: 2780 . COSPAR: 1967-043B. Apogee: 458 km (284 mi). Perigee: 399 km (247 mi). Inclination: 84.9000 deg. Period: 93.20 min. Summary: Radar monitoring. Due to the failure of the booster cut-off switch, the satellite went into a highly eccentric orbit..

1968 May 9 - . 06:15 GMT - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-114.
  • LRL BOX-14 X-ray astronomy mission - . Nation: USA. Agency: Sandia. Apogee: 178 km (110 mi).

1968 May 9 - . 07:30 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 21.7 N x 33.3 W. Launch Platform: VISE. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 162 km (100 mi).

1969 May 9 - .
  • Science sequence recommended for the Apollo 12 mission - . Nation: USA. Program: Apollo. Flight: Apollo 12. Spacecraft: Apollo ALSEP. NASA Hq. informed MSC that, for planning purposes and Change Control Board action, the following science sequence was being recommended for the Apollo 12 mission:

    1. contingency sample;
    2. ALSEP deployment; and
    3. field geology investigations.
    The message said, "It is important that ALSEP be deployed in the first EVA (extravehicular activity). Then the entire second EVA could be devoted to Field Geology Investigations."

1969 May 9 - .
  • HL-10 Flight 17 - . Crew: Manke. Payload: HL-10 flight 17. Nation: USA. Related Persons: Manke. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: HL-10. Summary: 3 chambers, first supersonic. Maximum Speed - 1197 kph. Maximum Altitude - 16250 m. Flight Time - 410 sec..

1970 May 9 - . 17:30 GMT - . Launch Site: Fort Greely. Launch Vehicle: Rocketsonde.
  • Starute,Datasonde - . Nation: USA. Agency: MRN. Apogee: 59 km (36 mi).

1971 May 9 - . 01:11 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur SLV-3C. LV Configuration: SLV-3C Centaur AC-24 / Centaur D-1A 5405C. FAILURE: Inadvertent Centaur electronic signal shut down stage early.. Failed Stage: 2.
  • Mariner H - . Payload: Mariner 71H. Mass: 996 kg (2,195 lb). Nation: USA. Agency: NASA. Program: Mariner. Class: Mars. Type: Mars probe. Spacecraft: Mariner 8-9. Decay Date: 1971-05-08 . COSPAR: F710509A. Summary: Intended Mars flyby..

1972 May 9 - . 14:03 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • Met Para - . Nation: USA. Agency: MRN. Apogee: 50 km (31 mi).

1973 May 9 - . 23:25 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 655. Launch Vehicle: Poseidon.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1974 May 9 - . 13:00 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1975 May 9 - . Launch Site: Barking Sands. LV Family: Sandhawk. Launch Vehicle: Terrier Sandhawk. LV Configuration: Terrier Sandhawk Sandia.
  • Monitoring mission - . Nation: USA. Agency: Sandia. Apogee: 406 km (252 mi).

1975 May 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-102 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 May 9 - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 HRV. LV Family: Stonechat. Launch Vehicle: Falstaff. LV Configuration: Falstaff F.0.
  • Test mission - . Nation: UK. Agency: RAE. Apogee: 119 km (73 mi).

1976 May 9 - . 16:30 GMT - . Launch Site: White Sands. Launch Vehicle: Rocketsonde.
  • Starute, Datasonde - . Nation: USA. Agency: MRN. Apogee: 66 km (41 mi).

1977 May 9 - . 15:14 GMT - . Launch Site: Antigua. Launch Vehicle: Rocketsonde.
  • - . Nation: USA. Agency: MRN. Apogee: 73 km (45 mi).

1978 May 9 - . 01:14 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 75 km (46 mi).

1979 May 9 - . 18:52 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 90 km (55 mi).

1980 May 9 - . 16:00 GMT - . Launch Site: Kerguelen. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1981 May 9 - . 18:35 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1983 May 9 - . 20:17 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 78 km (48 mi).

1984 May 9 - . 06:30 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.20UH.
  • X-ray astronomy mission - . Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).

1985 May 9 - . 17:00 GMT - . Launch Site: Primrose Lake. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 64 km (39 mi).

1986 May 9 - . 19:04 GMT - . Launch Site: Primrose Lake. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 58 km (36 mi).

1987 May 9 - . 04:00 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 7. LV Configuration: Skylark 7 DLR K-GR-146. FAILURE: Failure.
  • TEXUS 15 Microgravity mission - . Nation: Germany. Agency: DFVLR. Apogee: 252 km (156 mi).

1988 May 9 - . 09:05 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 7. LV Configuration: Skylark 7 DLR K-GR-157.
  • Testflug (BAE 1) test - . Nation: Germany. Agency: DFVLR. Apogee: 262 km (162 mi).

1990 May 9 - . 17:50 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout G. LV Configuration: Scout G-1 S212C.
  • Macsat 1; M-1 - . Payload: MacSat 1. Mass: 68 kg (149 lb). Nation: USA. Agency: DARPA. Class: Communications. Type: Military communications satellite. Spacecraft: Macsat. USAF Sat Cat: 20607 . COSPAR: 1990-043A. Apogee: 753 km (467 mi). Perigee: 602 km (374 mi). Inclination: 89.9000 deg. Period: 98.30 min. Summary: Multiple Access Communications Satellite; global store and forward communications. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..
  • Macsat 2; M-2 - . Payload: MacSat 2. Mass: 68 kg (149 lb). Nation: USA. Agency: DARPA. Class: Communications. Type: Civilian communications satellite. Spacecraft: Macsat. USAF Sat Cat: 20608 . COSPAR: 1990-043B. Apogee: 749 km (465 mi). Perigee: 600 km (370 mi). Inclination: 89.9000 deg. Period: 98.30 min. Summary: Multiple Access Communications Satellite; global store and forward communications. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B)..

1994 May 9 - . 02:47 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout G. LV Configuration: Scout G-1 S218C.
  • MSTI-2 - . Payload: MSTI 2. Mass: 163 kg (359 lb). Nation: USA. Class: Military. Type: Strategic defense satellite. Spacecraft: MSTI. Decay Date: 1998-11-28 . USAF Sat Cat: 23101 . COSPAR: 1994-028A. Apogee: 433 km (269 mi). Perigee: 415 km (257 mi). Inclination: 93.1000 deg. Period: 97.10 min. Summary: Last Scout launch; BMDO technology tests. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1998 May 9 - . 01:38 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan Centaur 401B. LV Configuration: Titan 401B/Centaur 4B-25/TC-18 (K-25).
  • USA 139 - . Payload: Advanced Orion 2. Nation: USA. Agency: NRO; NSA. Manufacturer: El Segundo. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Advanced Orion. USAF Sat Cat: 25336 . COSPAR: 1998-029A. Apogee: 35,800 km (22,200 mi). Perigee: 35,780 km (22,230 mi). Inclination: 0.0000 deg.

2001 May 9 - .
  • ISS Status Report: ISS 01-13 - . Nation: USA. Related Persons: Helms; Voss. Program: ISS. Flight: ISS EO-2. Summary: The International Space Station's Expedition Two crew has turned its attention to the initial checkout of the new robotic arm now that the outpost's command and control computers are working properly.. Additional Details: ISS Status Report: ISS 01-13.

2003 May 9 - . Launch Site: Kagoshima. Launch Complex: Kagoshima M-V. LV Family: M-V. Launch Vehicle: M-V. LV Configuration: M-V-1 M-V-5.
  • Hayabusa - . Payload: MUSES-C. Mass: 500 kg (1,100 lb). Nation: Japan. Agency: ISAS. Class: Asteroids. Type: Asteroid probe. Spacecraft: Hayabusa. Decay Date: 2010-06-13 . USAF Sat Cat: 27809 . COSPAR: 2003-019A. Summary: Asteroid sample return probe launched toward asteroid 1998 SF36. Launch delayed from Nov. 24, 2002, then May 5, 2003..

2007 May 9 - . 05:10 GMT - . Launch Site: Balasore. LV Family: Prithvi. Launch Vehicle: Prithvi.
  • - . Nation: India. Agency: IDRDL. Apogee: 100 km (60 mi).

2008 May 9 - .
  • ISS On-Orbit Status 05/09/08 - . Nation: USA. Related Persons: Kononenko, O D; Reisman; Volkov, Sergey. Program: ISS. Flight: ISS EO-16-3. Off-duty holiday for the crew: Russia's Victory Day, one of the most sacred national holidays for the Russian people, commemorating the dozens of millions of their countrymen fallen in the Great Patriotic War (World War II).

    FE-2 Reisman began the day with the periodic (monthly) CSA-CP (Compound Specific Analyzer-Combustion Products) maintenance/checkout, today changing out the battery on the prime unit. (The CSA-CP is a passive cabin atmosphere monitor that provides quick response capability during a combustion event (fire). Its collected data are stored on a logger. After replacing the battery with a new one (#1119), Garrett zero-calibrated the instrument (to eliminate drift in the combustion sensors), then redeployed the prime unit at the SM (Service Module) Central Post.) Additional Details: ISS On-Orbit Status 05/09/08.


2008 May 9 - .
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