Encyclopedia Astronautica
April 10


April 10 Chronology


1900 April 10 - .
  • Birth of Arnold O Beckman - . Nation: USA. Summary: American engineer, inventor and manufacturer of various analytical instruments..

1919 April 10 - .
  • Birth of John C Houbolt - . Nation: USA. Summary: American engineer, at NASA 1945-1985. Claimed to have discovered bur certainly promoted the lunar orbit rendezvous strategy used for Apollo..

1945 April 10 - .
  • Birth of Eric Edward Sundberg - . Nation: USA. Summary: American engineer military spaceflight engineer astronaut, 1979-1985. Later stationed at Pentagon. Retired from USAF in August 1997. Later with NRO..

1947 April 10 - .
  • XS-1 Flight 27 - . Crew: Goodlin. Payload: XS-1 # 1 flight 11. Nation: USA. Related Persons: Goodlin. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: Bell flight 11. Glide flight and stall check. At Muroc Dry Lake, California..

1952 April 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Vehicle: Lark. LV Configuration: Lark 602. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 0 km ( mi).

1953 April 10 - .
  • X-1A Flight 5 - . Crew: Ziegler. Payload: X-1A flight 5. Nation: USA. Related Persons: Ziegler. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1A. Summary: Bell flight 5. Pilot noted low-frequency elevator buzz at mach 0.93, did not proceed above this speed, pending buzz investigation..

1954 April 10 - . LV Family: R-5. Launch Vehicle: R-5M.
  • OKB-586 founded and nuclear-tipped R-5M IRBM development authorised. - . Nation: USSR. Related Persons: Kozlov. Council of Soviet Ministers (SM) Decree 'On approval of work on the R-5M missile and on establishment of OKB-586 at Dnepropetrovsk Plant No. 586' was issued. Sadoviy and Kozlov were named to lead the project. Based substantially on the R-5, it used the 8U25 launch portable launch stand.

1955 April 10 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1572T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1957 April 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1959 April 10 - .
  • Mercury escape-motor canting-angle tests completed at Wallops Island. - . Nation: USA. Program: Mercury. Spacecraft: Mercury; Mercury Escape Tower. Summary: Escape-motor canting-angle tests were completed at Wallops Island. Tests were conducted in 5 degree increments between 10 degrees to 30 degrees, and visually it appeared stability was better at the larger angle..

1961 April 10 - .
  • Joint meeting of the Apollo Technical Liaison Groups was held at STG - . Nation: USA. Program: Apollo. A joint meeting of the Apollo Technical Liaison Groups was held at STG. NASA Headquarters and STG representatives briefed members of the Groups on the status of the Apollo program. The individual Liaison Groups were asked to reexamine the Apollo guidelines in the light of NASA and contractor studies conducted during the past year and to help gather detailed technical information for use as background material in the preparation of the Apollo spacecraft specification.

1962 April 10 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: Kosmos 2. Launch Vehicle: R-12.
  • - . Nation: Ukraine. Agency: MVS. Apogee: 402 km (249 mi).

1963 April 10 - .
  • Link to build Apollo lunar mission simulators - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Simulator. North American awarded a $9.5 million letter contract to the Link Division of General Precision, Inc., for the development and installation of two spacecraft simulators, one at MSC and the other at the Launch Operations Center. Except for weightlessness, the trainers would simulate the entire lunar mission, including sound and lighting effects.

1963 April 10 - . 20:33 GMT - . Launch Site: ETR Launch Area. Launch Platform: EAG-154. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3X-14. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 0 km ( mi).

1964 April 10 - . Launch Site: Wallops Island. LV Family: RAM. Launch Vehicle: RAM B. LV Configuration: RAM B RAM B-3.
  • RAM B-3 re-entry vehicle test flight - . Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).

1964 April 10 - . 06:30 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.121GE.
  • Auroral emissions Aurora mission - . Nation: USA. Agency: NASA. Apogee: 172 km (106 mi).

1965 April 10 - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78. LV Configuration: Molniya 8K78 R103-26. FAILURE: Stage 3's engine 8D715K failed due to depressurization of the nitrogen pipeline of the LOX tank pressurization system of Block I.. Failed Stage: 3.
  • Luna failure - stage 3 engine failure. - . Payload: E-6 s/n 8. Nation: USSR. Agency: RVSN. Program: Luna. Class: Moon. Type: Lunar probe. Spacecraft: Luna E-6. Decay Date: 1965-04-10 . COSPAR: F650410A. Summary: The upper stages fell apart on re-entry into the atmosphere...

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

1966 April 10 - . LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton 8K82K.
  • Cosmonaut training for lunar flights announced - . Nation: USSR. Related Persons: Leonov. Program: Lunar L1. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-L1. Summary: Leonov announces that cosmonauts are in training for lunar missions..

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

1967 April 10 - . 20:14 GMT - . Launch Site: Kiruna. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.331IE.
  • DLR K-NA-4 Aurora / barium release mission - . Nation: USA. Agency: NASA. Apogee: 230 km (140 mi).

1967 April 10 - . 21:00 GMT - . Launch Site: Point Barrow. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.227GM.
  • Grenade Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 120 km (70 mi).

1968 April 10 - .
  • Cosmonauts occupied with Gagarin crash investigation - . Nation: USSR. Related Persons: Gagarin. Program: Soyuz. No cosmonauts will be sent to witness the next series of unmanned Soyuz flights beginning on 14 April. All cosmonaut staff efforts are concentrated on the Gagarin crash investigation. Kamanin notes the flight of Apollo 6. According to his information the first manned Apollo flight will take place in May-October 1968, and the first American moon landing by the end of 1969.

1968 April 10 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 630. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 April 10 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 630. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 April 10 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 630. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 April 10 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 630. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 April 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1411.
  • ST Olympic T. B-2 operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1969 April 10 - . 15:00 GMT - . Launch Site: Thule AFB. Launch Vehicle: Rocketsonde.
  • Met Para, Arcasonde - . Nation: USA. Agency: MRN. Apogee: 53 km (32 mi).

1970 April 10 - .
  • Documentary film on the Soyuz 6-7-8 missions - . Nation: USSR. Program: Soyuz. Flight: Soyuz 6; Soyuz 7; Soyuz 8. Summary: Kamanin previews the documentary film 'Launch after Launch' on the Soyuz 6-7-8 missions..

1970 April 10 - . 16:30 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 625. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3E. FAILURE: Failure.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 10 km (6 mi).

1971 April 10 - .
  • Old Comrades toast Gagarin's memory. - . Nation: USSR. Summary: -6 deg C at Baiknur, 5 m/s wind. A party of the 'old comrades' is held in Leninsk to commemorate the tenth anniversary of Gagarin's launch..

1972 April 10 - . 15:00 GMT - . Launch Site: Thule AFB. Launch Vehicle: Rocketsonde.
  • Met Para, AN/DMQ-9 - . Nation: USA. Agency: MRN. Apogee: 61 km (37 mi).

1973 April 10 - . 06:59 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.91DG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 198 km (123 mi).

1974 April 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Titan. Launch Vehicle: Titan 3D. LV Configuration: Titan IIID 23D-9.
  • KH-9 no. 08 Capsule - . Payload: P 73-7 / OPS 4547. Mass: 60 kg (132 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-9. USAF Sat Cat: 7244 . COSPAR: 1974-020xx. Apogee: 830 km (510 mi). Perigee: 786 km (488 mi). Inclination: 94.6000 deg. Period: 101.10 min. Summary: Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • KH-9 no. 08 - . Mass: 13,300 kg (29,300 lb). Nation: USA. Agency: NRO; CIA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-9. Decay Date: 1974-07-28 . USAF Sat Cat: 7242 . COSPAR: 1974-020A. Apogee: 285 km (177 mi). Perigee: 153 km (95 mi). Inclination: 94.5000 deg. Period: 88.90 min. Summary: KH-9 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • S73-7 Cal Balloon - . Nation: USA. Agency: USAF AFSC. Spacecraft: S73-7 Cal Balloon. Decay Date: 1974-07-28 . USAF Sat Cat: 7242 . COSPAR: 1974-020xx. Apogee: 247 km (153 mi). Perigee: 148 km (91 mi). Inclination: 94.4000 deg. Period: 88.50 min.
  • OPS 4547 - . Payload: SSF-B No. 25 / OPS 6935. Mass: 60 kg (132 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1980-02-22 . USAF Sat Cat: 7247 . COSPAR: 1974-020C. Apogee: 531 km (329 mi). Perigee: 503 km (312 mi). Inclination: 94.0000 deg. Period: 95.00 min. Summary: Radar monitoring..

1975 April 10 - . 04:40 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170A. LV Configuration: Aerobee 170A NASA 13.88GG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 176 km (109 mi).

1975 April 10 - . 09:54 GMT - . Launch Site: Fort Churchill. LV Family: Tomahawk Sandia. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.302-3.
  • AEOLUS Release, Sphere Aeronomy mission - . Nation: USA. Agency: USAF CRL. Apogee: 216 km (134 mi).

1975 April 10 - . 09:54 GMT - . Launch Site: Fort Churchill. LV Family: Tomahawk Sandia. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk CRL A10.302-4.
  • AEOLUS Release Aeronomy mission - . Nation: USA. Agency: USAF CRL. Apogee: 219 km (136 mi).

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

1976 April 10 - . 15:00 GMT - . Launch Site: Kerguelen. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 88 km (54 mi).

1978 April 10 - . 21:40 GMT - . Launch Site: Eareckson. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 61 km (37 mi).

1979 April 10 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle Enterprise delivered to Kennedy Space Centre - . Nation: USA. The decision was taken not to convert the Enterprise to a flight orbiter due to the numerous structural design changes made since its construction. Static test article OV-099 would be used for that instead. So Enterprise became a pathfinder vehicle at Cape Canaveral to verify fit and handling of ground facilities in the Vertical Assembly Building and LC39.

1979 April 10 - .
  • Ferry flight, MSFC to KSC - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Ferry flight, shuttle carrier aircraft/Enterprise (OV-101) from MSFC to KSC (1 hour, 52 minutes).

1979 April 10 - . 17:34 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
1980 April 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES STREP-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 April 10 - . 05:06 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1982 April 10 - . 06:47 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 3910/PAM. LV Configuration: Delta 3910/PAM 647/D161.
  • Insat 1A - . Mass: 1,152 kg (2,539 lb). Nation: India. Agency: ISRO. Program: Insat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Insat 1. Completed Operations Date: 1982-09-04 . USAF Sat Cat: 13129 . COSPAR: 1982-031A. Apogee: 35,829 km (22,263 mi). Perigee: 35,734 km (22,204 mi). Inclination: 13.3000 deg. Period: 1,435.80 min. Also carried transponders for domestic communications. Operational multipurpose satellite for telecommunications, meteorological, imaging and data relay, radio and television programme distribution and direct television broadcasting for community reception. Geosynchronous orbit longitude 74 E. A/AC.105/INF.391 was reissued as ST/SG/SER.E/79. Also registered by the United States as 1982-31A in ST/SG/SER.E/67, with category C and orbital parameters 1416.7 min, 35032 x 35783 km x 0.5 deg. Positioned in geosynchronous orbit at 73 deg E in 1982 As of 29 August 2001 located at 82.99 deg E drifting at 0.337 deg W per day. As of 2007 Mar 10 located at 39.55E drifting at 0.205W degrees per day.

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

1984 April 10 - . 14:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1548 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 45.00 days. Decay Date: 1984-05-25 . USAF Sat Cat: 14902 . COSPAR: 1984-036A. Apogee: 331 km (205 mi). Perigee: 165 km (102 mi). Inclination: 67.2000 deg. Period: 89.50 min. Summary: High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1985 April 10 - . 13:30 GMT - . Launch Site: Ascension. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 62 km (38 mi).

1986 April 10 - . 02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P. LV Configuration: MT-135P-R598.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 60 km (37 mi).

1987 April 10 - . 08:30 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: BUGAEV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 59 km (36 mi).

1988 April 10 - . 10:06 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: PRILIV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 57 km (35 mi).

1989 April 10 - . 08:21 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna MRL. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX MASER 3.
  • MASER 3 Microgravity mission - . Nation: Sweden. Agency: SSC. Apogee: 297 km (184 mi).

1991 April 10 - . 11:00 GMT - . Launch Site: Barking Sands. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 93 km (57 mi).

1992 April 10 - . 03:20 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 D208.
  • USA 80 - . Payload: GPS 2A-13 / GPS SVN 28. Mass: 1,816 kg (4,003 lb). Nation: USA. Agency: USAF. Manufacturer: Seal Beach. Program: Navstar. Class: Navigation. Type: Navigation satellite. Spacecraft: GPS Block 2 and 2A. USAF Sat Cat: 21930 . COSPAR: 1992-019A. Apogee: 20,277 km (12,599 mi). Perigee: 20,082 km (12,478 mi). Inclination: 54.5000 deg. Period: 717.90 min. Summary: Global Positioning System. Retired 15 August 1997..

1992 April 10 - . 06:30 GMT - . Launch Site: Zingst. Launch Vehicle: MMR-06.
  • MMR06-M Zingst launch 62 - . Nation: Russia. Agency: GMS. Apogee: 67 km (41 mi). Summary: Successful. Earth impacted at 4054 seconds. Reached 66.7 km. .

1997 April 10 - . 13:40 GMT - . Launch Site: Ascension. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 45 km (27 mi).

2002 April 10 - .
  • Yuji Hyakutake Dies At 51 - . Nation: Japan.

2003 April 10 - .
  • Starchaser 5 capsule shipped to America. - . Nation: UK. Program: X-Prize. Spacecraft: Starchaser 5. Summary: Starchaser Industries (Hyde, England, UK) publicly unveils the Nova mark II capsule in Florida. The parachutes will be fitted in Florida before shipping the capsule over to Arizona for drop tests..

2008 April 10 - .
  • ISS On-Orbit Status 04/10/08 - . Nation: USA. Related Persons: Kononenko, O D; Love; Malenchenko; Reisman; Volkov, Sergey; Whitson; Yi So-yeon. Program: ISS. Flight: ISS EO-16; ISS EO-16-3; ISS EO-17; ISS EP-14; STS-122; STS-124. The ISS crew's work/sleep cycle shifted this morning, from wakeup at 2:00am to 5:00am EDT (sleeptime tonight at 9:30pm, from 5:30pm).

    Work period will shift again tomorrow (6:20am -5:50pm) and on 4/12 (2:10am -5:40pm).


    Yest kasaniya! Soyuz TMA-12/16S docked smoothly at the DC1 port at 8:57am EDT, five minutes ahead of time, with Expedition 17 crewmembers CDR Sergei Volkov and FE-1 Oleg Kononenko, plus Korean SFP (Spaceflight Participant) So-Yeon Yi, 14th Visiting Crewmember (VC). After about 1.5 hrs spent in Soyuz on pre-transfer activities, the crew opened hatches, followed by crew transfer, the traditional joyful welcome event and the installation of the BZV QD (quick disconnect) clamps by Volkov and Kononenko at ~12:10pm. (After successful "kasaniya" (contact), automatic "sborka" (closing of Soyuz & DC1 port hooks & latches) took place shortly thereafter (~9:07am) while ISS was in free drift. Attitude control authority had been handed over to the Russian MCS (Motion Control System) at ~5:25am and was returned to US CMG control at ~10:05am. For the 16S docking, Russian thrusters were disabled during Soyuz volume pressurization and clamp installation; they were afterwards returned to active attitude control (~12:30pm). Before hatch opening, the crew performed leak checks of the Soyuz modules and the Soyuz/ISS interface vestibule. They then doffed their Sokol suits and set them up for drying (~1:05pm), deactivated the Atmosphere Purification Unit (BOA) in the Descent Module (SA), replaced the Soyuz ECLSS LiOH cartridges, equalized Soyuz/ISS pressures, and put the spacecraft into conservation mode on ISS integrated power.) Additional Details: ISS On-Orbit Status 04/10/08.


2009 April 10 - . 08:10 GMT - . Launch Site: Plesetsk. LV Family: Topol. Launch Vehicle: Topol.
  • Topol Test - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi). Summary: Op Test.

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