Encyclopedia Astronautica
June 24


June 24 Chronology


1912 June 24 - .
  • Birth of Helmut Horn - . Nation: Germany; USA. Summary: German engineer in WW2, member of the Rocket Team in the United States thereafter..

1913 June 24 - .
1928 June 24 - .
1943 June 24 - . Launch Site: Peenemuende. Launch Complex: Peenemuende P7. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-030.
  • V-2 4030 - . Nation: Germany. Agency: Wehrmacht. Summary: Burnout at T+65s; Flight duration 318 seconds. Range 287 km .

1944 June 24 - . Launch Site: Heidelager. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 18072. FAILURE: Failed.
1946 June 24 - .
  • Birth of Ellison Shoji Onizuka - . Nation: USA. Summary: American test engineer mission specialist astronaut. Flew on STS-51-C, STS-51-L. Died in Challenger accident..

1948 June 24 - .
  • Berlin blockade begins - . Nation: Germany.

1951 June 24 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1. LV Configuration: R-1 IIIB-8.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1952 June 24 - .
  • NACA to increase research on flight to 50 miles/Mach 10. - . Nation: USA. Spacecraft: X-15A. The NACA Committee on Aerodynamics recommended that NACA increase its research efforts on the problem of manned and unmanned flight at altitudes between 12 and 50 miles and at speeds of mach 4 through 10. As a result of this recommendation, the Langley Aeronautical Laboratory began preliminary studies on this project and immediately identified several problem areas. Two of these areas were aerodynamic heating and the achievement of stability and control at very high altitudes and speeds. Of the two, Langley considered aerodynamic heating to be the more serious, and, until this problem was resolved, the design of practical spacecraft impractical.

1954 June 24 - .
  • Birth of Craig Anton Puz - . Nation: USA. Summary: American engineer military spaceflight engineer astronaut, 1982-1990..

1954 June 24 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1448E.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1955 June 24 - . 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 305.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1955 June 24 - . 18:04 GMT - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Nike Deacon.
  • DAN-2 Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 105 km (65 mi). Summary: First Nike-Deacon sounding rocket launched at Wallops Island in cooperative USAF-NACA program of upper air density measurements..

1957 June 24 - .
  • X-1B Flight 19 - . Crew: McKay. Payload: X-1B flight 19. Nation: USA. Related Persons: McKay. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1B. Summary: NACA flight 9. Supersonic maneuvers to mach 1.5 at 18300 m to determine the dynamic and static stability and control characteristics..

1958 June 24 - .
  • Birth of Frederic Patat - . Nation: France. Summary: French physician payload specialist astronaut, 1985-1998. Degree in Acoustic Physics from the University of Paris (1981). Ph.D. in engineering (1984). Doctorate of medicine, 1991. Worked at the medical faculty of the University of Tours..

1958 June 24 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25A. LV Family: X-17. Launch Vehicle: X-17. LV Configuration: X-17 1-204-14.
  • Re-entry Vehicle test - . Nation: USA. Agency: USN. Apogee: 100 km (60 mi).

1959 June 24 - . LV Family: Redstone. Launch Vehicle: Redstone MRLV.
  • Eight Mercury Redstone launch vehicles final cost $20.1 million. - . Nation: USA. Program: Mercury. Summary: Against an original estimated cost of $15.5 million for eight Redstone launch vehicles in support of Project Mercury, the final negotiated figure was $20.1 million..

1959 June 24 - . 12:10 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 AA3.220C.
  • Ionosphere mission - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1960 June 24 - . Launch Site: Kapustin Yar. LV Family: R-2. Launch Vehicle: R-2A.
  • Carried dogs, final operational R-2A launch. - . Nation: USSR. Agency: Korolev. Apogee: 212 km (131 mi).

1960 June 24 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I G-10.
  • RVX-4 test - . Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi).

1960 June 24 - . 06:25 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.06GG.
  • Ultraviolet star photometer Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 211 km (131 mi).

1961 June 24 - . 03:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC19. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I M-1. FAILURE: Failure.
  • Mk 4 re-entry vehicle test - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1961 June 24 - . 23:17 GMT - . Launch Site: Wallops Island. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.15AI.
  • Topside Sounder Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 1,018 km (632 mi).

1963 June 24 - .
  • Controversy over Tereshkova's performance - . Nation: USSR. Related Persons: Tereshkova; Korolev; Bykovsky; Keldysh; Tyulin; Yazdovskiy. Flight: Vostok 6; Vostok 5. The cosmonauts are prepared by Keldysh, Tyulin, and Korolev for their first big press conference. Yazdovskiy has inserted a paragraph in the official press release about Tereshkova's poor emotional state while in space. He claims she experienced overwhelming emotions, tiredness, and a sharply reduced ability to work and complete all of her assigned tasks. Kamanin takes him aside and asks him not to exaggerate her difficulties during the flight. She only had tasks assigned for the first day. When the flight was extended for a second, and then a third day, there was essentially nothing for her to do. The ground command did nothing to support her during those additional days. She certainly was never tired, never objected, but rather did all she could to complete fully the flight program.

1963 June 24 - .
  • Manned Orbital Research Laboratory concept contracts. - . Nation: USA. Spacecraft: MORL. LaRC Director Floyd L. Thompson announced that two aerospace firms, The Boeing Company of Seattle and Douglas Aircraft Company, Inc., of Santa Monica, had been selected for final negotiations for study contracts of a Manned Orbital Research Laboratory (MORL) concept. Additional Details: Manned Orbital Research Laboratory concept contracts..

1963 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 610. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 610. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 610. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 610. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 610. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 610. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 June 24 - . 19:00 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2. LV Configuration: Black Brant II CC-2A-18.
  • Test mission - . Nation: Canada. Agency: CARDE. Apogee: 171 km (106 mi).

1963 June 24 - . 23:00 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2. LV Configuration: Black Brant II CC-2A-17.
  • Test mission - . Nation: Canada. Agency: CARDE. Apogee: 162 km (100 mi).

1964 June 24 - . LV Family: Atlas. Launch Vehicle: Atlas Agena D SLV-3.
  • Construction of Gemini-Agena facilities at complex 14 was completed. - . Nation: USA. Summary: General Dynamics finished the installation and checkout of equipment in the Launch Operations Building on July 20. Lockheed equipment in the Launch Operations Building was installed and checked out by July 31..

1964 June 24 - . 04:42 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC67/22. LV Family: Tsiklon. Launch Vehicle: R-36 8K67.
  • Kura state trials missile launch - . Nation: USSR. Agency: RVSN. Apogee: 874 km (543 mi).

1965 June 24 - .
  • Proposal to launch Gemini around the moon - . Nation: USA. Spacecraft: Gemini - Double Transtage. Gemini contractors proposed to launch a refurbished, modified Gemini around the moon by April 1967 for $ 350 million. The Titan 2-launched Gemini would rendezvous and dock with a Titan 3C-launched 'Double Transtage', which would propel the Gemini into a circumlunar trajectory. McDonnell-Douglas and Martin Marrietta's proposal was suppressed by NASA as a threat to the Apollo program.

1965 June 24 - . Launch Site: Reggane. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C86.
  • Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi).

1965 June 24 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C83.
  • Sodium release Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi).

1965 June 24 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. Launch Pad: Bacchus?. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C74.
  • TMA Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi).

1965 June 24 - . Launch Site: Ile du Levant. Launch Pad: CERES. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C84.
  • TMA Aeronomy mission - . Nation: France. Agency: CNES. Apogee: 150 km (90 mi).

1965 June 24 - . 06:07 GMT - . Launch Site: Barking Sands. LV Family: Honest John. Launch Vehicle: HJ Nike.
  • Aeronomy mission - . Nation: USA. Agency: DASA. Apogee: 100 km (60 mi).

1965 June 24 - . 22:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Thor Able-Star. LV Configuration: Thor Ablestar-2 447 AB019.
  • Transit O-4 - . Payload: NNS 30040 / OPS 8480. Mass: 61 kg (134 lb). Nation: USA. Agency: USN. Program: Transit. Class: Navigation. Type: Navigation satellite. Spacecraft: Transit. USAF Sat Cat: 1420 . COSPAR: 1965-048A. Apogee: 1,125 km (699 mi). Perigee: 1,016 km (631 mi). Inclination: 90.1000 deg. Period: 106.60 min. Summary: Spacecraft built by Naval Avionics Facility, but refurbished by APL. Operated for 7 to 11 months, but then failed due to poor workmanship of NAFI components..

1966 June 24 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2083.
  • Force modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 June 24 - . 00:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Thor Agena D SLV-2A/D. LV Configuration: Thor SLV-2A Agena D 473 (TA7) / Agena D SS-01B 631.
  • Pageos 1 - . Payload: Pageos A. Mass: 55 kg (121 lb). Nation: USA. Agency: NASA Langley. Class: Earth. Type: Geodetic satellite. Spacecraft: Pageos. Decay Date: 1975-07-12 . USAF Sat Cat: 2253 . COSPAR: 1966-056A. Apogee: 4,220 km (2,620 mi). Perigee: 3,913 km (2,431 mi). Inclination: 85.4000 deg. Period: 177.10 min. The PAGEOS (Passive Geodetic Earth Orbiting Satellite) spacecraft was a 30.48-m inflatable sphere, and had no instrumentation on board. It was the second (following GEOS 1) NASA satellite in the National Geodetic Satellites Program. The launch, orbit, separation, inflation and initial operation were nominal, with more than 40 ground stations participating in the observation program. The orbit was generally considered too high for drag-density study, although some work was done in this area by the Smithsonian Astrophysical Observatory. Additional Details: Pageos 1.
  • Pageos canister half - . Payload: Pageos canister half. Nation: USA. Agency: NASA Langley. Spacecraft: Pageos. USAF Sat Cat: 2511 . COSPAR: 1966-056D. Apogee: 4,255 km (2,643 mi). Perigee: 4,227 km (2,626 mi). Inclination: 87.0000 deg. Period: 181.50 min.
  • Pageos canister half - . Payload: Pageos canister half. Nation: USA. Agency: NASA Langley. Spacecraft: Pageos. USAF Sat Cat: 2256 . COSPAR: 1966-056C. Apogee: 4,276 km (2,656 mi). Perigee: 4,196 km (2,607 mi). Inclination: 86.9000 deg. Period: 181.40 min.

1967 June 24 - . 09:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Agency: GMS. Apogee: 78 km (48 mi).

1968 June 24 - . 22:51 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.214NB.
  • Biological mission - . Nation: USA. Agency: NASA. Apogee: 144 km (89 mi).

1969 June 24 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: SSBS. Launch Vehicle: SSBS S02. LV Configuration: SSBS S02 V4.
  • S02V-4 test - . Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1969 June 24 - . 06:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 287 - . Payload: Zenit-2 11F61 s/n 76. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Duration: 8.00 days. Decay Date: 1969-07-02 . USAF Sat Cat: 3991 . COSPAR: 1969-054A. Apogee: 265 km (164 mi). Perigee: 189 km (117 mi). Inclination: 51.8000 deg. Period: 89.00 min. Summary: Area survey photo reconnaissance satellite..

1969 June 24 - . 19:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL AT3.535.
  • Extreme ultraviolet Mon Solar extreme ultraviolet mission - . Nation: USA. Agency: USAF. Apogee: 216 km (134 mi).

1969 June 24 - . 19:02 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Agency: AN. Apogee: 170 km (100 mi).

1970 June 24 - . Launch Site: Kwajalein. Launch Complex: Kwajalein Meck. Launch Vehicle: Spartan. LV Configuration: Spartan ABM 800019.
  • Safeguard M1-1A Interceptor mission - . Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

1970 June 24 - . 04:33 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-313.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 June 24 - . LV Family: N1. Launch Vehicle: N1.
  • Soyuz 11 Day 19 - . Nation: USSR. Related Persons: Dobrovolsky; Patsayev; Volkov; Karas. Program: Salyut; Lunar L3. Flight: Soyuz 11. Dobrovolsky and Patsayev successfully complete the Svinets experiment, fixing the position of a rocket launched at night. The N1 launch has been delayed again. Karas reports that telemetry shows many problems with the rocket, even just sitting on the pad. Kamanin sees this lousy rocket as a heavy cross for Soviet cosmonautics to bear. As for Soyuz 11, the Landing Commission discusses moving the landing from the 3rd to 2nd revolution on 30 July. But then the crew will land in the dark, while for the 3rd revolution landing they will touch down 24 minutes before sunrise. It is decided to continue planning for the third revolution, in case the crew needs immediate medical assistance.

1971 June 24 - . 01:05 GMT - . Launch Site: Syowa Base. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210JA-4.
  • Auroral mission - . Nation: Japan. Agency: NIPR. Apogee: 130 km (80 mi).

1971 June 24 - . 05:50 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.08CG.
  • LPARL XRT X-ray astronomy mission - . Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).

1971 June 24 - . 07:59 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 428 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 12.00 days. Decay Date: 1971-07-06 . USAF Sat Cat: 5305 . COSPAR: 1971-057A. Apogee: 257 km (159 mi). Perigee: 205 km (127 mi). Inclination: 51.7000 deg. Period: 89.10 min. Summary: Area survey photo reconnaissance satellite; returned film capsule; deployed electron and gamma ray science capsule..
  • Nauka - . Payload: Nauka. Nation: USSR. Agency: MOM. Spacecraft: Nauka. Decay Date: 1971-07-13 . USAF Sat Cat: 5315 . COSPAR: 1971-057G. Apogee: 239 km (148 mi). Perigee: 199 km (123 mi). Inclination: 51.7000 deg. Period: 88.88 min.

1971 June 24 - . 15:00 GMT - . Launch Site: Point Barrow. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.367GM.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 111 km (68 mi).

1971 June 24 - . 15:10 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.371GM.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 114 km (70 mi).

1972 June 24 - . 15:00 GMT - . Launch Site: White Sands. Launch Vehicle: Rocketsonde.
  • Starute, Datasonde - . Nation: USA. Agency: MRN. Apogee: 60 km (37 mi).

1973 June 24 - . 02:00 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1974 June 24 - . LV Family: N1. Launch Vehicle: N1.
  • N1-L3 work suspended. - . Nation: USSR. Spacecraft: Soyuz 7K-OK; LK; L3M-1972. Summary: TsKBEM Decree 'On suspension of work on the N1 -L3' was issued..

1974 June 24 - . Launch Site: Baikonur. Launch Complex: Baikonur LC106. LV Family: R-36M. Launch Vehicle: R-36M.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 June 24 - . 22:38 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton-K 283-02.
  • Salyut 3 - . Payload: Almaz s/n 101-02. Mass: 18,500 kg (40,700 lb). Nation: USSR. Agency: MOM. Program: Almaz. Class: Manned. Type: Manned space station. Spacecraft: Almaz OPS. Duration: 90.00 days. Decay Date: 1975-01-24 . USAF Sat Cat: 7342 . COSPAR: 1974-046A. Apogee: 253 km (157 mi). Perigee: 213 km (132 mi). Inclination: 51.6000 deg. Period: 89.10 min. First successful Almaz military manned space station flight. Tested a wide array of reconnaissance sensors. Following the successful Soyuz 14 and unsuccessful Soyuz 15 missions, on 23 September 1974 the station ejected a film return capsule. The KSI capsule suffered damage during re-entry but all the film was recoverable. On 24 January 1975 trials of the on-board 23 mm Nudelmann aircraft cannon (other sources say it was a Nudelmann NR-30 30 mm gun) were conducted. The next day the station was commanded to retrofire to a destructive re-entry over the Pacific Ocean. Although only one of three planned crews managed to board the station, that crew did complete the first completely successful Soviet space station flight. Additional Details: Salyut 3.

1975 June 24 - .
  • Start structural assembly (MPTA-098) - . Nation: USA. Program: STS.

1975 June 24 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: SSBS. Launch Vehicle: SSBS S2. LV Configuration: SSBS S2 S-1E-2605.
  • Operational test - . Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1975 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 656. Launch Vehicle: Poseidon.
  • FOT-12? Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1975 June 24 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 656. Launch Vehicle: Poseidon.
  • FOT-12? Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1975 June 24 - . 11:18 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 6 AC. LV Configuration: Skylark 6 AC SL1105.
  • Soft X-ray 1D tel X-ray astronomy mission - . Nation: UK. Agency: BAC. Apogee: 180 km (110 mi).

1975 June 24 - . 12:05 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 745 - . Payload: DS-P1-Yu s/n 76. Mass: 400 kg (880 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-Yu. Completed Operations Date: 1976-03-07 . Decay Date: 1976-03-12 . USAF Sat Cat: 7982 . COSPAR: 1975-058A. Apogee: 514 km (319 mi). Perigee: 264 km (164 mi). Inclination: 71.0000 deg. Period: 92.40 min. Summary: Development of systems for air defence and the control of outer space..

1976 June 24 - .
  • Complete MPTA-098 proof load test - . Nation: USA. Program: STS. Summary: Complete MPTA-098 proof load test, Lockheed test site and on dock, Palmdale.

1976 June 24 - . 07:10 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 834 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 12.00 days. Decay Date: 1976-07-06 . USAF Sat Cat: 8914 . COSPAR: 1976-058A. Apogee: 237 km (147 mi). Perigee: 216 km (134 mi). Inclination: 81.4000 deg. Period: 89.10 min. Summary: Area survey photo reconnaissance satellite; returned film capsule..

1976 June 24 - . 23:40 GMT - . Launch Site: Syowa Base. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210JA-20.
  • VLF / HF / ne Aurora mission - . Nation: Japan. Agency: NIPR. Apogee: 118 km (73 mi).

1977 June 24 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle MPTA shipped to National Space Technology Laboratories - . Nation: USA. Summary: The test article of the shuttle orbiter's aft structure is mated to External Tank MPTA-ET (ET number one) and three prototype SSME engines..

1977 June 24 - .
  • Deliver MPTA-098 to NSTL - . Nation: USA. Program: STS.

1977 June 24 - . 05:41 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-37 - . 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: 1993-05-20 . USAF Sat Cat: 10092 . COSPAR: 1977-054A. Apogee: 4,564 km (2,835 mi). Perigee: 106 km (65 mi). Inclination: 62.6000 deg. Period: 134.90 min. Summary: Operation of a system of long range telephone-telegraph radiocommunication, and transmission of USSR Central Television programmes to the stations of the Orbita network. .

1977 June 24 - . 10:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3. LV Configuration: Tsiklon-3 No. 2L.
  • Cosmos 921 - . Payload: Tselina-D Mass model. Mass: 5,000 kg (11,000 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. USAF Sat Cat: 10095 . COSPAR: 1977-055A. Apogee: 651 km (404 mi). Perigee: 587 km (364 mi). Inclination: 75.8000 deg. Period: 97.10 min. Summary: Launch vehicle test. Dummy payload. Investigation of the upper atmosphere and outer space..

1978 June 24 - .
  • Death of Mstislav Vsevolodovich Keldysh - . Nation: Russia. Related Persons: Keldysh. Summary: Chief Theoretician of the Soviet missile and space programmes, 1946-1978. Played a key role in virtually every space project decision until his death. He was President of the Academy of Sciences of the USSR from 1961 to 1975..

1978 June 24 - . 21:13 GMT - . Launch Site: Wallops Island. Launch Platform: VISE. LV Family: MR-12. Launch Vehicle: MR-12. LV Configuration: MR-12 D-75MG.
  • JASPIC - . Nation: USSR. Apogee: 168 km (104 mi).

1979 June 24 - . 17:06 GMT - . Launch Site: Sriharikota. LV Family: RH. Launch Vehicle: RH-560. LV Configuration: RH-560.12A?.
  • X-ray astronomy mission - . Nation: India. Agency: ISRO. Apogee: 332 km (206 mi).

1980 June 24 - . 05:30 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.41UH.
  • X-ray astronomy mission - . Nation: USA. Agency: NASA. Apogee: 213 km (132 mi).

1981 June 24 - . 17:47 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Molniya 1-50 - . 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: 1991-12-14 . USAF Sat Cat: 12556 . COSPAR: 1981-060A. Apogee: 39,708 km (24,673 mi). Perigee: 190 km (110 mi). Inclination: 63.9000 deg. Period: 708.60 min. Replaced Molniya 1-42. Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. Operation of the long-range telephone and telegraph radio communications system in the USSR; transmission of USSR Central Television programmes to stations in the Orbita network.

1982 June 24 - . 16:29 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Soyuz T-6 - . Call Sign: Pamir (Pamirs ). Crew: Chretien; Dzhanibekov; Ivanchenkov. Backup Crew: Baudry; Kizim; Solovyov, Vladimir. Payload: Soyuz T s/n 9L. Mass: 6,850 kg (15,100 lb). Nation: USSR. Related Persons: Chretien; Dzhanibekov; Ivanchenkov; Baudry; Kizim; Solovyov, Vladimir. Agency: MOM. Program: Salyut 7. Class: Manned. Type: Manned spacecraft. Flight: Salyut 7 EP-1; Salyut 7 EO-1. Spacecraft: Soyuz T. Duration: 7.91 days. Decay Date: 1982-07-02 . USAF Sat Cat: 13292 . COSPAR: 1982-063A. Apogee: 233 km (144 mi). Perigee: 189 km (117 mi). Inclination: 51.7000 deg. Period: 88.70 min. Manned three crew. Docked with Salyut 7. Transported to the Salyut-7 orbital station the Soviet-French international crew, comprising V A Dzhanibekov (USSR), A S Ivanchenkov (USSR) and Jean-Loup Chretien (France) to conduct scientific research and experiments.

1983 June 24 - . 11:30 GMT - . Launch Site: Wallops Island. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki T 1-0548.
  • Test / aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 110 km (60 mi).

1983 June 24 - .
1984 June 24 - . 06:15 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 8B. LV Configuration: Black Brant 8B NASA 27.84UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 248 km (154 mi).

1985 June 24 - . 17:46 GMT - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.53UE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1985 June 24 - .
1986 June 24 - . 20:03 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1987 June 24 - . 11:30 GMT - . Launch Site: Thumba. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1988 June 24 - . 07:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: USHAKOV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 59 km (36 mi).

1991 June 24 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: SSBS. Launch Vehicle: SSBS S3. LV Configuration: SSBS S3 26010.
  • Operational test - . Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1992 June 24 - . 14:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 70 km (43 mi).

1993 June 24 - . 04:12 GMT - . Launch Site: Plesetsk. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 2252 - . Payload: Strela-3 no. 87. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 22687 . COSPAR: 1993-038A. Apogee: 1,417 km (880 mi). Perigee: 1,403 km (871 mi). Inclination: 82.6000 deg. Period: 114.00 min. Summary: Six satellites launched by a single carrier rocket..
  • Cosmos 2257 - . Payload: Strela-3 no. 92. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 22692 . COSPAR: 1993-038F. Apogee: 1,421 km (882 mi). Perigee: 1,407 km (874 mi). Inclination: 82.6000 deg. Period: 114.10 min.
  • Cosmos 2256 - . Payload: Strela-3 no. 91. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 22691 . COSPAR: 1993-038E. Apogee: 1,415 km (879 mi). Perigee: 1,400 km (800 mi). Inclination: 82.6000 deg. Period: 114.00 min.
  • Cosmos 2253 - . Payload: Strela-3 no. 88. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 22688 . COSPAR: 1993-038B. Apogee: 1,426 km (886 mi). Perigee: 1,408 km (874 mi). Inclination: 82.6000 deg. Period: 114.20 min.
  • Cosmos 2255 - . Payload: Strela-3 no. 90. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 22690 . COSPAR: 1993-038D. Apogee: 1,416 km (879 mi). Perigee: 1,404 km (872 mi). Inclination: 82.6000 deg. Period: 114.00 min.
  • Cosmos 2254 - . Payload: Strela-3 no. 89. Mass: 220 kg (480 lb). Nation: Russia. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 22689 . COSPAR: 1993-038C. Apogee: 1,414 km (878 mi). Perigee: 1,393 km (865 mi). Inclination: 82.6000 deg. Period: 113.90 min.

1994 June 24 - . 13:50 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas I. LV Configuration: Atlas I AC-76 / Centaur I 5056.
  • USA 104 - . Payload: UHF F/O F3. Mass: 2,847 kg (6,276 lb). Nation: USA. Agency: HCI. Program: UHF. Class: Communications. Type: Military communications satellite. Spacecraft: HS 601. USAF Sat Cat: 23132 . COSPAR: 1994-035A. Apogee: 35,795 km (22,241 mi). Perigee: 35,776 km (22,230 mi). Inclination: 4.8100 deg. Period: 1,436.05 min. Summary: US Navy communications . Stationed at 14.38 deg W 1995-1999. Launch vehicle put payload into subsynchronous earth orbit with MRS trajectory option..

1997 June 24 - . 03:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 MSLS IFT-1A.
  • MSLS IFT-1A Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,600 km (900 mi). RSLP (MSLS) IFT-1A. The target cluster consisted of 10 objects: one mock warhead, one bus (the stage of the missile which releases the warhead and decoys), and eight decoys. Three decoys were conical in shape, like the warhead, and five were spherical balloons. One balloon was large 2.2 meters in diameter and had a brighter IR signature than the mock warhead. The two medium-sized balloons were about as bright as the mock warhead; they did not deploy as expected and were not reliable parts of the testing program. The two small balloons were released via a canister and were much dimmer than the mock warhead.

1997 June 24 - . 04:00 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein Meck. LV Family: Minuteman. Launch Vehicle: Payload Launch Vehicle. LV Configuration: Minuteman 2 PLV PLV.
  • IFT-1A EKV ABM test - . Nation: USA. Agency: USA SSDC. Apogee: 200 km (120 mi). Non-intercept fly-by to assess the performance of the Boeing-built EKV seeker, collect target phenomenological data, and evaluate (post-test) target-modeling and discrimination algorithms. Boeing was not chosen as the NMD EKV contractor, partly as a result of its system's performance on this test.

1998 June 24 - . 08:01 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GRP-IDF-1.
  • GRP-IDF-1 test - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi). Summary: Two Minuteman 3 missiles launched from Vandenberg to Kwajalein Atoll, one from silo LF-09 and the second from LF-10. Each carried three re-entry vehicles..

1998 June 24 - . 12:46 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF10. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT168GB.
  • FOT GT168GM Follow-on Test launch - . Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi). Summary: FOT. Part of dual Minuteman 3 shot..

1998 June 24 - . 18:29 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2358 - . Mass: 6,600 kg (14,500 lb). Nation: Russia. Agency: MO. Manufacturer: Kozlov. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 120.00 days. Decay Date: 1998-10-22 . USAF Sat Cat: 25373 . COSPAR: 1998-038A. Apogee: 316 km (196 mi). Perigee: 167 km (103 mi). Inclination: 67.1000 deg. Period: 89.30 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. Landed October 22, 1998..

1999 June 24 - .
  • Cassini, second Venus Flyby - . Nation: USA. Spacecraft: Cassini.

1999 June 24 - .
  • Death of Hugo H Woerdemann - . Nation: Germany; USA. Related Persons: Woerdemann. Summary: German-American engineer in WW2. Member of the Rocket Team in the United States thereafter, arrived in America under Project Paperclip on 1945.11.16 aboard the Argentina from La Havre. Died at Temecula, Riverside, California..

1999 June 24 - . 15:44 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. Launch Pad: SLC17A. LV Family: Delta. Launch Vehicle: Delta 7320-10. LV Configuration: Delta 7320-10 D271.
  • FUSE - . Nation: USA. Agency: NASA Greenbelt. Manufacturer: Germantown. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: FUSE. USAF Sat Cat: 25791 . COSPAR: 1999-035A. Apogee: 760 km (470 mi). Perigee: 745 km (462 mi). Inclination: 25.0000 deg. Period: 99.90 min. The Delta 3-m payload fairing was successfully jettisoned and the Far Ultraviolet Spectroscopic Explorer was placed in a 754 km x 769 km x 25.0 degree initial orbit. After separation the Delta second stage then a depletion burn and was left in a 182 x 915 km x 19.1 degree orbit from which it would quickly decay out of orbit. Checkout of FUSE in orbit was proceeding well as of July 1.

1999 June 24 - . 17:00 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.182GS.
  • SERTS-99 (09) Solar ultraviolet mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

2000 June 24 - . 00:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M 394-02.
  • Ekspress A No. 3 - . Payload: Ekspress A3 / Ekspress 3A. Mass: 2,600 kg (5,700 lb). Nation: Russia. Agency: Intersputnik. Manufacturer: Reshetnev. Class: Communications. Type: Civilian communications satellite. Spacecraft: Ekspress. USAF Sat Cat: 26378 . COSPAR: 2000-031A. Apogee: 35,795 km (22,241 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Launch delayed from June 23. Geosynchronous communications satellite. Stationed at 11 deg W. Positioned in geosynchronous orbit at 11 deg W in 2000. As of 5 September 2001 located at 10.99 deg W drifting at 0.005 deg W per day. As of 2007 Mar 11 located at 11.00W drifting at 0.005E degrees per day.

2001 June 24 - . 21:21 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Improved Orion. LV Configuration: Improved Orion SO-MI-11.
  • MIDAS Aeronomy / ionosphere mission - . Nation: Norway. Agency: NDRE. Apogee: 85 km (52 mi).

2002 June 24 - . 18:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 2G. LV Configuration: Titan II SLV 23G-14 / M68B-72 + M68B-92 + M68B-71.
  • NOAA 17 - . Payload: NOAA-M. Mass: 1,475 kg (3,251 lb). Nation: USA. Agency: NOAA. Manufacturer: Lockheed. Program: Tiros. Class: Earth. Type: Weather satellite. Spacecraft: Tiros N. USAF Sat Cat: 27453 . COSPAR: 2002-032A. Apogee: 820 km (500 mi). Perigee: 802 km (498 mi). Inclination: 98.4000 deg. Period: 101.10 min. Launch delayed from August 2001. The refurbished Titan 2 missile put the NOAA M satellite on a suborbital trajectory of about -2500 x 820 km x 98 deg. at 1829 UTC. At 1837 UTC the NOAA M propulsion module fired its ATK/Thiokol Star 37XFP solid motor for the orbit insertion burn, followed by a hydrazine trim burn to put the satellite in an 807 x 822 km x 98.8 deg operational orbit. NOAA M became NOAA 17 on entering service with the US National Oceanic and Atmospheric Administration as the primary morning weather satellite, supplementing the NOAA 16 afternoon satellite. Built by Lockheed Martin, NOAA M carried weather imagers and microwave and infrared sounders, as well as a SARSAT search-and-rescue package. It had an on-orbit mass of 1475 kg.

2004 June 24 - .
  • Death of John Bernhardt Ona - . Nation: USA. Related Persons: Ona. Summary: American engineer. Headed Atlas missile final checkout; later Chief of Reliability Engineering for the Centaur..

2004 June 24 - . 21:57 GMT - .
  • EVA ISS EO-9-1 - . Crew: Fincke; Padalka. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.0097 days. Nation: USA. Related Persons: Fincke; Padalka. Program: ISS. Flight: ISS EO-9. The astronauts exited the station at 21:56 GMT on what was to be a six hour spacewalk to replace a failed gyroscope electronics module. The EVA had already been delayed from 10, then 16 June. The original plan was to use American suits, but a coolant leak in one of those forced the crew to use Russian suits. This in turn meant they would have to exist from the airlock in the station's Russian Pirs module, which in turn extended the distance they would have to travel outside the station to 30 m. Eight minutes after exiting the hatch, a serious leak was detected by Russian ground controllers in Fincke's suit. The crew was called back in and it was planned that the EVA would be repeated six days later.

2005 June 24 - . 19:41 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2 410-10? (07?).
  • Ekspress AM-3 - . Payload: Ekspress AM. Mass: 2,600 kg (5,700 lb). Nation: Russia. Agency: Svyaz. Manufacturer: Reshetnev; Cannes. Class: Communications. Type: Civilian communications satellite. Spacecraft: Ekspress. USAF Sat Cat: 28707 . COSPAR: 2005-023A. Apogee: 35,791 km (22,239 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. Summary: Delayed from April 2005. Satellite built by NPO PM with Alcatel C-, Ku- and L-band transponders.Stationed over 80 deg E longitude. As of 2007 Mar 11 located at 139.98E drifting at 0.015W degrees per day..

2006 June 24 - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/20. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 2421 - . Mass: 3,150 kg (6,940 lb). Nation: Russia. Agency: VMF. Manufacturer: Arsenal. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-PU. Decay Date: 2006-06-24 . USAF Sat Cat: 29246 . COSPAR: 2006-026A. Apogee: 414 km (257 mi). Perigee: 384 km (238 mi). Inclination: 65.0000 deg. Period: 92.50 min.

2006 June 24 - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz-U Zh15000-101 / ISS-22P.
  • Progress M-57 - . Payload: Progress M s/n 357. Mass: 7,250 kg (15,980 lb). Nation: Russia. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-13. Spacecraft: Progress M. Decay Date: 2007-01-17 . USAF Sat Cat: 29245 . COSPAR: 2006-025A. Apogee: 349 km (216 mi). Perigee: 335 km (208 mi). Inclination: 51.6000 deg. Period: 91.30 min. Summary: The Progress flew International Space Station resupply mission 22P (NASA called the flight Progress 22). It docked at the ISS Pirs port at 16:25 GMT on June 26..

2008 June 24 - .
  • ISS On-Orbit Status 06/24/08 - . Nation: USA. Related Persons: Kononenko, O D; Tani; Volkov, Sergey; Whitson. Program: ISS. Flight: ISS EO-17. Before breakfast and exercise, all crewmembers completed a 10-min session with the periodic Russian MedOps test "Hematokrit" (MO-10), which measures the red cell count of the blood, with CDR Volkov acting as CMO (Crew Medical Officer, Russian: Examiner).

    It was the second session for Volkov & Kononenko, the first for Chamitoff. (The blood samples were drawn from a finger with a perforator lancet, then centrifuged in two microcapillary tubes in the M-1100 kit's minicentrifuge, and its hematocrit value was read off the tubes with a magnifying glass. It is a well-known phenomenon of space flight that red blood cell count (normal range: 30-45%) tends to go down over time. After the exam, the data were saved in the IFEP software (In-Flight Examination Program) on the MEC (Medical Equipment Computer), and Kononenko stowed the equipment.) Additional Details: ISS On-Orbit Status 06/24/08.


2010 June 24 - . 10:00 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA2. LV Family: Terrier. Launch Vehicle: Terrier Orion.
  • NASA 41.088UO - . Nation: USA. Agency: NASA Greenbelt. Apogee: 120 km (70 mi). Summary: Educational payload.

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