Encyclopedia Astronautica
June 17


June 17 Chronology


1923 June 17 - .
1944 June 17 - . Launch Site: Heidelager. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 18026. FAILURE: Airburst.
  • V-2 M17 G2a - . Nation: Germany. Summary: Airburst 0.2 km to the right of the planned trajectory..

1948 June 17 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike J.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1949 June 17 - . 11:50 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-N-8. LV Configuration: Aerobee RTV-N-8 A13.
  • Classified mission - . Nation: USA. Agency: APL. Apogee: 88 km (54 mi). Summary: Classified flight. Launched at 0450 local time. Reached 88.5 km..

1952 June 17 - .
  • Death of John Marvel Whiteside 'Jack' Parsons - . Nation: USA. Related Persons: Parsons. Summary: American rocket pioneer; co-founder of Aerojet, inventor of solid rocket propellant and American inventor of the storable liquid rocket. Dabbled in the occult, expelled from Aerojet on DoD orders. Killed mixing rocket fuel in his garage..

1952 June 17 - . Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: Honest John. LV Configuration: Honest John 35.
  • Test mission - . Nation: USA. Apogee: 10 km (6 mi).

1954 June 17 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1402T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1959 June 17 - . 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).

1961 June 17 - . 07:29 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 ND3.112.
  • NRL ND3.112 Aeronomy mission - . Nation: USA. Agency: NRL. Apogee: 197 km (122 mi).

1962 June 17 - . 18:14 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 115D / Agena B SPS 2402.
  • Samos 8 - . Payload: Samos E-2 no. 2 / Agena B 2402. Mass: 1,860 kg (4,100 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Samos. Decay Date: 1962-06-18 . USAF Sat Cat: 307 . COSPAR: 1962-Psi-1. Apogee: 198 km (123 mi). Perigee: 198 km (123 mi). Inclination: 96.2000 deg. Period: 88.40 min. Summary: First generation photo surveillance; radio relay of images; Satellite and Missile Observation Satellite. Poor results..
  • FTV 2402 RV - . Payload: E-6 RV. Nation: USA. Agency: USAF. Spacecraft: Samos. COSPAR: 1962-Psi-xx.

1963 June 17 - . Launch Site: ETR Launch Area. Launch Platform: EAG-154. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3X-24.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 June 17 - . 18:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.87GT.
  • Attitude control test - . Nation: USA. Agency: NASA. Apogee: 182 km (113 mi).

1964 June 17 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • Contract with Aerojet-General for engines and related aerospace ground equipment revised. - . Nation: USA. Air Force Space Systems Division's cost-plus-fixed-fee contract with Aerojet-General for engines and related aerospace ground equipment for the Gemini launch vehicle was replaced by a cost-plus-incentive-fee contract. Contract negotiations had been conducted between May 25 and June 17, 1964. The final contract covered the procurement of 14 sets of engines (one set had already been delivered) and associated equipment during the period from July 1, 1963, through December 31, 1967. Cost, performance, and schedule incentives made possible a maximum fee of $5,885,250 versus a minimum fee of $1,177,050. The initial target cost was $39,235,000 with a target fee of $3,138,800.

1964 June 17 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Brigitte. LV Family: Diamant. Launch Vehicle: Emeraude VE121. FAILURE: Failure.
  • Test mission - . Nation: France. Agency: CNES. Apogee: 0 km ( mi).

1964 June 17 - . 01:01 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun Falling Sphere 14.
  • Aeronomy mission - . Nation: USA. Agency: USN. Apogee: 140 km (80 mi).

1964 June 17 - . 04:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. LV Family: UR-200. Launch Vehicle: UR-200.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 694 km (431 mi).

1965 June 17 - . 07:30 GMT - . Launch Site: Niijima. LV Family: S. Launch Vehicle: HM-16. LV Configuration: HM-16 HM-16-D.
  • Test mission - . Nation: Japan. Agency: STA. Apogee: 52 km (32 mi).

1965 June 17 - . 17:40 GMT - . Launch Site: Delamar Dry Lake DZ. Launch Pad: 37.3 N x 114.9 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 1-55-89.
  • X-15A IR Scanner, INS test - . Nation: USA. Agency: NASA; USAF. Apogee: 33 km (20 mi). Summary: Maximum Speed - 5697 kph. Maximum Altitude - 33071 m..

1965 June 17 - . 21:07 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.140GE.
  • CR fluxes Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 233 km (144 mi).

1965 June 17 - . 21:41 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.246UI.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 177 km (109 mi).

1966 June 17 - . 11:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 121 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 8.00 days. Decay Date: 1966-06-25 . USAF Sat Cat: 2210 . COSPAR: 1966-054A. Apogee: 327 km (203 mi). Perigee: 205 km (127 mi). Inclination: 72.8000 deg. Period: 89.80 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1967 June 17 - .
  • China conducts first thermonuclear bomb test. - . Nation: China. Program: Long March.

1967 June 17 - . 02:36 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78M. FAILURE: Stage 4's engine 11D33 failed to ignite because the turbopump had not been cooled before ignition.. Failed Stage: 3.
  • Cosmos 167 - . Payload: 1V (V-67) s/n 311. Mass: 1,106 kg (2,438 lb). Nation: USSR. Agency: MOM. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft: Venera 1V (V-67). Decay Date: 1967-06-25 . USAF Sat Cat: 2852 . COSPAR: 1967-063A. Apogee: 264 km (164 mi). Perigee: 211 km (131 mi). Inclination: 51.8000 deg. Period: 89.20 min. Suggestions for the cause of the failure included incorrect soldering of wires in multiple pin plugs, wrong attachments of the plugs to the pyrotechnic connectors, or a mix-up of the pyrotechnic connectors during assembly.. Investigation of the upper atmosphere and outer space.

1967 June 17 - . 08:30 GMT - . Launch Site: Natal. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.50IE.
  • GRS Test Technology / plasma mission - . Nation: Germany. Agency: NASA; DFVLR. Apogee: 991 km (615 mi).

1967 June 17 - . 16:28 GMT - . Launch Site: Indian Ocean. Launch Pad: 56.1 S x 59.8 E. Launch Platform: VOKV. LV Family: M-100. Launch Vehicle: M-100.
  • Ionosphere mission - . Nation: USSR. Agency: AN. Apogee: 90 km (55 mi).

1967 June 17 - . 21:15 GMT - . Launch Site: Indian Ocean. Launch Pad: 60.0 S x 60.2 E. Launch Platform: VOKV. LV Family: M-100. Launch Vehicle: M-100.
  • Ionosphere mission - . Nation: USSR. Agency: AN. Apogee: 90 km (55 mi).

1968 June 17 - .
  • Two-burn lunar orbit insertion (LOI) maneuver studied - . Nation: USA. Related Persons: Phillips, Samuel. Program: Apollo. Spacecraft: Apollo LM; LM Guidance. Apollo Program Director Phillips wrote MSC Director Gilruth concerning the April 10 proposal for a two-burn lunar orbit insertion (LOI) maneuver and a spring ejection of the LM from the spacecraft-lunar module adapter. Phillips agreed to the two-burn LOI in place of the originally planned one burn if results of an analysis should prove the requirement. He specified that an analysis be made of the tradeoffs and that the analysis include the risk of crash, the assumed risks due to lengthening the lunar orbit time (about four hours), and risks due to an additional spacecraft propulsion system burn, as well as the effect of the lunar gravitational potential on the ability to target the LOI maneuver to achieve the desired vector at the time of LM descent. The proposal for spring ejection of the LM from the SLA was approved with the provision that a failure analysis be made in order to understand the risks in the change.

1969 June 17 - .
  • Four-hour tour of the Gagarin Centre by the Bulgarian party boss and other high officials. - . Nation: USSR.

1970 June 17 - .
  • Soyuz 9 Day 17 - . Nation: USSR. Related Persons: Mishin; Kerimov; Grechko, Andrei; Nikolayev; Sevastyanov. Program: Soyuz. Flight: Soyuz 9. Spacecraft: Soyuz 7K-OK. Today the Soyuz 9 crew set a new space endurance record. Everything is normal aboard the spacecraft, except for the failed telemetry commutator and the engaged ASP switch. What would now be needed, notes Kamanin, are new Soyuz spacecraft to extend the duration in space gradualy to 30, 40, 50, and then 60 days. But there are no new spacecraft - Kamanin's plan for construction of an additional ten Soyuz was blocked. Grechko and others in the leadership want a big greeting ceremony for the crew in Moscow, but Kamanin only wants the crew in the hands of the doctors for the first 10 to 12 days after the flight. At 15:00, Mishin and Kerimov, following their bosses' orders from Moscow, announce that they want to extend the flight to 20 days.

1970 June 17 - .
  • X-24 Flight 14 - . Crew: Manke. Payload: X-24A flight 14. Nation: USA. Related Persons: Manke. Class: Manned. Type: Manned spaceplane. Spacecraft: X-24A. Summary: Maximum Speed - 1051 kph. Maximum Altitude - 18593 m. Flight Time - 432 sec..

1970 June 17 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25C. Launch Vehicle: Poseidon. LV Configuration: Poseidon C3XT-23.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1970 June 17 - . 08:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-312.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 June 17 - . 12:59 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 349 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 8.00 days. Decay Date: 1970-06-25 . USAF Sat Cat: 4416 . COSPAR: 1970-045A. Apogee: 332 km (206 mi). Perigee: 199 km (123 mi). Inclination: 65.4000 deg. Period: 89.80 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1971 June 17 - .
  • Soyuz 11 Day 12 - . Nation: USSR. Related Persons: Dobrovolsky; Patsayev; Volkov; Mishin. Program: Salyut. Flight: Soyuz 11. Spacecraft: Salyut 1. At the 08:00 comms session Volkov is on duty, while Dobrovolsky and Patsayev sleep. Kamanin notes that to Volkov everything in his account of the previous day's emergency is 'I' - 'I' decided, 'I' did, etc. Mishin expresses his opinion that the flight commander must make all the decisions; to which Volkov answers 'the whole crew decides things together'. The tracking team, however, considers him too independent and emotional, a person who won't recognise or acknowledge his errors. The State Commission meets at 11:00 and decides there is nothing to prevent the mission continuing. However it is decided to shut down all scientific equipment. They will be turned back on one by one in an attempt to find the origin of the burning.

1972 June 17 - . 00:49 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC43. Launch Vehicle: Rocketsonde.
  • Starute, Datasonde - . Nation: USA. Agency: MRN. Apogee: 63 km (39 mi).

1974 June 17 - . 16:40 GMT - . Launch Site: Thule AFB. Launch Vehicle: Rocketsonde.
  • Starute, AN/DMQ-9- - . Nation: USA. Agency: MRN. Apogee: 70 km (43 mi).

1975 June 17 - . 23:40 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 88 km (54 mi).

1976 June 17 - . 05:30 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 350. LV Configuration: Aerobee 350 NASA 17.17UH.
  • SAO XR X-ray astronomy mission - . Nation: USA. Agency: NASA. Apogee: 232 km (144 mi).

1976 June 17 - . 07:47 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 7 AC. LV Configuration: Skylark 7 AC SL1501.
  • Coded mask telescope X-ray astronomy mission - . Nation: UK. Agency: BAC. Apogee: 256 km (159 mi).

1977 June 17 - . 03:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47182-422.
  • Signe 3 - . Mass: 102 kg (224 lb). Nation: France. Agency: CNES. Program: Intercosmos. Class: Technology. Type: Navigation technology satellite. Spacecraft: Signe. Decay Date: 1979-06-20 . USAF Sat Cat: 10064 . COSPAR: 1977-049A. Apogee: 522 km (324 mi). Perigee: 449 km (278 mi). Inclination: 50.7000 deg. Period: 94.30 min. Summary: This marked the first time the Kapustin Yar cosmodrome was opened to capitalist countries. 20 French specialists worked on the satellite..

1977 June 17 - . 07:23 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 918 - . Mass: 1,400 kg (3,000 lb). Nation: USSR. Agency: MO. Class: Military. Type: Anti-satellite system. Spacecraft: IS-A. Decay Date: 1977-06-18 . USAF Sat Cat: 10065 . COSPAR: 1977-050A. Apogee: 197 km (122 mi). Perigee: 125 km (77 mi). Inclination: 65.1000 deg. Period: 87.70 min. Summary: ASAT interceptor. Failed to intercept Cosmos 909. Deorbited using on-board engine..

1978 June 17 - . 00:00 GMT - . Launch Site: Eareckson. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 57 km (35 mi).

1980 June 17 - . 02:01 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 72 km (44 mi).

1981 June 17 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1277 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-6U. Duration: 14.00 days. Decay Date: 1981-07-01 . USAF Sat Cat: 12520 . COSPAR: 1981-056A. Apogee: 373 km (231 mi). Perigee: 204 km (126 mi). Inclination: 70.4000 deg. Period: 90.30 min. Summary: Photo surveillance; returned film capsule..

1982 June 17 - . 10:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1983 June 17 - . Launch Site: Vandenberg.
  • First Peacekeeper missile launch. - . Nation: USA.

1983 June 17 - . 09:00 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.72NP.
  • SPAR 10 Microgravity mission - . Nation: USA. Agency: NASA. Apogee: 212 km (131 mi).

1985 June 17 - .
1985 June 17 - . 04:15 GMT - . Launch Site: Natal. LV Family: Sergeant. Launch Vehicle: Castor Lance. LV Configuration: Castor Lance GL A44.362. FAILURE: Failure.
  • BEAM Infrared astronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 500 km (310 mi).

1985 June 17 - . 11:33 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-25/51-G.
  • STS-51-G - . Call Sign: Discovery. Crew: Al-Saud; Baudry; Brandenstein; Creighton; Fabian; Lucid; Nagel. Payload: Discovery F05 / Morelos 1[PAM-D] / Telstar 303. Mass: 20,174 kg (44,476 lb). Nation: USA. Related Persons: Al-Saud; Baudry; Brandenstein; Creighton; Fabian; Lucid; Nagel. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-51-G. Spacecraft: Discovery. Duration: 7.07 days. Decay Date: 1985-06-24 . USAF Sat Cat: 15823 . COSPAR: 1985-048A. Apogee: 369 km (229 mi). Perigee: 358 km (222 mi). Inclination: 28.5000 deg. Period: 91.80 min. Deployed and retrieved Spartan 1; launched Morelos 1, Arabsat 1B, Telstar 3D.Payloads: Shuttle Pointed Autono-mous Research Tool for Astronomy (SPARTAN)-1; Automated Directional Solidification Furnace (ADSF); High Precision Tracking Experiment (HPTE); Orbiter Experiments (OEX); French Echocardiograph Experiment (FEE) and French Pocket Experiment (FPE).
  • Morelos 1 - . Payload: Morelos-A / PAM-D. Mass: 512 kg (1,128 lb). Nation: Mexico. Agency: Morelos. Program: Morelos. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. Completed Operations Date: 1994-03-04 . USAF Sat Cat: 15824 . COSPAR: 1985-048B. Apogee: 36,030 km (22,380 mi). Perigee: 35,999 km (22,368 mi). Inclination: 6.3000 deg. Period: 1,447.80 min. Released by STS 51G 17 June 1985; 113.5 deg W. Coverage of the national territory with television, radio and telephony signals and data transmission. Geostationary satellite. Positioned in geosynchronous orbit at 113 deg W in 1985-1994 As of 4 September 2001 located at 123.32 deg W drifting at 2.909 deg W per day. As of 2007 Mar 10 located at 176.84E drifting at 2.883W degrees per day.
  • Spartan 1 - . Payload: Spartan 101. Mass: 1,008 kg (2,222 lb). Nation: USA. Agency: NASA Greenbelt. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Spartan. Decay Date: 1985-06-24 . USAF Sat Cat: 15831 . COSPAR: 1985-048E. Apogee: 395 km (245 mi). Perigee: 359 km (223 mi). Inclination: 28.5000 deg. Period: 92.10 min. Summary: Released by STS 51G 20 June 1985, retrieved 22 June 1985..
  • Telstar 3D - . Payload: Telstar 303 / PAM-D. Mass: 630 kg (1,380 lb). Nation: USA. Agency: ATT. Program: Telstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 376. Completed Operations Date: 1999-02-04 . USAF Sat Cat: 15826 . COSPAR: 1985-048D. Apogee: 35,911 km (22,314 mi). Perigee: 35,888 km (22,299 mi). Inclination: 5.4000 deg. Period: 1,441.90 min. Released by STS 51G 19 June 1985; stationed at 76 deg W. Positioned in geosynchronous orbit at 125 deg W in 1985-1992; 123 deg W in 1992-1996; 120 deg W in 1996-1999 As of 31 August 2001 located at 16.95 deg W drifting at 1.400 deg W per day. As of 2007 Mar 10 located at 6.47W drifting at 1.400W degrees per day.
  • Arabsat 1B - . Payload: Discovery F5 / Morelos 1 [PAM-D] / Telstar 303 [PA. Mass: 592 kg (1,305 lb). Nation: Arab States. Agency: Arabsat. Program: Arabsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 100. Completed Operations Date: 1992-06-01 . USAF Sat Cat: 15825 . COSPAR: 1985-048C. Apogee: 35,746 km (22,211 mi). Perigee: 35,737 km (22,205 mi). Inclination: 1.9000 deg. Period: 1,433.80 min. Summary: Released by STS 51G 18 June 1985; 26 deg E. Positioned in geosynchronous orbit at 26 deg E in 1985-1992 As of 5 September 2001 located at 135.45 deg W drifting at 0.555 deg E per day. As of 2007 Mar 9 located at 165.57E drifting at 0.400E degrees per day..

1986 June 17 - . 20:10 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1987 June 17 - . 11:45 GMT - . Launch Site: Thumba. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 80 km (49 mi).

1988 June 17 - . 14:37 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1988 June 17 - .
1989 June 17 - .
  • Astronaut Stanley David Griggs dies at age of 49 -- Crash of a World-War-II-era training plane. - . Nation: USA. Related Persons: Griggs. Summary: American test pilot mission specialist astronaut. Flew on STS-51-D..

1991 June 17 - . 21:50 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton-K 337-01.
  • Mak 1 - . Payload: Mak. Nation: USSR. Agency: MOM. Program: Mir. Class: Earth. Type: Atmosphere satellite. Flight: Mir EO-9; Mir LD-3. Spacecraft: Mak. Decay Date: 1991-10-18 . USAF Sat Cat: 21425 . COSPAR: 1986-017DV. Apogee: 389 km (241 mi). Perigee: 377 km (234 mi). Inclination: 51.6000 deg. Period: 92.20 min. Summary: Deployed from MIR 6/17/91. Launched from Mir airlock. Investigation of features at the Earth's atmosphere. Launched with the Mir orbital station. .

1992 June 17 - . 14:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 85 km (52 mi).

1994 June 17 - . 07:07 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44LP. LV Configuration: Ariane 44LP+ V64.
  • Intelsat 702 - . Mass: 3,695 kg (8,146 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 23124 . COSPAR: 1994-034A. Apogee: 35,795 km (22,241 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.0200 deg. Period: 1,436.07 min. Stationed at 1.03 deg W. Positioned in geosynchronous orbit at 38 deg W in 1994; 1 deg W in 1994-1996; 177 deg E in 1996-1999 As of 5 September 2001 located at 175.99 deg E drifting at 0.001 deg E per day. As of 2007 Mar 9 located at 54.82E drifting at 0.001E degrees per day.
  • STRV-1A - . Mass: 53 kg (116 lb). Nation: UK. Class: Technology. Type: Navigation technology satellite. Spacecraft: STRV. USAF Sat Cat: 23126 . COSPAR: 1994-034C. Apogee: 31,321 km (19,461 mi). Perigee: 273 km (169 mi). Inclination: 7.4000 deg. Period: 547.70 min. Summary: 50 cm cube; Space Technology and Research Vehicle; included solar cell tests..
  • STRV-1B - . Mass: 50 kg (110 lb). Nation: UK. Class: Technology. Type: Navigation technology satellite. Spacecraft: STRV. USAF Sat Cat: 23125 . COSPAR: 1994-034B. Apogee: 31,817 km (19,770 mi). Perigee: 278 km (172 mi). Inclination: 7.5000 deg. Period: 557.00 min. Summary: 50 cm cube; Space Technology and Research Vehicle; included solar cell tests..

1995 June 17 - . LV Family: Atlas. Launch Vehicle: Atlas.
  • Lockheed Aircraft Corporation merged with Martin to form Lockheed Martin - . Nation: USA. Summary: Atlas assembly line moved from Kearney Mesa, California, to Littleton, Colorado.

1996 June 17 - . 05:50 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.134UR.
  • Radio astronomy mission - . Nation: USA. Agency: NASA Greenbelt. Apogee: 300 km (180 mi).

1998 June 17 - . 02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 57 km (35 mi).

1999 June 17 - .
  • ISS Status Report: ISS 99-22 - . Nation: USA. Program: ISS. International Space Station flight controllers prepared to maneuver the station slightly last weekend to avoid a possible close pass by orbital debris, but the maneuver was not carried out and ultimately was not required as the debris passed a harmless distance from the station early Sunday morning. Additional Details: ISS Status Report: ISS 99-22.

2000 June 17 - .
  • Discovery of the Dhofar 378 Meteorite (Mars Meteorite) - . Nation: Oman.

2001 June 17 - . 00:05 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Improved Orion. LV Configuration: Improved Orion SO-MI-05.
  • MIDAS Aeronomy / ionosphere mission - . Nation: Norway. Agency: NDRE. Apogee: 85 km (52 mi).

2002 June 17 - .
2005 June 17 - .
2006 June 17 - . 22:44 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M (DM3) 410-12.
  • Kazsat 1 - . Mass: 1,380 kg (3,040 lb). Nation: Russia. Agency: KazSat. Manufacturer: Chelomei. Class: Communications. Type: Civilian communications satellite. Spacecraft: Yakhta. USAF Sat Cat: 29230 . COSPAR: 2006-022A. Apogee: 35,781 km (22,233 mi). Perigee: 35,381 km (21,984 mi). Inclination: 0.0000 deg. Period: 1,425.60 min. Summary: As of 2007 Mar 9 located at 103.02E drifting at 0.000W degrees per day..

2007 June 17 - .
2008 June 17 - .
  • ISS On-Orbit Status 06/17/08 - . Nation: USA. Related Persons: Kononenko, O D; Love; Volkov, Sergey. Program: ISS. Flight: ISS EO-17. Major focus for CDR Volkov and FE-1 Kononenko today was on Orlan spacesuit activities in the DC1 'Pirs' Docking Compartment, to extend for the next several days.

    And preparing spacewalk hardware for the EVA-20 on 7/10 and prior simulation exercises.
    After configuring the DC1 communications system for their presence, Sergey & Oleg -

    Readied and checked out replaceable components (OTA) and auxiliary gear for their particular Orlan "skafandr" suits (i.e., portable primary & reserve O2 tanks (BK-3), storage batteries (825M3), LiOH canisters (PL-9), moisture collectors, liquid cooling garments (KVO), comm headsets (ShL-10), gloves (GP-10K), thermal comfort undergarments (BK-10), socks, diapers, filters for feedwater lines (FOR), Orlan CO2 measurement units (IK), degassing pump unit (BOS), etc.),
    Configured & tested the EVA support panels (POV) in the DC1 and SM PkhO (Service Module Transfer Compartment) (to be used for leak checks and valve tests on the Orlan suits, their BSS interface units & the hatch KVDs (pressure equalization valves)),
    Activated & inspected their spacesuits plus a third Orlan for training/testing (Orlan #27 (red stripe) for Volkov, #26 (blue stripe) for Kononenko, #25 for testing & training),
    Terminated the charging on the 825M3 battery pack started yesterday,
    Activated the training Orlan #25 and equipped it with the BRTA-25 telemetry system,
    Installed the 825M3 battery pack in the #25 backpack, and
    Reset the DC1 comm system to its regular configuration.
    In the U.S. 'Quest' Airlock, FE-2 Chamitoff - Additional Details: ISS On-Orbit Status 06/17/08.


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