Encyclopedia Astronautica
August 14


August 14 Chronology


1943 August 14 - .
  • Birth of Jon Andrew McBride - . Nation: USA. Summary: American test pilot astronaut. Flew on STS-41-G. Heavyset Navy pilot with a talent for playing to a crowd. Later ran in, but lost, the Republican primary for governor of West Virginia..

1944 August 14 - . 12:53 GMT - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 18305.
1952 August 14 - .
  • Birth of Mark Charles Lee - . Nation: USA. Summary: American engineer mission specialist astronaut. Flew on STS-30, STS-47, STS-64, STS-82. Was married to astronaut Jan Davis, part of first married couple to fly in space together..

1956 August 14 - .
  • OKB-1 made an independent design bureau. - . Nation: USSR. Summary: Decree 310 'On separation of OKB-1 from NII-88' was issued..

1956 August 14 - .
  • X-1B Flight 12 - . Crew: McKay. Payload: X-1B flight 11. Nation: USA. Related Persons: McKay. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1B. Summary: NACA flight 1. Pilot check; nose landing gear failed on landing, minor damage..

1957 August 14 - . 08:06 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 59.3 N x 47.8 W. Launch Platform: LSD-29. LV Family: Rockoon. Launch Vehicle: Loki Rockoon. LV Configuration: Loki Rockoon II5.15F.
  • SUI 70 Aeronomy / aurora / chemical release mission - . Nation: USA. Agency: SUI. Apogee: 100 km (60 mi). Summary: Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP15 - - Latitude: 59.30 N - Longitude: 47.80 W..

1958 August 14 - . 00:40 GMT - . Launch Site: Kheysa. LV Family: V-2. Launch Vehicle: R-1. LV Configuration: A-1.
  • Ionosphere / aeronomy mission - . Nation: USSR. Agency: MVS. Apogee: 100 km (60 mi).

1958 August 14 - . 13:28 GMT - . Launch Site: White Sands. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun OB6.01F.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 132 km (82 mi).

1959 August 14 - .
  • Negotiations for the fabrication of six additional Mercury spacecraft. - . Nation: USA. Program: Mercury. Spacecraft: Mercury. Summary: NASA Headquarters approved a Space Task Group proposal that negotiations be undertaken with McDonnell for the fabrication of six additional Mercury spacecraft..

1959 August 14 - . 09:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC18B. Launch Pad: LC18B. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 204.
  • Series IV research and development launch - . Nation: USA. Agency: USAF. Apogee: 520 km (320 mi).

1959 August 14 - . 16:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC19. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I B-5. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 0 km ( mi).

1959 August 14 - . 16:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LC-A. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp NN8.69CF.
  • Solar x-ray mission - . Nation: USA. Agency: USN. Apogee: 237 km (147 mi).

1959 August 14 - . 19:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25B. LV Family: Polaris. Launch Vehicle: Polaris AX. LV Configuration: Polaris AX-13.
  • SMS test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1959 August 14 - . 19:36 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC10W. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 190. FAILURE: Failure. Failed Stage: 1.
  • IWST - . Nation: USA. Agency: RAF. Apogee: 0 km ( mi).

1960 August 14 - . 11:00 GMT - . Launch Site: Pacific Ocean. Launch Pad: 12.2 N x 177.4 E. Launch Platform: SHIP-SOV. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Agency: GMS. Apogee: 47 km (29 mi).

1961 August 14 - . Launch Site: Cape Canaveral. LV Family: Saturn I. Launch Vehicle: Saturn I.
  • First Saturn I arrives at Cape Canaveral. - . Nation: USA. Related Persons: von Braun. Program: Apollo. Summary: Navy barge Compromise, carrying first Saturn booster, stuck in the mud in the Indian River just south of Cape Canaveral. Released several hours later, the Saturn was delayed only 24 hours in its 2,200-mile journey from Huntsville..

1962 August 14 - .
  • LEM added to Apollo CSM Statement of Work - . Nation: USA. Program: Apollo. Spacecraft: Apollo LM; LM Communications; LM ECS; LM Guidance; LM Hatch; LM Source Selection. The NAA spacecraft Statement of Work was revised to include the requirements for the lunar excursion module (LEM) as well as other modifications. The LEM requirements were identical with those given in the LEM Development Statement of Work of July 24.

    The command module (CM) would now be required to provide the crew with a one-day habitable environment and a survival environment for one week after touching down on land or water. In case of a landing at sea, the CM should be able to recover from any attitude and float upright with egress hatches free of water. Additional Details: LEM added to Apollo CSM Statement of Work.


1962 August 14 - .
  • Flight tests of the half-scale vehicle (HSTV) in the Paraglider Development Program. - . Nation: USA. Program: Gemini. Spacecraft: Gemini; Gemini Paraglide. North American began flight tests of the half-scale vehicle (HSTV) in Phase II-A of the Paraglider Development Program two months behind schedule. The instrumented HSTV with the paraglider predeployed was towed aloft by helicopter. Objectives of the predeployed flights were to evaluate flight performance, longitudinal and lateral control characteristics, effectiveness of control, and the flare maneuver capability of the paraglider. Despite various minor malfunctions in all five test flights (August 14, 17, 23, September 17, and October 23, 1962), test results verified the stability of the wing/vehicle combination in free flight and the adequacy of control effectiveness.

1962 August 14 - . 15:20 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 2. LV Configuration: Skylark-2 SL109.
  • La / ion / ne Ionosphere mission - . Nation: Australia. Agency: WRE; RAE. Apogee: 111 km (68 mi).

1962 August 14 - . 18:41 GMT - . Launch Site: Delamar Dry Lake DZ. Launch Pad: 37.3 N x 114.9 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3-9-18. FAILURE: Roll damper failure..
  • X-15A Const Theta Entry test - . Nation: USA. Agency: NASA; USAF. Apogee: 59 km (36 mi). Summary: Maximum Speed - 6029 kph. Maximum Altitude - 59010 m. New reentry technique using pitch angle instrument instead of AOA..

1963 August 14 - .
  • Definitive contract for Apollo command and service modules signed - . Nation: USA. Related Persons: Webb. Program: Apollo. Spacecraft: Apollo CSM. NASA Administrator James E. Webb signed the definitive contract with North American for the development of the Apollo CSM. This followed by almost two years North American's selection as prime contractor, The $938.4 million cost-plus-fixed-fee agreement was the most valuable single research and development contract in American history. The contract called for the initial production (i.e., through May 15, 1965) of 11 mockups, 15 boilerplate vehicles, and 11 production articles.

1964 August 14 - . 09:36 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92. LV Configuration: Vostok 8A92 R15001-04.
  • Cosmos 37 - . Payload: Zenit-2 11F61 s/n 22. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: Korolev. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Duration: 8.00 days. Decay Date: 1964-08-22 . USAF Sat Cat: 848 . COSPAR: 1964-044A. Apogee: 240 km (140 mi). Perigee: 208 km (129 mi). Inclination: 64.9000 deg. Period: 88.90 min. Summary: Area survey photo reconnaissance satellite. Program partially completed. Break in the film fof the SA-10 camera..

1964 August 14 - . 17:54 GMT - . Launch Site: Delamar Dry Lake DZ. Launch Pad: 37.3 N x 114.9 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 2-33-56. FAILURE: Nose gear deployed at Mach 4.2..
  • X-15A-2 Stability test - . Nation: USA. Agency: NASA; USAF. Apogee: 31 km (19 mi). Summary: Maximum Speed - 5776 kph. Maximum Altitude - 31486 m. Nose landing gear extended at Mach 4.5. Both tires blew on landing..

1964 August 14 - . 22:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Atlas. Launch Vehicle: Atlas Agena D SLV-3. LV Configuration: SLV-3 Agena D 7101 / Agena D S01A 4808.
  • KH 7-10 - . Payload: KH-7 no. 10 / OPS 3802. Mass: 2,000 kg (4,400 lb). Nation: USA. Agency: NRO; USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-7. Decay Date: 1964-08-23 . USAF Sat Cat: 850 . COSPAR: 1964-045A. Apogee: 300 km (180 mi). Perigee: 165 km (102 mi). Inclination: 95.4000 deg. Period: 89.10 min. Summary: KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .
  • OPS 3316 - . Payload: P-11 s/n 4202. Mass: 79 kg (174 lb). Nation: USA. Agency: USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1979-03-08 . USAF Sat Cat: 851 . COSPAR: 1964-045B. Apogee: 3,751 km (2,330 mi). Perigee: 272 km (169 mi). Inclination: 95.7000 deg. Period: 127.40 min.

1965 August 14 - . 11:16 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Vostok 8A92. LV Configuration: Vostok 8A92 U15001-02.
  • Cosmos 78 - . Payload: Zenit-2 11F61 s/n 30. 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: 1965-08-22 . USAF Sat Cat: 1505 . COSPAR: 1965-066A. Apogee: 379 km (235 mi). Perigee: 330 km (200 mi). Inclination: 69.0000 deg. Period: 91.60 min. Summary: Area survey photo reconnaissance satellite..

1966 August 14 - . 20:35 GMT - . Launch Site: Point Barrow. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.200GM.
  • Grenades Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).

1967 August 14 - .
  • Almaz space station schedule approved. - . Nation: USSR. Spacecraft: Almaz OPS. Summary: Central Committee of the Communist Party and Council of Soviet Ministers Decree 'On schedule of work on the Almaz space station' was issued..

1967 August 14 - .
  • Gulyayev grounded; Feoktistov in training. - . Nation: USSR. Related Persons: Gulyayev; Feoktistov. Program: Soyuz. Summary: Cosmonaut Gulyayev has hit his head on a stone when diving in the Kholodniy River. Feoktistov continues his attempt to complete 30 months of command cosmonaut training in 75 days. The makes ten dockings in the Volga trainer - 8 of the are rated as 'bad'..

1968 August 14 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
1968 August 14 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 618. LV Family: Polaris. Launch Vehicle: Polaris A2E. LV Configuration: Polaris A2E A2E.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1968 August 14 - . Launch Site: Baikonur. Launch Complex: Baikonur PU31. LV Family: Tsiklon. Launch Vehicle: R-36 8K67M.
  • Operational missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1969 August 14 - .
  • Birth of Tracy Ellen Caldwell - . Nation: USA. Summary: American chemist mission specialist astronaut. Chemist. Flew on STS-118, ISS EO-23..

1969 August 14 - . 02:01 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C58/1.
  • ESRO C58 / 1 Meteorites mission - . Nation: Europe. Agency: ESRO. Apogee: 112 km (69 mi).

1970 August 14 - . 08:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • OT GT31M operational test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1971 August 14 - . 19:54 GMT - . Launch Site: Fort Greely. LV Family: Arcas. Launch Vehicle: Arcas. LV Configuration: Arcas NASA 15.90GM.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 60 km (37 mi).

1972 August 14 - . 20:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 91 km (56 mi).

1973 August 14 - . 08:58 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 4001.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 121 km (75 mi).

1974 August 14 - . LV Family: N1. Launch Vehicle: N1.
  • Glushko meets with TsKBEM staff - . Nation: USSR. Related Persons: Glushko; Korolev; Barmin. Program: Lunar L3. Spacecraft: LK; Soyuz 7K-LOK. He solicited their support in the reorganization and new projects for the bureau. Glushko was sartorially perfect, and had an aristocratic air, never using the familiar forms of address in Russian. He only loosened up a little in the last years of his life. He was a nitpicker, correcting Russian syntax in documents. He was capable of clear logic but did not have the intuitive genius of Korolev (according to Barmin, while Korolev did not look after his appearance, he possessed a pure 'Russian' intelligence).

1974 August 14 - . 15:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 24B. LV Configuration: Titan 24B 24B-12 (3B-46).
  • OPS 3004 - . Payload: KH-8 no. 43 / Agena D. Mass: 3,000 kg (6,600 lb). Nation: USA. Agency: NRO; USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-8. Decay Date: 1974-09-29 . USAF Sat Cat: 7416 . COSPAR: 1974-065A. Apogee: 402 km (249 mi). Perigee: 135 km (83 mi). Inclination: 110.5000 deg. Period: 89.90 min. Summary: KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1974 August 14 - . 18:08 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.417UA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 133 km (82 mi).

1975 August 14 - . 13:29 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53731-288.
  • Cosmos 755 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 8072 . COSPAR: 1975-074A. Apogee: 1,008 km (626 mi). Perigee: 966 km (600 mi). Inclination: 82.9000 deg. Period: 104.80 min. Summary: Military navigation satellite..

1978 August 14 - .
  • Start coefficient tests, STA-099 - . Nation: USA. Program: STS. Summary: Start coefficient tests, STA-099, Lockheed facility, Palmdale.

1978 August 14 - . 14:45 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.34DS. FAILURE: Failure.
  • HRTS-3 Solar mission - . Nation: USA. Agency: NASA. Apogee: 220 km (130 mi).

1979 August 14 - .
  • Ferry flight, Denver to Hill AFB, Ogden, Utah - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Ferry flight, shuttle carrier aircraft/Enterprise (OV-101), Denver to Hill AFB, Ogden, Utah (1 hour, 30 minutes).

1979 August 14 - . 15:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1121 - . Payload: Yantar-2K s/n 929. Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-2K. Duration: 30.00 days. Decay Date: 1979-09-13 . USAF Sat Cat: 11487 . COSPAR: 1979-074A. Apogee: 348 km (216 mi). Perigee: 171 km (106 mi). Inclination: 67.2000 deg. Period: 89.70 min. Summary: Area survey photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1979 August 14 - . 16:50 GMT - . Launch Site: White Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk GL A08.705-2.
  • DMSP MS Aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 190 km (110 mi).

1979 August 14 - . 18:10 GMT - . Launch Site: Kiruna. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion SSC T3 Test.
  • Dummy Orion test - . Nation: Sweden. Agency: SSC. Apogee: 11 km (6 mi).

1979 August 14 - . 20:20 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 GL A04.703.
  • DMSP UV Aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 178 km (110 mi).

1980 August 14 - . 02:02 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.05UA.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 192 km (119 mi).

1981 August 14 - . Launch Site: Wallops Island. LV Family: Black Brant. Launch Vehicle: Black Brant 10. LV Configuration: Black Brant X NASA 12.38GT.
  • Test mission - . Nation: USA. Agency: NASA. Apogee: 625 km (388 mi).

1984 August 14 - . 06:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U 711.
  • Progress 23 - . Payload: Progress s/n 124. Mass: 7,020 kg (15,470 lb). Nation: USSR. Agency: MOM. Program: Salyut 7. Class: Manned. Type: Manned logistics spacecraft. Flight: Salyut 7 EO-3. Spacecraft: Progress. Duration: 13.79 days. Completed Operations Date: 1984-08-28 01:27:45 . Decay Date: 1984-08-28 01:27:45 . USAF Sat Cat: 15193 . COSPAR: 1984-086A. Apogee: 250 km (150 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg. Period: 88.90 min. Transport of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 16 Aug 1984 08:11:00 GMT. Undocked on 26 Aug 1984 16:13:00 GMT. Destroyed in reentry on 28 Aug 1984 01:28:00 GMT. Total free-flight time 3.46 days. Total docked time 10.33 days.

1985 August 14 - . 02:30 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1986 August 14 - . 08:30 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: VOKV. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 88 km (54 mi).

1987 August 14 - . 16:29 GMT - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion GL A12.629.
  • COLDR Aeronomy mission - . Nation: USA. Agency: USAF GL. Apogee: 86 km (53 mi).

1991 August 14 - . 23:15 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L V45.
  • Intelsat 6 F-5 - . Payload: Intelsat 605. Mass: 4,296 kg (9,471 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 393. USAF Sat Cat: 21653 . COSPAR: 1991-055A. Apogee: 35,788 km (22,237 mi). Perigee: 35,784 km (22,235 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. International communications; 14.5 deg W. Positioned in geosynchronous orbit at 24 deg W in 1991-1997; 27 deg W in 1997-1999 As of 2 September 2001 located at 27.48 deg W drifting at 0.015 deg W per day. As of 2007 Mar 10 located at 174.03E drifting at 0.000W degrees per day.

1996 August 14 - . 22:20 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
  • Molniya-1T - . Mass: 1,600 kg (3,500 lb). Nation: Russia. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1T. USAF Sat Cat: 24273 . COSPAR: 1996-045A. Apogee: 39,391 km (24,476 mi). Perigee: 968 km (601 mi). Inclination: 64.1000 deg. Period: 717.90 min.

1997 August 14 - . 12:22 GMT - . Launch Site: Wallops Island. LV Family: Loki. Launch Vehicle: Super Loki. LV Configuration: Super Loki Sphere.
  • CRISTA Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 115 km (71 mi).

1997 August 14 - . 12:27 GMT - . Launch Site: Wallops Island. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A Sphere.
  • CRISTA Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 125 km (77 mi).

1997 August 14 - . 20:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 381-01.
  • Cosmos 2345 - . Payload: SPRN No. 8. Mass: 2,500 kg (5,500 lb). Nation: Russia. Agency: MO. Manufacturer: Lavochkin. Class: Military. Type: Early warning satellite. Spacecraft: Prognoz SPRN. Completed Operations Date: 1999-01-01 . USAF Sat Cat: 24894 . COSPAR: 1997-041A. Apogee: 36,504 km (22,682 mi). Perigee: 35,134 km (21,831 mi). Inclination: 2.6000 deg. Period: 1,437.80 min. Geosynchronous ballistic missile early warning satellite. Positioned in geosynchronous orbit at 23 deg W in 1997-1999 As of 4 September 2001 located at 142.44 deg E drifting at 0.028 deg E per day. As of 2007 Mar 9 located at 66.03W drifting at 0.329E degrees per day.

1997 August 14 - . 21:53 GMT - . Launch Site: Wallops Island. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A Sphere.
  • CRISTA Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 124 km (77 mi).

1997 August 14 - .
  • Landing of Soyuz TM-25 - . Return Crew: Tsibliyev; Lazutkin. Nation: Russia. Related Persons: Tsibliyev; Lazutkin. Program: Mir. Flight: Mir EO-24; Mir NASA-4; Mir EO-23. Following a mission that seemed to consist of an endless series of collisions, breakdowns, fires, and other emergencies, the EO-23 crew handed over the station to EO-24 and on August 14 entered Soyuz TM-25 landed in Kazakstan at 12:17 UTC, 170 km SE of Dzezkazgan. The Soyuz landing rockets failed to fire on touchdown, giving one of the roughest landings experienced by a returning Mir crew.

1999 August 14 - .
  • Galileo, Callisto 22 Flyby - . Nation: USA. Spacecraft: Galileo.

2001 August 14 - .
  • STS-105 Mission Status Report #08 - . Nation: USA. Related Persons: Culbertson; Dezhurov; Horowitz; Tyurin. Program: ISS. Flight: ISS EO-2; ISS EO-3; STS-105. Discovery's crewmembers, including their new Expedition Two crewmates from the International Space Station, were awakened at 4:10 a.m. Central time to the theme from the movie, "Arthur", to begin a day highlighted by the transfer of equipment and supplies to the station from Discovery and from the pressurized cargo carrier the shuttle brought into space. Additional Details: STS-105 Mission Status Report #08.

2004 August 14 - .
2007 August 14 - . 23:44 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA3. LV Family: Ariane 5. Launch Vehicle: Ariane 5ECA. LV Configuration: Ariane 5ECA V177 (537).
  • Spaceway 3 - . Mass: 6,075 kg (13,393 lb). Nation: USA. Agency: Hughes. Manufacturer: El Segundo. Program: DirecTV. Class: Communications. Type: Civilian communications satellite. Spacecraft: HS 702. USAF Sat Cat: 32018 . COSPAR: 2007-036A. Apogee: 35,788 km (22,237 mi). Perigee: 35,786 km (22,236 mi). Inclination: 0.0200 deg. Period: 1,436.12 min. Summary: Satellite launched for Hughes Network Systems, with a Ka-band payload for space-based internet. Mass 3655 kg dry..
  • BSAT-3A - . Payload: A2100A. Mass: 1,967 kg (4,336 lb). Nation: Japan. Agency: BSAT. Manufacturer: Lockheed. Program: BSAT. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 32019 . COSPAR: 2007-036B. Apogee: 35,826 km (22,261 mi). Perigee: 35,746 km (22,211 mi). Inclination: 0.1000 deg. Period: 1,436.00 min. Summary: Satllite launched for the Japan Broadcasting Satellite Systems Corp. (BSAT) with a Ku-band television payload. Mass 930 kg dry..

2010 August 14 - . 11:07 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 531.
  • USA 214 - . Payload: AEHF SV-1. Nation: USA. Agency: Martin. Class: Communications. Type: Military communications satellite. Spacecraft: AEHF. USAF Sat Cat: 36868 . COSPAR: 2010-039A. Apogee: 51,018 km (31,701 mi). Perigee: 12,053 km (7,489 mi). Inclination: 9.9000 deg. Period: 1,224.50 min. First USAF Advanced EHF communications satellite. Placed in an initial 221 x 50179 km x 22.2 deg geosynchronous transfer orbit by the Atlas Centaur upper stage. However the satellite's main BT-4 engine failed, meaning the secondary hydrazine thrusters were used to much more satellite raise the spacecraft to geosynchronous orbit.

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