Encyclopedia Astronautica
August 23


August 23 Chronology


1915 August 23 - .
  • Birth of Travis L Maloy - . Nation: USA. Summary: American engineer. Manager of flight test and launch operations for the Atlas..

1944 August 23 - . Launch Site: Peenemuende. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-226.
1946 August 23 - .
  • Birth of Robert Henry Clegg - . Nation: USA. Summary: American geophysicist payload specialist astronaut, 1990-1992..

1949 August 23 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Deacon.
  • D3 Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1952 August 23 - .
1954 August 23 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 2827T.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1956 August 23 - .
  • Birth of Dr David Alexander 'Bluto' Wolf - . Nation: USA. Summary: Jewish-American physician mission specialist astronaut. Flew on STS-58, Mir NASA-5, STS-112, STS-127..

1956 August 23 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: X-17. Launch Vehicle: X-17. LV Configuration: X-17 R-5 4203-5.
  • 4203-5 re-entry vehicle test flight - . Nation: USA. Agency: USAF. Apogee: 142 km (88 mi). Summary: A five-stage, solid-fuel rocket test vehicle, the world's first, was launched to a speed of mach 15 from Wallops Island, Va. by the NACA Langley Aeronautical Laboratory's Pilotless Aircraft Research Division..

1957 August 23 - . 21:54 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun RP6.X1 igniter test.
  • RP6.1 test - . Nation: USA. Agency: BRL. Apogee: 114 km (70 mi).

1960 August 23 - .
  • Final Department of Defense approval for SAINT development. - . Nation: USA. Spacecraft: SAINT; SAINT II.

1960 August 23 - . LV Family: DF-2; Kosmos 2; R-2. Launch Vehicle: DF-1.
  • Last Russian advisers leave China. - . Nation: China. Related Persons: Tsien. Program: Long March. Summary: The last Russian technical advisers are withdrawn from China..

1960 August 23 - . 17:01 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.16UE.
  • Cosmic rays mission - . Nation: USA. Agency: NASA. Apogee: 190 km (110 mi).

1960 August 23 - . 17:10 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 AA3.128.
  • Solar extreme ultraviolet mission - . Nation: USA. Agency: USAF. Apogee: 237 km (147 mi).

1961 August 23 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • Golovin Committee evaluates three rendezvous methods for manned lunar landing - . Nation: USA. Program: Apollo. Spacecraft: Apollo LM; LM ECS; LM Source Selection. The Large Launch Vehicle Planning Group (Golovin Committee) notified the Marshal! Space Flight Center (MSFC), Langley Research Center, and the Jet Propulsion Laboratory (JPL) that the Group was planning to undertake a comparative evaluation of three types of rendezvous operations and direct flight for manned lunar landing. Rendezvous methods were earth orbit, lunar orbit, and lunar surface. MSFC was requested to study earth orbit rendezvous, Langley to study lunar orbit rendezvous, and JPL to study lunar surface rendezvous. The NASA Office of Launch Vehicle Programs would provide similar information on direct ascent. Additional Details: Golovin Committee evaluates three rendezvous methods for manned lunar landing.

1961 August 23 - . 01:16 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 101D.
  • Research and development launch - . Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi).

1961 August 23 - . 10:04 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC12. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 111D (AA1) / Agena B 6001 (AA1). FAILURE: Agena B second stage failure.. Failed Stage: 2.
  • Ranger 1 - . Payload: NASA P-32 (RA-1). Mass: 306 kg (674 lb). Nation: USA. Agency: NASA. Program: Ranger. Class: Moon. Type: Lunar probe. Spacecraft: Ranger 1-2. Decay Date: 1961-08-30 . USAF Sat Cat: 173 . COSPAR: 1961-Phi-1. Apogee: 446 km (277 mi). Perigee: 179 km (111 mi). Inclination: 32.9000 deg. Period: 90.60 min. Lunar probe; failed to leave Earth orbit. Ranger 1, a test version of the spacecraft which would attempt an unmanned crash landing on the moon, was launched from the Atlantic Missile Range by an Atlas-Agena B booster. The 306 kg spacecraft did not attain the scheduled extremely elongated orbit because of the misfiring of the Agena B rocket. Although the spacecraft systems were tested successfully, only part of the eight project experiments could be carried out. Ranger 1 reentered on August 29 after 111 orbits. Ranger 1's primary mission was to test the performance of those functions and parts that are necessary for carrying out subsequent lunar and planetary missions using essentially the same spacecraft design.

1961 August 23 - . 17:02 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150.
  • Extreme ultraviolet Mon / X-ray counter Aeronomy / solar extreme ultraviolet mission - . Nation: USA. Agency: USAF. Apogee: 225 km (139 mi).

1962 August 23 - . 07:15 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima TMP. LV Family: Kappa. Launch Vehicle: Kappa 8L. LV Configuration: Kappa 8L K-8L-1.
  • Test mission - . Nation: Japan. Agency: ISAS. Apogee: 173 km (107 mi).

1962 August 23 - . 11:44 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC5. LV Family: Scout. Launch Vehicle: Scout X-2M. LV Configuration: Scout X-2M S117.
  • P 35-2 - . Mass: 91 kg (200 lb). Nation: USA. Agency: USAF. Program: DMSP. Class: Earth. Type: Weather satellite. Spacecraft: Program 35. USAF Sat Cat: 369 . COSPAR: 1962-A-Omicron-1. Apogee: 752 km (467 mi). Perigee: 578 km (359 mi). Inclination: 98.5000 deg. Period: 98.10 min. Summary: Military weather satellite to provide targetting information for reconnaisance satellites..

1962 August 23 - . 17:10 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.30CA.
  • Structure Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 129 km (80 mi).

1963 August 23 - . 17:01 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 617. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2P-208.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 August 23 - . 17:41 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 617. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2P-211.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1965 August 23 - . 20:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 454.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 August 23 - . 09:04 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: HAD. LV Configuration: HAD 189.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 100 km (60 mi).

1967 August 23 - .
1967 August 23 - . 04:41 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC10W. LV Family: Delta. Launch Vehicle: Thor Burner 2. LV Configuration: Thor Burner 2 266.
  • DMSP-Block-4A F9 - . Payload: DAPP 3419 (FTV-4) / OPS 7202. Mass: 130 kg (280 lb). Nation: USA. Agency: USAF. Program: DMSP. Class: Earth. Type: Weather satellite. Spacecraft: DMSP Block 4A. USAF Sat Cat: 2920 . COSPAR: 1967-080A. Apogee: 873 km (542 mi). Perigee: 818 km (508 mi). Inclination: 98.9000 deg. Period: 101.90 min. Summary: Defense Meteorological Satellite Program..

1968 August 23 - . Launch Site: Baikonur. Launch Complex: Baikonur PU33. LV Family: Tsiklon. Launch Vehicle: R-36 8K67P.
  • RGCh state trials flight - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1968 August 23 - . 04:48 GMT - . Launch Site: Tonopah. LV Family: Sandhawk. Launch Vehicle: Sandhawk. LV Configuration: Sandhawk Sandia 152-?.
  • LRL AXE-2 X-ray astronomy mission - . Nation: USA. Agency: Sandia. Apogee: 187 km (116 mi).

1969 August 23 - . 16:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 3B. LV Configuration: Titan 23B 23B-1 (3B-23).
  • OPS 7807 - . Payload: KH-8 no. 23 / 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: 1969-09-07 . USAF Sat Cat: 4078 . COSPAR: 1969-074A. Apogee: 377 km (234 mi). Perigee: 138 km (85 mi). Inclination: 108.1000 deg. Period: 89.60 min. Summary: KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1971 August 23 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 618. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 August 23 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 618. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1971 August 23 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 618. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Follow-on operational missile test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1972 August 23 - . 21:00 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.104-1.
  • RM-57 Solar x-ray / ultraviolet mission - . Nation: USA. Agency: USAF. Apogee: 268 km (166 mi).

1973 August 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-3.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 August 23 - . 03:45 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.08GG.
  • 13-in RC Flight 1 Ultraviolet astronomy mission - . Nation: USA. Agency: NASA. Apogee: 213 km (132 mi).

1973 August 23 - . 22:57 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur SLV-3D. LV Configuration: SLV-3D Centaur AC-31 / Centaur D-1AR 5010D.
  • Intelsat 4 F-7 - . Mass: 1,410 kg (3,100 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 4. Completed Operations Date: 1984-02-23 . USAF Sat Cat: 6796 . COSPAR: 1973-058A. Apogee: 36,132 km (22,451 mi). Perigee: 36,080 km (22,410 mi). Inclination: 10.4000 deg. Period: 1,452.50 min. Over Atlantic Ocean. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit over the Atlantic Ocean at 30 deg W in 1973-1976 over the Atlantic Ocean 1 deg W in 1976-1980; over the Indian Ocean 56 deg E in 1980-1981; over the Pacific Ocean179 deg E in 1981-1982; over the Atlantic Ocean 53 deg W in 1982-1983 As of 31 August 2001 located at 74.52 deg W drifting at 4.067 deg W per day. As of 2007 Mar 10 located at 19.61E drifting at 4.058W degrees per day.

1974 August 23 - . 19:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHOK. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1976 August 23 - .
1976 August 23 - .
  • Start Delta F modification, Enterprise (OV-101) - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise.

1977 August 23 - . 23:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1978 August 23 - . 17:31 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • - . Nation: USA. Agency: MRN. Apogee: 39 km (24 mi).

1979 August 23 - . Launch Site: Edwards.
  • Enterprise / shuttle carrier demate, Edwards - . Nation: USA. Program: STS. Class: Manned. Type: Manned spaceplane. Spacecraft: Enterprise. Summary: Enterprise (OV-101)/ shuttle carrier demate, Edwards.

1979 August 23 - . Launch Site: Natal. LV Family: Sonda. Launch Vehicle: Sonda 3. LV Configuration: Sonda 3-M2 XV-07.
  • Ionosphere mission - . Nation: Brazil. Agency: IAE. Apogee: 248 km (154 mi).

1980 August 23 - .
  • Death of Boris Nikolayevich Petrov - . Nation: Russia. Related Persons: Petrov, Boris. Summary: Russian engineer, Department Chief 1951-1980 of the Institute of Control Problems, chair of the Inter-Cosmos Council, which promoted cooperation in space among eastern European nations during the height of the Cold War, 1966-1980..

1983 August 23 - .
1983 August 23 - . 11:05 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1493 - . 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: 1983-09-06 . USAF Sat Cat: 14299 . COSPAR: 1983-087A. Apogee: 362 km (224 mi). Perigee: 188 km (116 mi). Inclination: 72.9000 deg. Period: 90.00 min. Summary: Photo surveillance; returned film capsule..

1984 August 23 - . 09:11 GMT - . Launch Site: Wallops Island. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.42GE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).

1985 August 23 - . Launch Site: Vandenberg.
  • First Peacekeeper ICBM "cold launch" - . Nation: USA. Summary: First Peacekeeper ICBM 'cold launch' from an underground silo (LF08). First eight launches conducted from an above ground launch stand at Test Pad 01..

1985 August 23 - . 22:33 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 1677 - . Mass: 3,800 kg (8,300 lb). Nation: USSR. Agency: MO. Program: RORSAT. Class: Surveillance. Type: Military naval surveillance radar satellite. Spacecraft: US-A. Decay Date: 1985-12-14 . USAF Sat Cat: 16192 . COSPAR: 1985-075B. Apogee: 1,001 km (621 mi). Perigee: 880 km (540 mi). Inclination: 64.7000 deg. Period: 103.90 min. Summary: Ocean surveillance; nuclear powered..

1986 August 23 - . 18:25 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-15.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1987 August 23 - . 19:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1988 August 23 - . 09:20 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1964 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 15.00 days. Decay Date: 1988-09-07 . USAF Sat Cat: 19412 . COSPAR: 1988-072A. Apogee: 271 km (168 mi). Perigee: 206 km (128 mi). Inclination: 70.0000 deg. Period: 89.30 min. Summary: Military cartographic satellite; returned film capsule..

1988 August 23 - . 11:15 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1965 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs F2. Duration: 30.00 days. Decay Date: 1988-09-22 . USAF Sat Cat: 19414 . COSPAR: 1988-073A. Apogee: 228 km (141 mi). Perigee: 179 km (111 mi). Inclination: 82.3000 deg. Period: 88.60 min. Summary: Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation. .

1989 August 23 - . 03:09 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 T15000-037.
  • Progress M-1 - . Payload: Progress M s/n 201. Mass: 7,270 kg (16,020 lb). Nation: USSR. Agency: MOM. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Mir EO-5. Spacecraft: Progress M. Duration: 100.34 days. Completed Operations Date: 1989-12-01 11:21:28 . Decay Date: 1989-12-01 11:21:28 . USAF Sat Cat: 20191 . COSPAR: 1989-066A. Apogee: 217 km (134 mi). Perigee: 187 km (116 mi). Inclination: 51.6000 deg. Period: 88.50 min. Unmanned supply vehicle to Mir; first flight of new vehicle design. Tested on-board systems under different conditions and delivered expendable materials and sundry cargo to the Mir manned space station. Docked with Mir on 25 Aug 1989 05:19:02 GMT. Undocked on 1 Dec 1989 09:02:23 GMT. Destroyed in reentry on 1 Dec 1989 11:21:00 GMT. Total free-flight time 2.19 days. Total docked time 98.16 days.

1989 August 23 - . 18:05 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 36.59UL.
  • Extreme ultraviolet Spectrometer Aeronomy / solar extreme ultraviolet mission - . Nation: USA. Agency: NASA. Apogee: 333 km (206 mi).

1990 August 23 - . 16:17 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC90/19. Launch Pad: LC90/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-2.
  • Cosmos 2096 - . Mass: 3,000 kg (6,600 lb). Nation: USSR. Agency: MO. Program: EORSAT. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: US-P. Decay Date: 1992-08-30 . USAF Sat Cat: 20765 . COSPAR: 1990-075A. Apogee: 415 km (257 mi). Perigee: 402 km (249 mi). Inclination: 65.0000 deg. Period: 92.70 min. Summary: Ocean surveillance..

1994 August 23 - . 14:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/4. Launch Pad: LC43/4?. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
  • Molniya-3-46 - . Payload: Molniya-3 s/n 60. Mass: 1,600 kg (3,500 lb). Nation: Russia. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-3. Decay Date: 2009-02-10 . USAF Sat Cat: 23211 . COSPAR: 1994-051A. Apogee: 38,837 km (24,132 mi). Perigee: 1,518 km (943 mi). Inclination: 64.9000 deg. Period: 717.80 min. Summary: Replaced Molniya 3-40. As of 1994, the Molniya 3 constellation consisted of Molniya 3-36, 3-38, 3-39, 3-42, 3-43, 3-44, 3-45, and 3-46..

1995 August 23 - . 02:05 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P. LV Configuration: MT-135P-R935.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 60 km (37 mi).

1997 August 23 - . 06:51 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC6. LV Family: Athena. Launch Vehicle: Athena-1. LV Configuration: LMLV-1 LM-002.
  • Lewis - . Payload: SSTI/Lewis. Nation: USA. Agency: TRW; NASA. Manufacturer: Chantilly. Class: Earth. Type: Earth resources satellite. Spacecraft: Lewis. Decay Date: 1997-09-28 . USAF Sat Cat: 24909 . COSPAR: 1997-044A. Apogee: 134 km (83 mi). Perigee: 124 km (77 mi). Inclination: 97.5000 deg. Period: 87.10 min. Summary: Reentered Sep 28.

1999 August 23 - . 10:30 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A TR-S-06 Sphere.
  • TRAMP-99 Aeronomy mission - . Nation: Norway. Agency: DLR. Apogee: 75 km (46 mi).

2000 August 23 - . 11:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. Launch Pad: SLC17B. LV Family: Delta. Launch Vehicle: Delta 3. LV Configuration: Delta 8930 D280.
  • DM-F3 - . Payload: Dummy Payload. Mass: 4,348 kg (9,585 lb). Nation: USA. Agency: Seal Beach. Manufacturer: Douglas. Class: Technology. Type: Navigation technology satellite. Decay Date: 2009-02-04 . USAF Sat Cat: 26475 . COSPAR: 2000-048A. Apogee: 19,547 km (12,145 mi). Perigee: 212 km (131 mi). Inclination: 27.6000 deg. Vehicle Demonstration. Return to flight following earlier failure. The third Boeing Delta III launch was financed by the company and carried a dummy payload in order to bolster customer confidence in the new launch vehicle. The second stage ignited at an altitude of 158 km and the RL-10 shut off as planned in a 157 x 1363 km x 29.5 deg parking orbit. The engine fired again until fuel depletion, to place the vehicle in a geostationary transfer orbit of 190 x 20,655 km x 27.6 deg. This was much lower than that planned (23,400 km plus or minus 3,000 km) due to the fuel temperature and atmospheric conditions on the day of launch. The DM-F3 dummy payload was a mass model of the Orion 3 HS-601 satellite launched on the second Delta 3. The 4348 kg model was a 2.0m diameter, 1.7m high cylinder with two circular end plates, painted with black and white patterns. It was to be used by US Air Force researchers as a calibration target.

2001 August 23 - .
2002 August 23 - .
  • International Space Station Status Report #02-37 - . Nation: USA. Related Persons: Korzun; Whitson. Program: ISS. Flight: ISS EO-5. The Expedition Five crew spent a large portion of its week preparing for the next scheduled spacewalk. Commander Valery Korzun and Flight Engineer Sergei Treschev plan to leave the Pirs Docking Compartment of the International Space Station around 12:00 a.m. Central time (0500 GMT) Monday, Aug. 26, to begin a six-hour spacewalk. While Korzun and Treschev work outside, Flight Engineer Peggy Whitson will tend to space station systems and assist the spacewalkers as necessary. She will also maneuver the Canadarm2 to provide camera views of the cosmonauts for the two mission control centers. Additional Details: International Space Station Status Report #02-37.

2004 August 23 - .
  • Cassini, Periapsis Raise Maneuver (OTM-2), Successful - . Nation: USA. Spacecraft: Cassini.

2005 August 23 - . 21:10 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. Launch Pad: LC109/95. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Kirari - . Mass: 570 kg (1,250 lb). Nation: Japan. Agency: JAXA. Manufacturer: Toshiba. Class: Technology. Type: Navigation technology satellite. Spacecraft: Kirari. USAF Sat Cat: 28809 . COSPAR: 2005-031A. Apogee: 614 km (381 mi). Perigee: 596 km (370 mi). Inclination: 97.8000 deg. Period: 96.80 min. Moved from J-1A . Delayed from August 15. Optical Inter-Orbit Communications Engineering Test Satellite. Its laser communications experiment was be used in with ESA's Artemis geostationary satellite. The satellite was renamed Kirari (twinkle) after launch.
  • Reimei - . Payload: Index. Mass: 60 kg (132 lb). Nation: Japan. Agency: JAXA. Manufacturer: Mitsubishi. Class: Technology. Type: Navigation technology satellite. Spacecraft: Reimei. USAF Sat Cat: 28810 . COSPAR: 2005-031B. Apogee: 650 km (400 mi). Perigee: 601 km (373 mi). Inclination: 97.8000 deg. Period: 97.20 min. Summary: Plasma Science Technology. INDEX, renamed Reimei ("Dawn") after launch, was a test satellite with new lightweight satellite components, and a demonstration auroral imager payload..

2007 August 23 - . 08:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minotaur. Launch Vehicle: Minotaur 2. LV Configuration: Minotaur 2 TLV-7.
  • TLV-7 - . Nation: USA. Agency: USAF. Apogee: 1,300 km (800 mi). Mission 2a sensor target for the NFIRE satellite. The Minotaur II, a three-stage refurbished Minuteman 2 missile with a new guidance and payload section, was aimed to pass within 4 and 20 km of the NFIRE satellite while its third stage motor was burning, to allow NFIRE's sensors to characterize the the rocket and its exhaust. The Missile Defense Agency reported that Mission 2a was successful.

2009 August 23 - . 16:01 GMT - . Launch Site: Vandenberg. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • Mk 12 RV? GT195 - . Mass: 1,300 kg (2,800 lb). Nation: USA. Agency: USAF. Summary: Operational test.

2010 August 23 - . 17:57 GMT - . Launch Site: White Sands. LV Family: Black Brant. Launch Vehicle: Black Brant 9.
  • NASA 36.219US - . Nation: USA. Agency: NASA Greenbelt. Apogee: 295 km (183 mi). Summary: Solar UV payload (Rapid Acquisition Imaging Spectropgraph)..

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