Encyclopedia Astronautica
August 02


August 02 Chronology


1934 August 2 - .
1944 August 2 - . Launch Site: Peenemuende. Launch Complex: Peenemuende GWO. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 18204.
1949 August 2 - .
1950 August 2 - . Launch Site: Camp de Suippes. LV Family: Veronique. Launch Vehicle: Veronique R. LV Configuration: Veronique R R1. FAILURE: Failure.
  • Test mission - . Nation: France. Agency: LRBA. Apogee: 2.00 km (1.20 mi).

1951 August 2 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Deacon.
  • Boojum model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1954 August 2 - . 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 320.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1957 August 2 - . Launch Site: Wallops Island. LV Family: Honest John. Launch Vehicle: HJ Nike.
  • Flat re-entry vehicle test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1958 August 2 - . 05:47 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-2. Launch Vehicle: R-2A. LV Configuration: R-2A No. 6.
  • Ionosphere / biological mission - . Nation: USSR. Agency: MVS. Apogee: 211 km (131 mi).

1958 August 2 - . 22:16 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC13. LV Family: Atlas. Launch Vehicle: Atlas B. LV Configuration: Atlas B 4B.
  • Research and development test - . Nation: USA. Agency: USAF. Apogee: 900 km (550 mi). Summary: Second full-powered flight of USAF Atlas ICBM traveled 2,500 miles with radio-inertial guidance, fully successful..

1960 August 2 - . 03:14 GMT - . Launch Site: Wallops Island. LV Family: Strongarm. Launch Vehicle: Strongarm. FAILURE: Failure.
  • Ionosphere mission - . Nation: USA. Agency: USA BRL. Apogee: 550 km (340 mi).

1960 August 2 - . 13:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NN2.32.
  • Ionosphere mission - . Nation: USA. Agency: NRL. Apogee: 148 km (91 mi).

1961 August 2 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • Apollo launch site study begun. - . Nation: USA. Program: Apollo. NASA headquarters announced that it was making a world-wide study of possible launching sites for Moon vehicles; the size, power, noise, and possible hazards of Saturn-Nova type rockets requiring greater isolation for public safety than presently available.

1961 August 2 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2X-21.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1962 August 2 - . LV Family: Saturn I; Saturn V.
  • Apollo lunar bus - . Nation: USA. Program: Apollo. Spacecraft: Lunar Bus. NASA's Office of Manned Space Flight issued Requests for Proposals for a study of the lunar "bus" and studies for payloads which could be handled by the C-1B and C-5 launch vehicles. Contract awards were expected by September 1 and completion of the studies by December 1.

1962 August 2 - . 00:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Thor Agena D. LV Configuration: Thor Agena D 344 / Agena D 1152.
  • KH-4 9041 - . Payload: KH-4 s/n 9041 / Agena D 1152. Mass: 1,150 kg (2,530 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-4. Decay Date: 1962-08-22 . USAF Sat Cat: 360 . COSPAR: 1962-A-Kappa-1. Apogee: 423 km (262 mi). Perigee: 212 km (131 mi). Inclination: 83.0000 deg. Period: 90.80 min. Summary: KH-4; film capsule recovered 4.1 days later. Severe corona and radiation fog..

1962 August 2 - . 17:56 GMT - . Launch Site: Mud Lake DZ. Launch Pad: 37.9 N x 117.1 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3-8-16.
  • X-15A MH-96 fixed gain test - . Nation: USA. Agency: NASA; USAF. Apogee: 44 km (27 mi). Summary: Maximum Speed - 5532 kph. Maximum Altitude - 44040 m..

1963 August 2 - .
  • No further Soviet manned flights in 1963 - . Nation: USSR. Related Persons: Tereshkova; Korolev. Flight: Vostok 7. It is clear that there may be no Soviet manned flights in 1963, and certainly not in the spring. It is possible the unmanned biosat Vostok will be flown in the second half of 1963. Korolev's plate is full with other work -- Soyuz development, several Zenit reconnaissance satellite launches, lots of Luniks. Meanwhile Kamanin is completely occupied with cosmonaut tours and publicity. Over 200,000 cosmonaut fan letters have been received -- they can't handle them all, a special unit will have to be created just to handle the mail. The KGB has assigned Yevgeniya Pavlovna Kassirova to accompany Tereshkova on her travels. She is a good choice, has foreign travel experience and excellent English.

1963 August 2 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • Grumman to design the LEM to have a thrusting capability with the Apollo CSM attached - . Nation: USA. Program: Apollo. Spacecraft: Apollo LM; CSM SPS. North American asked MSC if Grumman was designing the LEM to have a thrusting capability with the CSM attached and, if not, did NASA intend to require the additional effort by Grumman to provide this capability. North American had been proceeding on the assumption that, should the service propulsion system (SPS) fail during translunar flight, the LEM would make any course corrections needed to ensure a safe return trajectory. Additional Details: Grumman to design the LEM to have a thrusting capability with the Apollo CSM attached.

1963 August 2 - . Launch Site: Point Mugu. Launch Platform: F-3B. LV Family: Sparoair. Launch Vehicle: Sparoair I.
  • Ultraviolet astronomy mission - . Nation: USA. Agency: USN NMC. Apogee: 107 km (66 mi).

1963 August 2 - . 21:43 GMT - . Launch Site: Wallops Island. LV Family: Sergeant. Launch Vehicle: Shotput. LV Configuration: Shotput 7.
  • San Marco Satellite test - . Nation: USA. Agency: NASA. Apogee: 294 km (182 mi).

1963 August 2 - . 23:33 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.75UA.
  • Density Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 151 km (93 mi).

1965 August 2 - .
  • Marquardt to build Apollo Block II SM reaction control system engines - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM RCS. NASA's office at Downey, Calif., approved the contract with the Marquardt Corporation for the procurement of Block II SM reaction control system engines. Estimated cost of the fixed price contract would be $6.5 million. Marquardt was supplying the Block I SM engines.

1965 August 2 - .
  • First prototype Apollo portable life support system - . Nation: USA. Program: Apollo. Spacecraft: A7L. Summary: Hamilton Standard shipped the first prototype portable life support system to Houston, where it would undergo testing by the Crew Systems Division..

1966 August 2 - .
  • S-IVB airlock module (AM) experiment planned as part of the dual-launch Apollo-Saturn 209-210 mission. - . Nation: USA. Related Persons: Mueller; Seamans. Spacecraft: Orbital Workshop. George E. Mueller, Associate Administrator for Manned Space Flight, recommended to Deputy Administrator Robert C. Seamans, Jr., that NASA proceed with its procurement effort on an S-IVB airlock module (AM) experiment as part of the dual-launch Apollo-Saturn 209-210 mission. The AM, to replace a LM aboard one of the vehicles, was to serve as the module affording a docking adapter at one end to permit CSM docking and at the other end a sealed connection to a hatch in the spent S-IVB stage of the rocket. Additional Details: S-IVB airlock module (AM) experiment planned as part of the dual-launch Apollo-Saturn 209-210 mission..

1966 August 2 - .
  • Letter to Central Committee on OKB-1 actions. - . Nation: USSR. Related Persons: Malinovskiy. Program: Soyuz; Lunar L1; Lunar L3. Summary: Malinovskiy decides to send the letter to the Central Committee complaining about MOM and OKB-1's after two days of indecision..

1966 August 2 - . Launch Site: White Sands. Launch Complex: White Sands LC50. Launch Vehicle: Sprint. LV Configuration: Sprint ABM FLA-5. FAILURE: Failure.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 0 km ( mi).

1966 August 2 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-102.
  • ACS technology mission - . Nation: USA. Agency: Sandia. Apogee: 306 km (190 mi).

1966 August 2 - . Launch Site: San Nicolas. LV Family: Terrier. Launch Vehicle: Terrier/551.
  • Flight test 2 test - . Nation: USA. Agency: NMC. Apogee: 443 km (275 mi).

1966 August 2 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-29.
  • Scan Converter Technology mission - . Nation: USA. Agency: Sandia. Apogee: 303 km (188 mi).

1967 August 2 - .
1968 August 2 - .
  • Reduced L3 recovery forces accepted. - . Nation: USSR. Related Persons: Vershinin; Afanasyev, Sergei; Keldysh; Ryabikov; Gagarin. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. Summary: Vershinin, Afanasyev, Keldysh, and Ryabikov accept the reduced recovery forces estimate. Meanwhile a letter from the cosmonauts disputes the Gagarin crash investigation finding ('pilot error resulting in an abrupt manoeuvre')..

1968 August 2 - . 06:19 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 5B. LV Configuration: Black Brant VB ADD-VB-18.
  • Aeronomy / ionosphere / Fields mission - . Nation: Canada. Agency: NRCC. Apogee: 284 km (176 mi).

1969 August 2 - . 11:37 GMT - . Launch Site: South Uist. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P12H.
  • SpE fine scale Ionosphere mission - . Nation: UK. Agency: SRC. Apogee: 126 km (78 mi).

1971 August 2 - .
  • EVA Apollo 15-5 - . Crew: Scott; Irwin. EVA Type: Internal Vehicular Activity. EVA Duration: 0.0014 days. Nation: USA. Related Persons: Scott; Irwin. Program: Apollo. Class: Moon. Type: Manned lunar lander. Flight: Apollo 15. Spacecraft: Apollo LM. Summary: Threw excess equipment out of LM before lift-off..

1971 August 2 - .
  • Apollo 15 departs lunar surface - . Nation: USA. Flight: Apollo 15. Liftoff of the ascent stage of the LM, the first to be televised via the camera on the rover, occurred at 1:11 p.m. EDT. About two hours later the LM and CSM rendezvoused and docked, and film, equipment, and 77 kilograms of lunar samples were transferred from the LM to the CSM. The ascent stage was jettisoned and hit the lunar surface at 11:04 p.m. EDT. Its impact was recorded by the Apollo 12, Apollo 14, and Apollo 15 seismometers, left on the moon during those missions. Additional Details: Apollo 15 departs lunar surface.

1971 August 2 - . 08:52 GMT - .
  • EVA Apollo 15-4 - . Crew: Scott; Irwin. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.20 days. Nation: USA. Related Persons: Scott; Irwin. Program: Apollo. Class: Moon. Type: Manned lunar lander. Flight: Apollo 15. Spacecraft: Apollo LRV. Summary: Drove in lunar rover to Hadley Rille..

1972 August 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-7W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 August 2 - . 08:15 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 513 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4M. Duration: 14.00 days. Decay Date: 1972-08-15 . USAF Sat Cat: 6135 . COSPAR: 1972-060A. Apogee: 307 km (190 mi). Perigee: 172 km (106 mi). Inclination: 64.9000 deg. Period: 89.30 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1973 August 2 - .
  • Skylab 3 RCS problems - . Nation: USA. Flight: Skylab 3. On 2 August the service module reaction control system engines were inhibited, and the isolation valves closed because of another leak. Acceptable control modes and deorbit and entry procedures were defined, consistent with the constraints imposed by the two reaction control system problems.

1973 August 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • FOT GT113M Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1974 August 2 - . 20:00 GMT - . Launch Site: Poker Flat. Launch Vehicle: Rocketsonde.
  • Met Para, Datasonde - . Nation: USA. Agency: MRN. Apogee: 74 km (45 mi).

1975 August 2 - . 01:14 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Starute, Datasonde - . Nation: USA. Agency: MRN. Apogee: 76 km (47 mi).

1976 August 2 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle carrier aircraft - . Nation: USA. Summary: Work begins on modification of 747 N9668 to carry the shuttle on its back in a $30 million contract. After completion the aircraft is rolled out as N905NA..

1976 August 2 - .
  • Start carrier aircraft modification - . Nation: USA. Program: STS.

1977 August 2 - . 14:37 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 68 km (42 mi).

1978 August 2 - . 21:36 GMT - . Launch Site: Barking Sands. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 89 km (55 mi).

1979 August 2 - . Launch Site: Baikonur. Launch Complex: Baikonur LC170. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100U 15A16.
  • Joint flight trials launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1982 August 2 - .
  • Death of Nikolai Alekseyevich Pilyugin - . Nation: Russia. Related Persons: Pilyugin. Summary: Russian chief designer. Chief Designer 1948-1982 of Nll-885 and NII AP. Specialised in missile and spaceship guidance..

1983 August 2 - . 20:45 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1984 August 2 - . 08:38 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL.
  • Cosmos 1586 - . Payload: Oko #36. Mass: 1,250 kg (2,750 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Oko. USAF Sat Cat: 15147 . COSPAR: 1984-079A. Apogee: 36,751 km (22,835 mi). Perigee: 3,607 km (2,241 mi). Inclination: 66.4000 deg. Period: 717.90 min. Summary: Replaced Cosmos 1456. Covered Oko constellation plane 4 - 35 degree longitude of ascending node..

1984 August 2 - . 20:30 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima N. LV Family: Delta. Launch Vehicle: N-2. LV Configuration: N-2 N-13(F).
  • Himawari 3 - . Payload: GMS 3. Mass: 303 kg (668 lb). Nation: Japan. Agency: NASDA. Class: Earth. Type: Weather satellite. Spacecraft: GMS. Completed Operations Date: 1995-06-22 . USAF Sat Cat: 15152 . COSPAR: 1984-080A. Apogee: 35,942 km (22,333 mi). Perigee: 35,877 km (22,292 mi). Inclination: 9.8000 deg. Period: 1,442.40 min. Stationed at 140 deg E; also studied alpha particles, electrons. GMS-3 (Himawari-3). Launch 2030 GMT. Improvement of meteorological observation. Development of meteorological satellite technology. N Launch vehicle flight no 13. Launching organization NASDA. Positioned in geosynchronous orbit at 140 deg E in 1984-1989; 120 deg E in 1989-1995 As of 28 August 2001 located at 146.92 deg E drifting at 1.558 deg W per day. As of 2007 Mar 11 located at 168.90W drifting at 1.566W degrees per day.

1985 August 2 - . Launch Site: Baikonur. Launch Complex: Baikonur Jubilee.
1985 August 2 - . 07:15 GMT - .
1985 August 2 - . 11:40 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1671 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 14.00 days. Decay Date: 1985-08-16 . USAF Sat Cat: 15931 . COSPAR: 1985-065A. Apogee: 281 km (174 mi). Perigee: 195 km (121 mi). Inclination: 72.9000 deg. Period: 89.30 min. Summary: Military cartographic satellite; returned film capsule; maneuverable..

1986 August 2 - . 01:35 GMT - . Launch Site: ETR Launch Area. Launch Platform: UK S27. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3TK/A3R.
  • Chevaline demonstration and shakedown operations launch - . Nation: UK. Agency: RN. Apogee: 1,000 km (600 mi).

1986 August 2 - . 09:20 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1768 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Resurs F1-14F40. Duration: 14.00 days. Decay Date: 1986-08-16 . USAF Sat Cat: 16890 . COSPAR: 1986-058A. Apogee: 273 km (169 mi). Perigee: 180 km (110 mi). Inclination: 82.6000 deg. Period: 89.00 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 2 - . 11:29 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2035 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 14.00 days. Decay Date: 1989-08-16 . USAF Sat Cat: 20151 . COSPAR: 1989-060A. Apogee: 236 km (146 mi). Perigee: 176 km (109 mi). Inclination: 82.6000 deg. Period: 88.60 min. Summary: Military cartographic satellite; returned film capsule..

1990 August 2 - . Launch Vehicle: Babylon Gun.
  • Iraq invades Kuwait. - . Nation: Iraq. Summary: Iraq invaded Kuwait, precipitating the Gulf War. This ended Western covert sponsorship of Iraqi supergun, space launch, and long-range missile projects..

1990 August 2 - .
  • Iraqi troops invade Kuwait and seize petroleum reserves, setting off Persian Gulf War - . Nation: International.

1990 August 2 - . 05:39 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 6925. LV Configuration: Delta 6925 D197.
  • USA 63 - . Payload: GPS 2-8 / GPS SVN 21. Mass: 1,665 kg (3,670 lb). Nation: USA. Agency: USAF. Manufacturer: Seal Beach. Program: Navstar. Class: Navigation. Type: Navigation satellite. Spacecraft: GPS Block 2 and 2A. USAF Sat Cat: 20724 . COSPAR: 1990-068A. Apogee: 20,468 km (12,718 mi). Perigee: 19,896 km (12,362 mi). Inclination: 54.7000 deg. Period: 718.00 min. Summary: Global Positioning System. Placed in Plane E Slot 2..

1990 August 2 - . 10:07 GMT - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Terrier. Launch Vehicle: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.29UE.
  • EQUIS Spread F Plasma mission - . Nation: USA. Agency: NASA. Apogee: 480 km (290 mi).

1990 August 2 - . 22:40 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna S. LV Family: Skylark. Launch Vehicle: Skylark 7. LV Configuration: Skylark 7 DLR K-GR-182.
  • SISSI 3 Aeronomy mission - . Nation: Germany. Agency: DLR. Apogee: 239 km (148 mi).

1991 August 2 - . 15:02 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-43.
  • STS-43 - . Call Sign: Atlantis. Crew: Adamson; Baker, Mike; Blaha; Low; Lucid. Payload: Atlantis F09 / TDRS 5 [IUS]. Mass: 21,265 kg (46,881 lb). Nation: USA. Related Persons: Adamson; Baker, Mike; Blaha; Low; Lucid. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-43. Spacecraft: Atlantis. Duration: 8.89 days. Decay Date: 1991-08-11 . USAF Sat Cat: 21638 . COSPAR: 1991-054A. Apogee: 306 km (190 mi). Perigee: 301 km (187 mi). Inclination: 28.5000 deg. Period: 90.60 min. Manned five crew. Deployed TDRS 5 satellite. Payloads: Tracking and Data Relay Satellite (TDRS)-E/lnertial Upper Stage (lUS), Space Station Heatpipe Advanced Radiator Element (SHARE)-ll, Shuttle Solar Backscatter Ultraviolet (SSBUV) instrument 03, Optical Communications Through the Shuttle Window (OCTW), Air Force Maui Optical Site (AMOS) Calibration Test, Auroral Photography Experiment (APE)-B, Bioserve-lnstrumentation Technology Associates Materials Dispersion Apparatus (BlMDA)-02, Investigations Into Polymer Membrane Processing (IPMP)-03, Protein Crystal Growth Ill Block Il, Space Acceleration Measure-ment System (SAMS), Solid Surface Combustion Experiment (SSCE)-02, Tank Pressure Control Experiment (TPCE).
  • TDRS 5 - . Payload: TDRS E. Mass: 2,200 kg (4,800 lb). Nation: USA. Agency: NASA Greenbelt. Program: STS. Class: Communications. Type: Civilian communications satellite. Spacecraft: TDRS. USAF Sat Cat: 21639 . COSPAR: 1991-054B. Apogee: 35,790 km (22,230 mi). Perigee: 35,783 km (22,234 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. NASA communications; 174 deg W; deployed from STS-43 8/2/91. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). Positioned in geosynchronous orbit at 174 deg W in 1991-1999 As of 1 September 2001 located at 174.28 deg W drifting at 0.011 deg E per day. As of 2007 Mar 10 located at 171.61W drifting at 0.006W degrees per day.

1993 August 2 - . 01:02 GMT - . Launch Site: Kiruna. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR K-NO-204 NLC-93.
  • SSC Decimals B Aeronomy mission - . Nation: Germany. Agency: DLR; SSC. Apogee: 105 km (65 mi).

1993 August 2 - . 19:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Titan. Launch Vehicle: Titan 403A. LV Configuration: Titan 403A K-11 (45F-9). FAILURE: Radial cut inadvertently made in SRM during repairs resulted in explosion of SRM and vehicle at T+101 seconds.. Failed Stage: 0.
  • NOSS 19 - . Payload: NOSS B-3. Nation: USA. Agency: USN. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: NOSS-2. Decay Date: 1993-08-02 . COSPAR: F930802A. Apogee: 33 km (20 mi). Summary: Third attempted launch by Titan 4 of new generation of NOSS naval reconnaissance satellites. No known launches of this system thereafter..
  • TLD - . Payload: TLD. Nation: USA. Agency: USAF AFMC. Spacecraft: NOSS. COSPAR: F930802E. Apogee: 33 km (20 mi).
  • SSU - . Payload: SSU. Nation: USA. Agency: USAF AFMC. Spacecraft: NOSS. COSPAR: F930802C. Apogee: 33 km (20 mi).
  • SSU - . Payload: SSU. Nation: USA. Agency: USAF AFMC. Spacecraft: NOSS. COSPAR: F930802D. Apogee: 33 km (20 mi).
  • SSU - . Payload: SSU. Nation: USA. Agency: USAF AFMC. Spacecraft: NOSS. COSPAR: F930802B. Apogee: 33 km (20 mi).

1994 August 2 - . 20:00 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M.
  • Cosmos 2285 - . Mass: 825 kg (1,818 lb). Nation: Russia. Agency: MO. Class: Military. Type: Radar calibration target. Spacecraft: Taifun-1. USAF Sat Cat: 23189 . COSPAR: 1994-045A. Apogee: 1,013 km (629 mi). Perigee: 974 km (605 mi). Inclination: 74.0300 deg. Period: 104.98 min. Summary: Radar calibration mission..

1995 August 2 - . 23:59 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-2BL N15000-294 10M127S.
  • Interbol 1 - . Payload: SO-M2 s/n 511. Mass: 1,250 kg (2,750 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Prognoz-M. Decay Date: 2000-10-16 . USAF Sat Cat: 23632 . COSPAR: 1995-039A. Apogee: 188,331 km (117,023 mi). Perigee: 4,426 km (2,750 mi). Inclination: 68.2000 deg. Period: 5,461.60 min. Summary: Particles and fields research. Paired with Magion 4 subsatellite..
  • Magion 4 - . Payload: S2. Mass: 50 kg (110 lb). Nation: Czech Republic. Agency: VKS. Program: Intercosmos. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Magion. USAF Sat Cat: 23646 . COSPAR: 1995-039F. Apogee: 175,449 km (109,018 mi). Perigee: 17,068 km (10,605 mi). Inclination: 70.3000 deg. Period: 5,454.00 min. Summary: Deployed from Interbol-1 on 8/3/95; solar wind studies in conjunction with Interbol-1..

1996 August 2 - .
  • Death of Aleksandr Emmanuelovich Nudelman - . Nation: Russia. Related Persons: Nudelman. Summary: Russian engineer. Chief Designer 1965-1987 of OKB8-16. Pre-eminent designer of aircraft guns in the Soviet Union. Adapted his aircraft designs for self-defence space guns for Kozlov's Soyuz VI and Chelomei's Almaz spacecraft..

1996 August 2 - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Standard-ER. Launch Vehicle: Standard SM-2ER Block IV. LV Configuration: SM-2-IV NTW ETR-1A.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 10 km (6 mi).

1998 August 2 - . 16:24 GMT - . Launch Site: Wallops Island DZ. Launch Pad: 37.0 N x 72.0 W. Launch Platform: L-1011. LV Family: Pegasus. Launch Vehicle: Pegasus XL/HAPS. LV Configuration: Pegasus XL/HAPS F22.
  • Orbcomm B5 - . Payload: Orbcomm s/n FM17. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25413 . COSPAR: 1998-046A. Apogee: 824 km (512 mi). Perigee: 813 km (505 mi). Inclination: 45.0000 deg. Period: 101.28 min. Summary: Plane B. Ascending node 61 degrees..
  • Orbcomm B6 - . Payload: Orbcomm s/n FM18. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25414 . COSPAR: 1998-046B. Apogee: 827 km (513 mi). Perigee: 810 km (500 mi). Inclination: 45.0000 deg. Period: 101.28 min. Summary: Plane B. Ascending node 59.7 degrees..
  • Orbcomm B2 - . Payload: Orbcomm s/n FM14. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25419 . COSPAR: 1998-046G. Apogee: 826 km (513 mi). Perigee: 811 km (503 mi). Inclination: 45.0000 deg. Period: 101.28 min. Summary: Plane B. Ascending node 60.4 degrees..
  • Orbcomm B3 - . Payload: Orbcomm s/n FM15. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25418 . COSPAR: 1998-046F. Apogee: 825 km (512 mi). Perigee: 812 km (504 mi). Inclination: 45.0100 deg. Period: 101.28 min. Summary: Plane B. Ascending node 60 degrees..
  • Orbcomm B4 - . Payload: Orbcomm s/n FM16. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25417 . COSPAR: 1998-046E. Apogee: 825 km (512 mi). Perigee: 812 km (504 mi). Inclination: 45.0000 deg. Period: 101.28 min. Summary: Plane B. Ascending node 59.9 degrees..
  • Orbcomm B7 - . Payload: Orbcomm s/n FM19. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25415 . COSPAR: 1998-046C. Apogee: 828 km (514 mi). Perigee: 809 km (502 mi). Inclination: 45.0000 deg. Period: 101.28 min. Summary: Plane B. Ascending node 61.1 degrees..
  • Orbcomm B8 - . Payload: Orbcomm s/n FM20. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25416 . COSPAR: 1998-046D. Apogee: 826 km (513 mi). Perigee: 811 km (503 mi). Inclination: 45.0000 deg. Period: 101.28 min. Summary: Plane B. Ascending node 61.2 degrees..
  • Orbcomm B1 - . Payload: Orbcomm s/n FM13. Nation: USA. Agency: Orbcomm. Manufacturer: Germantown. Program: Orbcomm. Class: Communications. Type: Civilian communications satellite. Spacecraft: Orbcomm. USAF Sat Cat: 25420 . COSPAR: 1998-046H. Apogee: 824 km (512 mi). Perigee: 813 km (505 mi). Inclination: 45.0000 deg. Period: 101.27 min. Summary: Plane B. Ascending node 60.4 degrees..

1999 August 2 - . Launch Site: Taiyuan. LV Family: DF-31. Launch Vehicle: DF-31.
  • Test mission - . Nation: China. Agency: PRC. Apogee: 1,000 km (600 mi).

1999 August 2 - . 11:37 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC94. Launch Pad: FIX. Launch Vehicle: Hera. LV Configuration: Hera 16.
  • BRV/THAAD Target mission - . Nation: USA. Agency: USA. Apogee: 270 km (160 mi).

1999 August 2 - . 11:44 GMT - . Launch Site: White Sands. Launch Vehicle: THAAD. LV Configuration: THAAD FT-11.
  • ABM test - . Nation: USA. Agency: USA. Apogee: 100 km (60 mi).

2001 August 2 - . 18:00 GMT - . Launch Site: SvalRak. Launch Complex: SvalRak LONG. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A ROFS-09.
  • ROMA Aeronomy mission - . Nation: Germany. Agency: DLR. Apogee: 100 km (60 mi).

2002 August 2 - .
  • International Space Station Status Report #02-34 - . Nation: USA. Related Persons: Korzun; Whitson. Program: ISS. Flight: ISS EO-5. Summary: Commander Valery Korzun, Astronaut Peggy Whitson and Cosmonaut Sergei Treschev completed their eighth week aboard the International Space Station, conducting scientific research, maintenance work and daily exercise routines.. Additional Details: International Space Station Status Report #02-34.

2005 August 2 - .
  • Messenger, Earth Flyby, Successful - . Nation: USA. Spacecraft: Messenger.

2005 August 2 - .
  • Cassini, Mimas Non-Targeted Flyby, Successful - . Nation: USA. Spacecraft: Cassini.

2005 August 2 - . 07:30 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C CZ2C-27 (86).
  • FSW-3 No. 4 - . Payload: FSW-21. Mass: 3,000 kg (6,600 lb). Nation: China. Agency: CAST. Manufacturer: SAST. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: FSW. Duration: 27.00 days. Decay Date: 2005-08-29 . USAF Sat Cat: 28776 . COSPAR: 2005-027A. Apogee: 259 km (160 mi). Perigee: 153 km (95 mi). Inclination: 63.0000 deg. Period: 88.60 min. Summary: Military reconnaisance satellite, which maneuvered to raise its apogee on Aug 5 and 7 to a 166 x 552 km x 63.0 orbit; and again to the same altitude on Aug 19 after the apogee decayed to 535 km. Return capsule with film aboard recovered on 29 August..

2007 August 2 - . 17:33 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz-U Sh15000-108 / ISS-26P.
  • Progress M-61 - . Payload: Progress M s/n 361. Mass: 7,200 kg (15,800 lb). Nation: Russia. Agency: RAKA. Manufacturer: Korolev. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Flight: ISS EO-15; ISS EO-15-1. Spacecraft: Progress M. Duration: 173.00 days. Decay Date: 2008-01-22 . USAF Sat Cat: 32001 . COSPAR: 2007-033A. Apogee: 346 km (214 mi). Perigee: 334 km (207 mi). Inclination: 51.6000 deg. Period: 91.30 min. International space station resupply; docked with the Pirs module at 18:40 GMT on 5 August. Undocked at 03:59 GMT on 22 December to clear port for Progress M-62 launched the next day. Deorbited over the Pacific on 22 January 2008 after a month of free flight carrying out the Plazma-Progress experiment.

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