Encyclopedia Astronautica
July 29


July 29 Chronology


1900 July 29 - .
  • Birth of Mikhail Klavdiyevich Tikhonravov - . Nation: Russia. Summary: Pioneering Soviet engineer and space visionary. Designer at Nll-4 and Korolev design bureau. Leader in development of Sputnik and Vostok spacecraft. Also performed early ICBM work and was pioneering rocketeer at GIRD and Nll-3..

1901 July 29 - .
  • Birth of Florence Lowe 'Pancho' Barnes - . Nation: USA. Summary: American pioneering aviatrix, from 1928 a barnstormer, air racer, Hollywood stunt flier; pioneered new air routes into Mexico. Opened a desert flying dude ranch in the 1930's, later a legendary watering hole for Edwards AFB test pilots..

1923 July 29 - .
  • Birth of Melvin Sherman Day - . Nation: USA. Summary: American engineer. Worked in leadership positions in the area of technical information services at the AEC (1947-1960) and NASA (1960-1970)..

1944 July 29 - . Launch Site: Peenemuende. Launch Complex: Peenemuende GWO. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 V-178.
1948 July 29 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 19R.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1950 July 29 - . 11:25 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: V-2. Launch Vehicle: Bumper-WAC. LV Configuration: Bumper-WAC Bumper 7.
  • Test mission - . Nation: USA. Agency: USA; GE. Apogee: 50 km (31 mi). Bumper No. 7 was the second missile launch from Cape Canaveral. This was to be a maximum range test of a two-stage vehicle, to study the problems in staging. The launch was delayed because of moisture in the vehicle. But when finally launched, the WAC achieved the highest sustained speed in the atmosphere to that date (Mach 9/2500 m/s) and 35.2 km altitude before impacting 305 km downrange.

1951 July 29 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1B. LV Configuration: R-1B 1.
  • Test / biology mission - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi). Summary: Electrical failure. No payload recovery. Carried dogs..

1952 July 29 - . Launch Platform: WYG-279. LV Family: Rockoon. Launch Vehicle: Rockoon.
  • First Rockoon launch attempt. - . Nation: USA. Related Persons: Van Allen. First Rockoon (balloon-launched rocket) launched from icebreaker Eastwind off Greenland by ONR group under James A. Van Allen. Rockoon low-cost technique was later used by ONR and University of Iowa research groups in 1953-55 and 1957, from ships in sea between Boston and Thule, Greenland.

1953 July 29 - .
  • Ministry of Medium Machine Building made responsible for all Soviet missile research. - . Nation: USSR. Summary: Council of Soviet Ministers (SM) Decree 'On transferring all missile work on guided missiles to the Ministry of Medium Machine Building' was issued..

1954 July 29 - . Launch Site: White Sands. LV Family: Corporal. Launch Vehicle: Corporal. LV Configuration: Corporal 1406R.
  • Test mission - . Nation: USA. Apogee: 30 km (18 mi).

1955 July 29 - . LV Family: Vanguard. Launch Vehicle: Vanguard.
  • Eisenhower approves earth satellites for IGY - . Nation: USA. Related Persons: Eisenhower. Spacecraft: Vanguard 2. Summary: President Eisenhower endorsed the IGY proposal for the launching of small earth-circling satellites..

1955 July 29 - . 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 0427.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1957 July 29 - .
  • X-1B Flight 22 - . Crew: McKay. Payload: X-1B flight 22. Nation: USA. Related Persons: McKay. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1B. Summary: NACA flight 12. Enlarged wing tips installed to simulate wing tips to be used with reaction controls. Mach 1.55 at 18,300 m..

1957 July 29 - . 21:59 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee Hi. LV Configuration: Aerobee Hi NN3.13F.
  • NRL NN3.13F Aeronomy mission - . Nation: USA. Agency: NRL. Apogee: 210 km (130 mi).

1958 July 29 - .
  • National Aeronautics and Space Act - . Nation: USA. Related Persons: Eisenhower. Summary: President Dwight D. Eisenhower signed the National Aeronautics and Space Act of 1958, Public Law 85-568, which established the National Aeronautics and Space Administration (NASA)..

1958 July 29 - . LV Family: Saturn I. Launch Vehicle: Saturn I.
  • Saturn I initial contract. - . Nation: USA. Related Persons: von Braun. Program: Apollo. Summary: ARPA gives Von Braun team contract to develop Saturn I (called 'cluster's last stand' due to design concept)..

1958 July 29 - . 05:03 GMT - . Launch Site: Point Mugu. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp NN8.56F.
  • Test / solar ultraviolet mission - . Nation: USA. Agency: USN. Apogee: 200 km (120 mi).

1959 July 29 - . 04:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 11D.
  • Research and development test - . Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi). Summary: First Atlas successful D missile flight..

1960 July 29 - . 13:13 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC14. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 50D. FAILURE: Structural failure of Atlas.. Failed Stage: 1.
  • Mercury MA-1 - . Nation: USA. Agency: USAF. Program: Mercury. Spacecraft: Mercury. Apogee: 13 km (8 mi). Mercury-Atlas 1 (MA-1) was launched from the Atlantic Missile Range in a test of spacecraft structural integrity under maximum heating conditions. After 58.5 seconds of flight, MA-1 exploded and the spacecraft was destroyed upon impact off-shore. None of the primary capsule test objectives were met. The mission objectives were to check the integrity of the spacecraft structure and afterbody shingles for a reentry associated with a critical abort and to evaluate the open-loop performance of the Atlas abort-sensing instrumentation system. The spacecraft contained no escape system and no test subject. Standard posigrade rockets were used to separate the spacecraft from the Atlas, but the retrorockets were dummies. The flight was terminated because of a launch vehicle and adapter structural failure. The spacecraft was destroyed upon impact with the water because the recovery system was not designed to actuate under the imposed flight conditions. Later most of the spacecraft, the booster engines, and the liquid oxygen vent valve were recovered from the ocean floor. Since none of the primary flight objectives was achieved, Mercury-Atlas 2 (MA-2) was planned to fulfill the mission.

1962 July 29 - . Launch Site: Baikonur. LV Family: R-9. Launch Vehicle: Romashka. FAILURE: Failure.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1963 July 29 - . 23:28 GMT - . Launch Site: Kronogard. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun K-63-2.
  • Grenades Aeronomy mission - . Nation: Sweden. Agency: RTG. Apogee: 128 km (79 mi).

1964 July 29 - . 09:22 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 248D.
  • NTMP KX-13 Target mission - . Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).

1964 July 29 - . 09:30 GMT - . Launch Site: White Sands. LV Family: Apache. Launch Vehicle: Nike Apache.
  • Sphere Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 200 km (120 mi).

1964 July 29 - . 10:07 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-5.
  • Chemical release mission - . Nation: Japan. Agency: ISAS. Apogee: 300 km (180 mi).

1964 July 29 - . 19:55 GMT - . Launch Site: Hidden Hills DZ. Launch Pad: 36.1 N x 116.0 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3-31-52.
  • X-15A Heat tran/Local Flow test - . Nation: USA. Agency: NASA; USAF. Apogee: 23 km (14 mi). Summary: Maximum Speed - 5250 kph. Maximum Altitude - 23774 m. First test of various heat-resistant panels attached to fuselage..

1965 July 29 - .
  • Failure of the Apollo A-003 Little Joe II launch vehicle not determined - . Nation: USA. Program: Apollo. Failure of the Little Joe II launch vehicle on Mission A-003 and subsequent lack of positive failure cause identification and corrective action led to a lower than desirable confidence level in the capability of the controlled version of Little Joe II to accomplish the planned A-004 mission. The test objectives for A-004 were set forth.

1966 July 29 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • The launch vehicle acceptance test of Gemini launch vehicle (GLV) 12 was conducted. - . Nation: USA. Flight: Gemini 12. The vehicle acceptance team convened August 9 and accepted the vehicle August 12. GLV-12 was deerected August 17 and formally accepted by the Air Force August 30. Stage I was airlifted to Cape Kennedy the same day. Stage II arrived September 3. Both stages were placed in controlled access storage in Hanger T pending the launch of Gemini XI and the revalidation of the launch pad, completed September 16.

1966 July 29 - . 18:43 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Titan. Launch Vehicle: Titan 3B. LV Configuration: Titan IIIB 3B-1 / Agena D 4751.
  • OPS 3014 - . Payload: KH-8 no. 01 (Gambit) / 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: 1966-08-06 . USAF Sat Cat: 2376 . COSPAR: 1966-069A. Apogee: 252 km (156 mi). Perigee: 154 km (95 mi). Inclination: 94.2000 deg. Period: 88.50 min. Summary: KH-8 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). .

1967 July 29 - .
  • Review of Soyuz trainer status. - . Nation: USSR. Related Persons: Mishin; Feoktistov; Tsybin. Program: Lunar L1; Soyuz. Spacecraft: Soyuz 7K-OK; Soyuz 7K-L1. The Soyuz simulator has not been functional for three months -- entirely the fault of Mishin and Tsybin. The L1 trainer has not been finished, and the autonomous navigation system has not completed development. There are two prototype electronic computers at TsKBEM, but they are not complete and don't work. The first L1 spacecraft was to fly in May, but it is now clear it won't be ready until September at the earliest. There will be no manned lunar flyby for the fiftieth anniversary of the October Revolution as was ordered by the Party. Additional Details: Review of Soyuz trainer status..

1967 July 29 - . 08:48 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 150F.
  • ABRES MBRV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 July 29 - .
  • Reduced L3 recovery forces. - . Nation: USSR. Related Persons: Mishin; Smirnov; Vershinin. Program: Lunar L3. Spacecraft: Soyuz 7K-LOK. Vershinin looks bad after his surgery. His loss would be a blow for Kamanin's cause - Vershinin was steadfast against the unobjective positions of Mishin and Smirnov. Vershinin had just sent yet another letter about the procurement of the 16 m centrifuge for the TsPK. This is a six-year long story. The VVS has been trying to procure this essential piece of cosmonaut training equipment since 1962, but it still has not been delivered. Vershinin also has issued a letter on the L3 recovery force issue. He points out that the resolution of the Central Committee ordered the expenditure of 600 million roubles and the commitment of 9,000 men for recovery services. Another 400 million roubles and 12,000 men were earmarked by the Rocket Forces. Despite this huge commitment, Mishin now says he doesn't need any of them, that he can bring his L1 and L3 spacecraft to precision landings within the confines of the cosmodrome, eliminating the need for any Indian Ocean recoveries. This optimism is not accepted, but it is agreed the total requirement can be reduced to 400 million roubles and 7,000 men, through use of lighter recovery ships of the Leninskiy Komsomol class, and the use of three airborne relay stations instead of nine.

1969 July 29 - .
  • Tentative planning schedule for the Apollo program - . Nation: USA. Program: Apollo. Flight: Apollo 12; Apollo 13; Apollo 14; Apollo 15; Apollo 16; Apollo 17; Apollo 18; Apollo 19; Apollo 20. Spacecraft: Surveyor; Apollo Lunar Landing. NASA issued a tentative planning schedule for the Apollo program:

    FlightLaunch PlansTentative Landing Area
    Apollo 12November 1969Oceanus Procellarum lunar lowlands
    Apollo 13March 1970Fra Mauro highlands
    Apollo 14July 1970Crater Censorinus highlands
    Apollo 15November 1970Littrow volcanic area
    Apollo 16April 1971Crater Tycho (Surveyor VII impact area)
    Apollo 17September 1971Marius Hills volcanic domes
    Apollo 18February 1972Schroter's Valley, riverlike channel-ways
    Apollo 19July 1972Hyginus Rille region-Linear Rille, crater area
    Apollo 20December 1972Crater Copernicus, large crater impact area

1969 July 29 - . 22:57 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Pad: LA2 SL. LV Family: Skylark. Launch Vehicle: Skylark 3. LV Configuration: Skylark 3 SL730.
  • Dayglow / electrons Ionosphere mission - . Nation: UK. Agency: BAC. Apogee: 262 km (162 mi).

1970 July 29 - .
  • DOS plans laid out at Monino Space Conference. - . Nation: USSR. Spacecraft: Soyuz 7KT-OK; Salyut 1. The Fourth Military-Scientific VVS Space Conference at Monino. The VPK has finally approved completion of space stations DOS #1 and #2. They are designed to support 70 to 80 days of inhabited flight. They will be launched by a Proton UR-500K, then followed 8-10 days later by a Soyuz 7KS launched by an R-7. After thirty days aboard the station, the first crew will return. A few days later a second crew will be launched to man the station. The 7KS version of the Soyuz will have an internal hatch for transfer of the crew from the spacecraft to the station. There will be no solo Soyuz flight to test the crew's response to a 30-day mission before the first DOS flight. DOS#1 is scheduled for launch in February 1971, to coincide with the 24th Meeting of the Communist Party of the USSR. Kamanin knows it actually can't be any earlier than May 1971, but nevertheless the cosmonauts are required to train so that they will be ready by 1 February.

1971 July 29 - . 14:20 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde.
  • Starute - . Nation: USA. Agency: MRN. Apogee: 63 km (39 mi).

1972 July 29 - . 03:20 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/23. LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton-K 260-01. FAILURE: Second stage malfunction at T+ 162 sec.. Failed Stage: 2.
  • Zarya s/n 122 - . Payload: Zarya s/n 122. Mass: 18,000 kg (39,000 lb). Nation: USSR. Agency: RVSN. Program: Salyut. Class: Manned. Type: Manned space station. Spacecraft: Salyut 1. Decay Date: 1972-07-29 . COSPAR: F720729A. Summary: Second Salyut space station (DOS 2), failed to reach orbit..

1974 July 29 - . 12:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC81/24. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 287-01.
  • Molniya 1-S - . Payload: Molniya 1 s/n 38. Mass: 800 kg (1,760 lb). Nation: USSR. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1. Completed Operations Date: 1974-07-01 . USAF Sat Cat: 7392 . COSPAR: 1974-060A. Apogee: 35,848 km (22,274 mi). Perigee: 35,738 km (22,206 mi). Inclination: 14.8000 deg. Period: 1,436.40 min. Evidently a unique experimental satellite. Arrangements for experimental television broadcasts and establishment of long-range radio-communications. As of 29 August 2001 located at 104.72 deg E drifting at 0.115 deg W per day. As of 2007 Mar 10 located at 41.05E drifting at 0.029W degrees per day.

1975 July 29 - . 16:34 GMT - . Launch Site: Wallops Island. LV Family: Arcas. Launch Vehicle: Super Arcas. LV Configuration: Super Arcas NASA 15.144GM.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 81 km (50 mi).

1976 July 29 - . Launch Site: Kwajalein. LV Family: Honest John. Launch Vehicle: HJ Nike Hydac. LV Configuration: HJ Nike Hydac HAVE JEEP IV-1.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 500 km (310 mi).

1976 July 29 - . 17:07 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Delta 2310. LV Configuration: Delta 2310 605/D126.
  • NOAA 5 - . Payload: ITOS H. Mass: 340 kg (740 lb). Nation: USA. Agency: NOAA. Program: Tiros. Class: Earth. Type: Weather satellite. Spacecraft: ITOS. USAF Sat Cat: 9057 . COSPAR: 1976-077A. Apogee: 1,523 km (946 mi). Perigee: 1,507 km (936 mi). Inclination: 102.3000 deg. Period: 116.30 min. Summary: Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C)..

1976 July 29 - . 20:03 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53716-329.
  • Cosmos 846 - . Mass: 650 kg (1,430 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Tsiklon. USAF Sat Cat: 9061 . COSPAR: 1976-078A. Apogee: 1,009 km (626 mi). Perigee: 947 km (588 mi). Inclination: 82.9000 deg. Period: 104.70 min. Summary: Military navigation satellite..

1977 July 29 - . Launch Site: Kwajalein. Launch Complex: Kwajalein RN. LV Family: Honest John. Launch Vehicle: HJ Nike Hydac. LV Configuration: HJ Nike Hydac SRK-11.
  • HAVE JEEP IV Reentry test - . Nation: USA. Agency: USAF SAMSO. Apogee: 500 km (310 mi).

1977 July 29 - . 08:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 935 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 13.00 days. Decay Date: 1977-08-11 . USAF Sat Cat: 10168 . COSPAR: 1977-073A. Apogee: 251 km (155 mi). Perigee: 217 km (134 mi). Inclination: 81.3000 deg. Period: 89.20 min. Summary: Area survey photo reconnaissance satellite; returned film capsule..

1978 July 29 - . Launch Site: Baikonur. Launch Complex: Baikonur LC106. LV Family: R-36M. Launch Vehicle: R-36M.
  • DP - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 July 29 - . 04:00 GMT - .
1981 July 29 - . 11:55 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1284 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Program: Resurs. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-6U. Duration: 14.00 days. Decay Date: 1981-08-12 . USAF Sat Cat: 12614 . COSPAR: 1981-068A. Apogee: 237 km (147 mi). Perigee: 178 km (110 mi). Inclination: 82.3000 deg. Period: 88.70 min. Summary: Medium resolution photo surveillance; film capsule; also performed earth resources tasks. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation..

1982 July 29 - .
  • Burnup of Salyut 6 Space Station (USSR) - . Nation: USSR. Spacecraft: Salyut 6.

1982 July 29 - . 19:40 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC107/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53793-472.
  • Cosmos 1397 - . Mass: 550 kg (1,210 lb). Nation: USSR. Agency: MO. Class: Military. Type: Radar calibration target. Spacecraft: Taifun-2. Decay Date: 1983-05-18 . USAF Sat Cat: 13394 . COSPAR: 1982-076A. Apogee: 539 km (334 mi). Perigee: 343 km (213 mi). Inclination: 50.7000 deg. Period: 93.40 min. Summary: Released 25 Romb radar calibration subsatellites..

1983 July 29 - . 14:22 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1984 July 29 - .
1985 July 29 - . 21:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-26/51-F.
  • STS-51-F - . Call Sign: Challenger. Crew: Acton; Bartoe; Bridges; England; Fullerton; Henize; Musgrave. Payload: Challenger F08 / PDP / Spacelab 2 PLT. Mass: 15,603 kg (34,398 lb). Nation: USA. Related Persons: Acton; Bartoe; Bridges; England; Fullerton; Henize; Musgrave. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-51-F. Spacecraft: Challenger. Duration: 7.95 days. Decay Date: 1985-08-06 . USAF Sat Cat: 15925 . COSPAR: 1985-063A. Apogee: 337 km (209 mi). Perigee: 203 km (126 mi). Inclination: 49.5000 deg. Period: 89.90 min. Manned seven crew. At 5 minutes, 45 seconds into ascent the number one engine shut down prematurely due to a a sensor problem and an abort to orbit was declared. Despite the anomaly the mission continued. Launched PDP; carried Spacelab 2. Payloads: Spacelab-2 with 13 experiments, Shuttle Amateur Radio Experiment (SAREX), Protein Crystal Growth (PCG). The flight crew was divided into a red and blue team. Each team worked 12-hour shifts for 24-hour-a-day operation.
  • CRNE - . Nation: USA. Agency: NASA. Program: STS. Decay Date: 1985-08-06 . USAF Sat Cat: 15925 . COSPAR: 1985-063xx. Apogee: 328 km (203 mi). Perigee: 300 km (180 mi). Inclination: 49.5000 deg. Period: 90.80 min.
  • Spacelab 2 PLT - . Nation: USA. Agency: NASA. Program: Spacelab. Class: Manned. Type: Manned space laboratory. Spacecraft: Spacelab. Decay Date: 1985-08-06 . USAF Sat Cat: 15925 . COSPAR: 1985-063xx. Apogee: 328 km (203 mi). Perigee: 300 km (180 mi). Inclination: 49.5000 deg. Period: 90.80 min.
  • Spacelab 2 PLT - . Nation: USA. Agency: NASA. Program: Spacelab. Class: Manned. Type: Manned space laboratory. Spacecraft: Spacelab. Decay Date: 1985-08-06 . USAF Sat Cat: 15925 . COSPAR: 1985-063xx. Apogee: 328 km (203 mi). Perigee: 300 km (180 mi). Inclination: 49.5000 deg. Period: 90.80 min.
  • Spacelab 2 PLT - . Nation: USA. Agency: NASA. Program: Spacelab. Class: Manned. Type: Manned space laboratory. Spacecraft: Spacelab. Decay Date: 1985-08-06 . USAF Sat Cat: 15925 . COSPAR: 1985-063xx. Apogee: 328 km (203 mi). Perigee: 300 km (180 mi). Inclination: 49.5000 deg. Period: 90.80 min.
  • PDP - . Payload: Challenger F8 / PDP. Mass: 285 kg (628 lb). Nation: USA. Agency: NASA Huntsville. Class: Earth. Type: Magnetosphere satellite. Spacecraft: PDP. Decay Date: 1985-08-06 . USAF Sat Cat: 15929 . COSPAR: 1985-063B. Apogee: 321 km (199 mi). Perigee: 311 km (193 mi). Inclination: 49.5000 deg. Period: 90.90 min. Summary: Plasma Diagnostics Package; released by STS 51F 8/1/85, retrieved 8/2/85. .

1986 July 29 - . 11:30 GMT - . Launch Site: Thumba. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 84 km (52 mi).

1987 July 29 - . 14:07 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 77 km (47 mi).

1990 July 29 - .
  • Death of Cai Qiao - . Nation: China. Related Persons: Cai Qiao. Summary: Chinese Biologist. Cai Qiao was Vice President of the Military Medical Sciences Academy of the People's Liberation Army. In April 1966 he was one of three senior scientists that laid out the plans for China's first manned spacecraft..

1991 July 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 735. LV Family: Trident. Launch Vehicle: Trident D-5.
  • CET - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1991 July 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 735. LV Family: Trident. Launch Vehicle: Trident D-5.
  • CINC Evaluation Test launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1991 July 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 735. LV Family: Trident. Launch Vehicle: Trident D-5.
  • CET - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1991 July 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 735. LV Family: Trident. Launch Vehicle: Trident D-5.
  • CET - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1992 July 29 - . Launch Site: ETR Launch Area. Launch Platform: SSBN 738. LV Family: Trident. Launch Vehicle: Trident D-5.
  • DASO-9 demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1994 July 29 - . 09:30 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2284 - . Payload: Yantar-1KFT no. 17. Mass: 6,600 kg (14,500 lb). Nation: Russia. Agency: MOM. Class: Surveillance. Type: Cartographic satellite. Spacecraft: Yantar-1KFT. Duration: 44.00 days. Decay Date: 1994-09-11 . USAF Sat Cat: 23187 . COSPAR: 1994-044A. Apogee: 274 km (170 mi). Perigee: 211 km (131 mi). Inclination: 70.3000 deg. Period: 89.35 min. Summary: Topographic mapping for the Army General Staff. Landed September 11 1994..

1997 July 29 - . 12:59 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 99 km (61 mi).

1998 July 29 - . 02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 54 km (33 mi).

1999 July 29 - .
  • Deep Space 1, Asteroid Braille Flyby - . Nation: USA. Spacecraft: Deep Space 1.

2003 July 29 - . Launch Site: Mojave. Launch Complex: Mojave RW12/30. Launch Platform: W-Knight. Launch Vehicle: Tier One.
  • White Knight/SpaceShipOne Flight 29C / 02C - . Crew: Melvill. Nation: USA. Related Persons: Binnie; Melvill. Agency: Scaled. Program: X-Prize. Spacecraft: SpaceShipOne. Apogee: 14 km (8 mi). Objectives: First manned captive carry flight of SpaceShipOne. A man-in-loop launch rehearsal and inflight checkout of all ship systems including flight controls and propulsion sytem plumbing. Results: Complete full up rehearsal for SS1's first glide flight, including airspace, range control, Scaled mission control, data and video TM and high and low chase platforms. Additional Details: White Knight/SpaceShipOne Flight 29C / 02C.

2004 July 29 - . Launch Site: Point Mugu. LV Family: R-17. Launch Vehicle: R-17. LV Configuration: Scud FMA.
  • Arrow Target mission - . Nation: USA. Agency: MDA. Apogee: 80 km (49 mi).

2005 July 29 - .
2009 July 29 - . 18:46 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. LV Family: R-36M. Launch Vehicle: Dnepr.
  • Deimos 1 - . Mass: 90 kg (198 lb). Nation: Spain. Agency: Makeyev. Spacecraft: MicroSat-100. USAF Sat Cat: 35681 . COSPAR: 2009-041A. Apogee: 677 km (420 mi). Perigee: 635 km (394 mi). Inclination: 98.1000 deg. Period: 97.80 min. Summary: Deimos Space SL, Madrid, Spain..
  • Dubaisat 1 - . Mass: 190 kg (410 lb). Nation: UAE. Agency: Makeyev. Spacecraft: SatRec. USAF Sat Cat: 35682 . COSPAR: 2009-041B. Apogee: 682 km (423 mi). Perigee: 666 km (413 mi). Inclination: 98.1000 deg. Period: 98.20 min. Summary: Emirates Institute of Advanced Science and Technology, Dubai..
  • DMC 2 - . Mass: 95 kg (209 lb). Nation: UK. Agency: Makeyev. Spacecraft: MicroSat-100. USAF Sat Cat: 35683 . COSPAR: 2009-041C. Apogee: 677 km (420 mi). Perigee: 625 km (388 mi). Inclination: 98.1000 deg. Period: 97.80 min. Summary: DMC International Imaging, Guildford, Surrey, UK..
  • Aprizesat 4 - . Nation: Argentina. Agency: Makeyev. Program: AIS. Spacecraft: Aprizesat. USAF Sat Cat: 35684 . COSPAR: 2009-041D. Apogee: 677 km (420 mi). Perigee: 607 km (377 mi). Inclination: 98.1000 deg. Period: 97.60 min. Summary: Spacequest, Fairfax, Virginia..
  • Nanosat 1B - . Mass: 22 kg (48 lb). Nation: Spain. Agency: Makeyev. USAF Sat Cat: 35685 . COSPAR: 2009-041E. Apogee: 677 km (420 mi). Perigee: 587 km (364 mi). Inclination: 98.1000 deg. Period: 97.30 min. Summary: INTA, Spain..
  • Aprizesat 3 - . Nation: Argentina. Agency: Makeyev. Program: AIS. Spacecraft: Aprizesat. USAF Sat Cat: 35686 . COSPAR: 2009-041F. Apogee: 677 km (420 mi). Perigee: 566 km (351 mi). Inclination: 98.1000 deg. Period: 97.10 min. Summary: Spacequest, Fairfax, Virginia..

2011 July 29 - . 07:42 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2C.
  • SJ-11-02 - . Nation: China. Spacecraft: SJ-11. USAF Sat Cat: 37765 . COSPAR: 2011-039A. Apogee: 705 km (438 mi). Perigee: 688 km (427 mi). Inclination: 98.1000 deg. Period: 98.70 min. Summary: Believed to carry infrared surveillance system sensors..

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