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Thor Delta C1
Part of Thor Family
American orbital launch vehicle. Three stage vehicle consisting of 1 x Thor DSV-2A + 1 x Delta D + 1 x FW4D

Status: Retired 1969. First Launch: 1966-05-25. Last Launch: 1969-01-22. Number: 3 . Payload: 81 kg (178 lb). Thrust: 756.00 kN (169,955 lbf). Gross mass: 52,000 kg (114,000 lb). Height: 27.50 m (90.20 ft). Diameter: 2.44 m (8.00 ft). Apogee: 1,000 km (600 mi).

LEO Payload: 81 kg (178 lb).


More at: Thor Delta C1.

Family: orbital launch vehicle. Country: USA. Spacecraft: OSO, AE. Projects: Explorer. Launch Sites: Cape Canaveral, Cape Canaveral LC17B. Stages: Altair 1, Delta D, Thor DM-21. Agency: Douglas.

1966 May 25 - . 14:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Delta C1.
  • Explorer 32 - . Payload: AE B. Mass: 225 kg (496 lb). Nation: USA. Agency: NASA Greenbelt. Program: Explorer. Class: Earth. Type: Atmosphere satellite. Spacecraft: AE. Decay Date: 1985-02-22 . USAF Sat Cat: 2183 . COSPAR: 1966-044A. Apogee: 2,723 km (1,691 mi). Perigee: 282 km (175 mi). Inclination: 64.6000 deg. Period: 116.00 min. Atmospheric Explorer; aeronomy experiments. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

1967 October 18 - . 15:58 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Delta C1.
  • OSO 4 - . Payload: OSO D. Mass: 272 kg (599 lb). Nation: USA. Agency: NASA Greenbelt. Class: Astronomy. Type: Solar satellite. Spacecraft: OSO. Decay Date: 1982-06-15 . USAF Sat Cat: 3000 . COSPAR: 1967-100A. Apogee: 555 km (344 mi). Perigee: 552 km (342 mi). Inclination: 32.9000 deg. Period: 95.70 min. Extreme UV solar observations. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .

1969 January 22 - . 16:48 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Delta C1.
  • OSO 5 - . Payload: OSO F. Mass: 291 kg (641 lb). Nation: USA. Agency: NASA Greenbelt. Class: Astronomy. Type: Solar satellite. Spacecraft: OSO. Decay Date: 1984-04-02 . USAF Sat Cat: 3663 . COSPAR: 1969-006A. Apogee: 559 km (347 mi). Perigee: 538 km (334 mi). Inclination: 33.0000 deg. Period: 95.60 min. Orbiting Solar Observatory; solar radiation data. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). .


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