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Thor Delta C1
Part of Thor
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.
1967 October 18 - . 15:58 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Delta C1.
1969 January 22 - . 16:48 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Delta C1.

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