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Thor DSV-2D
Status: Retired 1962. First Launch: 1962-01-15. Last Launch: 1962-07-18. Number: 2 . Thrust: 743.00 kN (167,033 lbf). Gross mass: 50,000 kg (110,000 lb). Height: 21.70 m (71.10 ft). Diameter: 2.44 m (8.00 ft). Apogee: 1,500 km (900 mi).
More at: Thor DSV-2D.
Family: orbital launch vehicle. Country: USA. Spacecraft: Program 437, Program 922. Launch Sites: Cape Canaveral, Cape Canaveral LC17A. Stages: Thor DM-21. Agency: Douglas.
1962 January 15 - . 11:07 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Thor DSV-2D.
1962 Feb - . LV Family: Thor. Launch Vehicle: Thor DSV-2D.
- Standard Thor to use three strap-on, solid-propellant motors. - . Space Systems Division asked the Douglas Aircraft Company to define the performance and design of a Standard Thor (DSV-2C) using three strap-on, solid-propellant motors..
1962 July 18 - . 09:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Thor DSV-2D.
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