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Thor Delta A
Part of Thor
Delta A no. 13
Delta A no. 13
Delta A no. 13 - COSPAR 1962 Beta Gamma
American orbital launch vehicle. Three stage vehicle consisting of 1 x Thor DM-21 + 1 x AJ10-118 + 1 x Altair

AKA: Delta A. Status: Retired 1962. First Launch: 1962-10-02. Last Launch: 1962-10-27. Number: 2 . Payload: 250 kg (550 lb). Thrust: 667.20 kN (149,993 lbf). Gross mass: 50,756 kg (111,897 lb). Height: 31.00 m (101.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 100,000 km (60,000 mi).

LEO Payload: 250 kg (550 lb). Payload: 68 kg (149 lb) to a GTO. Flyaway Unit Cost 1985$: 9.590 million.

Stage Data - Delta A



Family: orbital launch vehicle. Country: USA. Engines: MB-3-1, AJ10-118. Spacecraft: EPE. Projects: Explorer. Launch Sites: Cape Canaveral, Cape Canaveral LC17B. Stages: Altair 1, Delta A, Thor DM-21. Agency: Douglas.

1959 April 28 - . LV Family: Thor. Launch Vehicle: Thor Delta A.
1962 October 2 - . 22:11 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Delta A.
1962 October 27 - . 23:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Thor Delta A.

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