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Thor Delta D
Part of Thor
Delta D no. 30
Delta D no. 30
Delta D no. 30 - COSPAR 1965-028
American orbital launch vehicle. Four stage vehicle consisting of 3 x Castor + 1 x Thor DSV-2C + 1 x Delta D + 1 x Altair 2

AKA: Delta D;Thrust Augmented Thor. Status: Retired 1965. First Launch: 1964-08-19. Last Launch: 1965-04-06. Number: 2 . Payload: 450 kg (990 lb). Thrust: 1,571.00 kN (353,174 lbf). Gross mass: 63,966 kg (141,020 lb). Height: 32.00 m (104.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 40,000 km (24,000 mi).

LEO Payload: 450 kg (990 lb). Payload: 104 kg (229 lb) to a GTO. Flyaway Unit Cost 1985$: 12.720 million.

Stage Data - Delta D



Family: orbital launch vehicle. Country: USA. Engines: AJ10-118D, MB-3-3. Spacecraft: Syncom, Intelsat 1. Projects: Intelsat. Launch Sites: Cape Canaveral, Cape Canaveral LC17A. Stages: Delta Thor TA, Delta D, Altair 2, Castor 1. Agency: Douglas.
Photo Gallery

Delta DDelta D
Credit: © Mark Wade



1964 August 19 - . 12:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Thor Delta D.
1965 April 6 - . 23:47 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Thor. Launch Vehicle: Thor Delta D.

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