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Delta 3920-8
Part of Thor Family
American orbital launch vehicle. Three stage vehicle consisting of 9 x Castor 4A + 1 x ELT Thor/RS-27 + 1 x Delta K

Status: Retired 1989. First Launch: 1989-03-24. Last Launch: 1989-03-24. Number: 1 . Thrust: 3,188.00 kN (716,690 lbf). Gross mass: 190,000 kg (410,000 lb). Height: 36.00 m (118.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 500 km (310 mi).



Family: orbital launch vehicle. Country: USA. Spacecraft: SDI. Launch Sites: Cape Canaveral, Cape Canaveral LC17B. Stages: Delta Thor RS27, Castor 4, Delta K. Agency: Douglas.

1989 March 24 - . 21:50 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 3920-8.
  • USA 36 - . Payload: Delta Star. Mass: 6,000 kg (13,200 lb). Nation: USA. Agency: SDIO. Class: Military. Type: Strategic defense satellite. Spacecraft: SDI. Decay Date: 1992-06-23 . USAF Sat Cat: 19911 . COSPAR: 1989-026A. Apogee: 312 km (193 mi). Perigee: 307 km (190 mi). Inclination: 47.7000 deg. Period: 90.70 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). .


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