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Delta 6920-8
Part of Thor
American orbital launch vehicle. Three stage vehicle consisting of 9 x Castor 4A + 1 x EELT Thor/RS-27+ 1 x Delta K with 2.4 m (8 foot) diameter fairing)

Status: Retired 1990. First Launch: 1990-02-14. Last Launch: 1990-02-14. Number: 1 . Thrust: 3,790.00 kN (852,020 lbf). Gross mass: 219,000 kg (482,000 lb). Height: 39.00 m (127.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 1,000 km (600 mi).


More at: Delta 6920-8.

Family: orbital launch vehicle. Country: USA. Engines: RS-27A. Spacecraft: LACE, RME. Launch Sites: Cape Canaveral, Cape Canaveral LC17B. Stages: Delta Thor XLT-C, Castor 4A engine, Delta K. Agency: Douglas.

1990 February 14 - . 16:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Thor. Launch Vehicle: Delta 6920-8.

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