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Delta 5000
Part of Thor
Delta 5920
Delta 5920
Delta 5920-8 no. 189 - COSPAR 1989-089
American orbital launch vehicle. The Delta 5000 series used the more powerful Castor 4A strap-ons but with the Extended Long Tank core with RS-27 engine. Only one was launched.

Status: Out of production. Payload: 3,848 kg (8,483 lb). Thrust: 3,468.90 kN (779,840 lbf). Gross mass: 201,580 kg (444,400 lb). Height: 34.00 m (111.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 3,848 kg (8,483 lb) to a 185 km orbit. Payload: 1,405 kg (3,097 lb) to a GTO. Flyaway Unit Cost 1985$: 34.220 million.

Stage Data - Delta 5000



Family: orbital launch vehicle. Country: USA. Engines: RS-27, AJ10-118K. Spacecraft: COBE. Stages: Delta Thor RS27, Castor 4A engine, Delta K. Agency: Douglas.

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