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Delta 4000


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Delta 4925
Delta 4925-8 no. 196 - COSPAR 1990-051
American orbital launch vehicle. The Delta 4000 series used more powerful Castor 4A strap-ons, but the old Extended Long Tank core with MB-3 engine. Only two of these were launched.

Status: Out of production. Payload: 3,400 kg (7,400 lb). Thrust: 3,468.80 kN (779,817 lbf). Gross mass: 200,740 kg (442,550 lb). Height: 34.00 m (111.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 185 km (114 mi).

LEO Payload: 3,400 kg (7,400 lb) to a 185 km orbit. Payload: 1,200 kg (2,600 lb) to a GTO. Flyaway Unit Cost 1985$: 34.220 million.

Stage Data - Delta 4000

Family: orbital launch vehicle. Country: USA. Engines: RS-27, AJ10-118K. Spacecraft: HS 376, Insat 1. Stages: Delta Thor ELT, Castor 4A engine, Delta K. Agency: Douglas. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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