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Delta IV Small
Part of Delta IV
American orbital launch vehicle. Light launch vehicle using the Delta-4 core with the traditional Delta K and PAM-D upper stages. 2 m diameter payload fairing. Not flown as of 2008 but cancellation of the Delta II could lead to its eventual use.

Status: In production. Payload: 2,200 kg (4,800 lb). Thrust: 2,949.00 kN (662,961 lbf). Gross mass: 244,046 kg (538,029 lb). Height: 59.00 m (193.00 ft). Diameter: 5.00 m (16.40 ft).

Payload: 2,200 kg (4,800 lb) to a GTO.

Stage Data - Delta IV Small



Family: orbital launch vehicle. Country: USA. Engines: AJ10-118K, RS-68. Stages: Delta RS-68, Delta K, Star 48. Agency: Douglas.

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