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Delta IV Heavy Upgrade 87 t

Launch vehicle · USA

Original archive entry. The text, images and links below are kept as they were written.

American orbital launch vehicle. Proposed upgrade to Delta IV Heavy by clustering seven common booster modules, using a new RS-800K engine in the booster stages, and an AUS-60 27 metric ton thrust LOx/LH2 upper stage. Payload fairings over 6.5 m diameter could be accommodated. Introduction would require new launch pads and booster assembly infrastructure.

LEO Payload: 79,000 kg (174,000 lb) to a 407 km orbit at 28.50 degrees. Payload: 30,000 kg (66,000 lb) to a earth escape.

Country
USA
Agency
Douglas