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Winged orbital launch vehicle. Family:
Winged. Country: USA. Status: Study 1963.

Douglas design of the early 1960's for a two-stage-to-orbit, winged, recoverable vehicle. Two versions were envisioned - a preliminary one the size of a DC-8 and a monster vehicle capable of delivering one million pounds payload to orbit. It was assumed at this scale that Lox/LH2 vehicles could achieve stage propellant mass fractions of 88% to 86%.

Manufacturer: Douglas. LEO Payload: 454,500 kg (1,002,000 lb). to: 325 km Orbit. at: 28.00 degrees. Total Length: 270.00 m (880.00 ft). Span: 125.00 m (410.00 ft).


Bibliography:

  • Bono, Philip, Advanced in the Astronautical Sciences, "Design Objectives for Tomorow's Big Boosters", 1963.


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