A conceptual design is presented for a carrier vehicle for an air launched space booster. This airplane is capable of carrying a 500,000 pound satellite launch system to an altitude over 40,000 feet for launch. The airplane features a twin fuselage configuration for improved payload and landing gear integration, a high aspect ratio wing for maneuverability at altitude, and is powered by six General Electric GE-90 engines. The analysis methods used and the systems employed in the airplane are discussed. Launch costs are expected to be competitive with existing launch systems.
Design of an airborne launch vehicle for an air launched space booster
01.01.1993
Report
Keine Angabe
Englisch
Design of an Airborne Launch Vehicle and an Air Launched Space Booster
British Library Conference Proceedings | 1993
|Gryphon: Air Launched Space Booster
NTIS | 1993