HIGH OPERATIONS TEMPO ENERGETIC ACCESS TO GLOBE AND LAUNCH EXPERIMENT (HOT EAGLE). Phase 1
Technical Report,01 Oct 2002,31 May 2005
Conceptual Research Corporation Playa del Rey United States
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In this report, the researchers defined and assessed a reusable launch vehicle upper stage that is suitable for use with areusable first stage. A subscale demonstrator that is intended for the flight test validation of key HOT EAGLEtechnologies and system concepts has been defined and sized to allow flight on an existing first-stage booster. This reportalso includes studies on propulsion, structure, and systems and avionics.