by
Aiaa Space Conference
,
J. Bradford
,
J. Olds
,
R. Bechtel
,
T. Cormier
,
D. Messitt
,
John Bradford
,
John R. Olds
,
Ryan Bechtel
,
Tim Cormier
,
Donald G. Messitt
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Abstract:
The ABLV-GT is a conceptual design for an advanced reusable launch vehicle based on the current NASA Langley ABLV concept. It is a Vision Vehicle class, horizontal takeoff, horizontal landing singlestage -to-orbit vehicle. Main propulsion is provided by Aerojet's `Strutjet' LOX/LH2 rocket-based combined cycle engine design. The ABLV-GT is designed to deliver 25,000 lbs. to the orbit of the International Space Station from Kennedy Space Center. This paper will report the findings of a conceptual design study on the ABLV-GT performed over the last year by members of the Space Systems Design Lab at Georgia Tech. This work has been sponsored by the Advanced Reusable Transportation Technologies program office at NASA Marshall Space Flight Center. Details of the concept design including external and internal configuration, mass properties, trajectory analysis, aerodynamics, and aeroheating are given. This vehicle study resulted in the closure of 18 different vehicle designs. The trade vari...
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