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A combined design and trajectory optimisation algorithm for an orbiter vehicle

By A McGregor

Abstract

SIGLEAvailable from British Library Document Supply Centre-DSC:DXN006935 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Topics: 22C - Spacecraft trajectories, spacecraft re-entry, 22D - Spacecraft launching, ground support, 22A - Astronautics, A combined design and trajectory optimisation algorithm for an orbiter vehicle [ Spaceplanes]
Year: 1995
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Provided by: OpenGrey Repository
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