A Novel Aerobrake Design for a Mars Landerby John E. Crawford, TRW, Redondo Beach, United States,
Ralph G. Colbert, TRW, Redondo Beach, United States,
Manual I. Cruz, TRW, Redondo Beach, United States,
Abstract: A flexible/inflatable aerobrake is proposed for delivering small payloads to Mars as an alternative to propulsion landing. Some results that demonstrate feasibility are presented.
Subject Headings: Mars | Structural design | Payloads | Space structures | Feasibility studies | Space exploration | Mathematics | Mathematical models
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