Organizational Unit:
Space Systems Design Laboratory (SSDL)
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Publication Search Results
Aeroelastic Design Considerations of a Clamped Ballute for Titan Aerocapture
Ultra Lightweight Ballutes for Return to Earth from the Moon
A Survey of Ballute Technology for Aerocapture
Tanker Argus: Re-supply for a LEO Cryogenic Propellant Depot
Ultra Lightweight Ballutes for Return to Earth from the Moon
Entry System Options for Human Return from the Moon and Mars
Flight System Options for a Long Duration Mars Airplane
Static Aeroelastic Analysis of a Thin-Film Clamped Ballute for Titan Aerocapture
Tempest: Crew Exploration Vehicle Concept
Modeling Approach for Analysis and Optimization of a Long-Duration Mars Airplane