Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
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Publication Search Results
Ultra Lightweight Ballutes for Return to Earth from the Moon
Tempest: Crew Exploration Vehicle Concept
Modeling Approach for Analysis and Optimization of a Long-Duration Mars Airplane
A Comparison of Modern and Historic Mass Estimating Relationships on a Two-Stage to Orbit Launch Vehicle
Static Aeroelastic Analysis of a Thin-Film Clamped Ballute for Titan Aerocapture
A Survey of Ballute Technology for Aerocapture
Tanker Argus: Re-supply for a LEO Cryogenic Propellant Depot
Entry System Options for Human Return from the Moon and Mars
Flight System Options for a Long Duration Mars Airplane
Solar Electric Propulsion Module Concept for the BiFrost Architecture