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Aerodynamics / Spacecraft propulsion / Fluid dynamics / Manned spacecraft / Ballute / Atmospheric entry / Inflatable / Drag / Ballistic coefficient / Aerospace engineering / Space technology / Spaceflight


An Evaluation of Ballute Entry Systems for Lunar Return Missions AE8900 MS Special Problems Report Space Systems Design Lab (SSDL) Guggenheim School of Aerospace Engineering
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Document Date: 2011-06-01 10:53:05


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File Size: 466,05 KB

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Company

Knudsen / /

Facility

Aerospace Engineering Georgia Institute of Technology Atlanta / /

IndustryTerm

ballute using nitrogen gas / gas constant nose radius / aerocapture technology portion / kinetic energy / ablative systems / ballute technology / technology path consisting / thermal protection systems / inflatable drag devices / energy / /

Organization

Guggenheim School / National Aeronautics and Space Administration / Lunar Return Missions AE8900 MS Special Problems Report Space Systems Design Lab / Aerospace Engineering Georgia Institute of Technology Atlanta / /

Position

Rt Rt / Rt / GA Author / Ian G. Clark Advisor / Rn Rt / Rt´/Rt / /

Product

Apollo capsule / /

Technology

ballute technology / /

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