The paper examines the utilization of aerodynamic forces to capture a vehicle into a closed orbit and/or to modify an orbit. Attention is given to two techniques: aerobraking which uses drag during successive passes through the upper atmosphere to circularize a highly elliptical orbit, and aerocapture which transfers a vehicle into a closed stable orbit from a hyperbolic flyby trajectory. Sample missions employing both techniques are discussed.
Aerobraking and aerocapture for planetary missions
01.02.1980
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Keine Angabe
Englisch
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