Autonomous Aerobraking Development Software: Phase One Performance Analysis at Mars, Venus, and Titan

When entering orbit about a planet or moon with an appreciable atmosphere, instead of using only the propulsion system to insert the spacecraft into its desired orbit, aerodynamic drag can be used after the initial orbit insertion to further decelerate the spacecraft. Several past NASA missions have...

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Bibliographische Detailangaben
Hauptverfasser: Maddock, Robert W., Bowes, Angela, Powell, Richard W., Prince, Jill L. H., Cianciolo, Alicia Dwyer
Format: Tagungsbericht
Sprache:eng
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