Aeroshell design techniques for aerocapture entry vehicles

A major goal of NASA's In-Space Propulsion Program is to shorten trip times for scientific planetary missions. To meet this challenge arrival speeds will increase, requiring significant braking for orbit insertion, and thus increased deceleration propellant mass that may exceed launch lift capa...

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Veröffentlicht in:	Acta astronautica 2007-12, Vol.61 (11), p.1029-1042
Hauptverfasser:	Dyke, R. Eric, Hrinda, Glenn A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerocapture Aeroshells Design engineering Missions NASA Planetary probes Vehicles
Online-Zugang:	Volltext
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