Fully-propulsive Mars atmospheric transit strategies for high-mass payload missions

A systems analysis focused on the use of propulsion during entry, descent, and landing at Mars is presented. The propellant mass fractions of various fully-propulsive EDL strategies are presented. A key aspect of the study is the propellant costs of meeting specified heat rate constraints and the tr...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Marsh, C.L., Braun, R.D.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Aerodynamics Gravity Humans Mars Moon Payloads Propellants Propulsion Space technology Space vehicles
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