A Simplified Model for the Evaluation of the DeltaV of Ascent Trajectories
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American Institute of Aeronautics and Astronautics
Reference9 articles.
1. 2Whitehead J.C. "Mars Ascent Propulsion Trades with Trajectory Analysis", 40thAIAA/ASME/SAE/ASEE Joint Propulsion Conference, Fort Lauderdale, USA, 2004.
2. 3Whitehead J.C. "Mars Ascent Propulsion Options for Small Sample Return Vehicles", 33rdAIAA/ASME/SAE/ASEE Joint Propulsion Conference, Seattle,USA, 1997.
3. Mars ascent propulsion on a minimum scale
4. 5Whitehead J.C., Brewster G.T. "Mars to Orbit with Pumped Hydrazine", 35thAIAA/ASME/SAE/ASEE Joint Propulsion Conference, Los Angeles, USA, 1999.
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1. A Simple Analytic Model for Estimating Mars Ascent Vehicle Mass and Performance;AIAA/AAS Astrodynamics Specialist Conference;2014-08-01
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