Mars ascent propulsion on a minimum scale

Author:

Whitehead John C.,Guernsey Carl S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference3 articles.

1. Mars Ascent Propulsion Options for Small Sample Return Vehicles;Whitehead,1997

2. Evaluation of Some Candidate Propulsion Technologies for Mars Ascent;Guernsey;AIAA 98-0651,1998

3. Whitehead, J., L. Pittenger, N. Colella, Design and Flight Testing of a Reciprocating Pump Fed Rocket. AIAA 94-3031.

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1. Rotational moulding of PEEK polymer liners with carbon fibre/PEEK over tape-placement for space cryogenic fuel tanks;Materials & Design;2017-10

2. Trajectory Analysis and Staging Trades for Smaller Mars Ascent Vehicles;Journal of Spacecraft and Rockets;2005-11

3. A Simplified Model for the Evaluation of the DeltaV of Ascent Trajectories;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

4. Mars Ascent Propulsion Trades with Trajectory Analysis;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

5. High-Pressure-Pumped Hydrazine for Mars Sample Return;Journal of Spacecraft and Rockets;2000-07

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