Chemical Propulsion Systems for Low Cost Mars Sample Return-Reference-Cited by-同舟云学术

Chemical Propulsion Systems for Low Cost Mars Sample Return

Published:2004-06-26 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Baker Adam¹,Coxhill Ian¹,Henshall Paul²

Affiliation:

1. Surrey Satellite Technology Ltd.

2. Surrey Space Centre

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3492

Reference7 articles.

1. SSTL pre-Phase A study, Aurora Earth Re-Entry Vehicle Demonstrator, EVD. Engineering data package ENG_01. ESAStatement ofWorkAO/1-4398/03/NL/AG. March31st,2004.

2. Schmidt E W, Bewster G T, Cain G A; Mars Lander Retro Propulsion; paper IAF-99-S.2.02; presented at the 50thI.A.F.Congress,Amsterdam,theNetherlands,October1999;pp.15.

3. Morrisey D C; Historical perspective: Viking Mars lander propulsion; AIAApaper 89-2391; presented at the 25thAIAAJointPropulsionConference;Monterey,USA;July1989;pp.19.

4. Stephenson D; Mars ascent vehicle - Concept development; AIAA 2002-4318; presented at the 38thAIAA Joint PropulsionConference; Indianapolis, USA; July2002; pp. 9.

5. Whitehead J C; Hydrogen peroxide gas generator with a reciprocating pump; AIAA 2002-3702; presented at the 38thAIAAJointPropulsionConference&Exhibit;July2002,Indianapolis,USA;pp.9.

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

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