Mars ascent propulsion options for small sample return vehicles-Reference-Cited by-同舟云学术

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Mars ascent propulsion options for small sample return vehicles

Published:1997-07-06 Issue: Volume: Page:
ISSN:
Container-title:33rd Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Whitehead John¹,Whitehead John¹

Affiliation:

1. Lawrence Livermore National Lab., Livermore, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2950

Reference34 articles.

1. Wallace, R.A., R.T. Camber, et al, Low Cost Mars SampleReturnMissionOptions.AIAA96-0336,1996.

2. Guernsey, C.S.,Mars Ascent Vehicle (MAVI Fact Sheet.JPLMemorandum,Spring 1996.

3. Whitehead, J.C., Single Stage to Orbit Mass Budgets Derived from Propellant Density and Specific Impulse. AJAA96-3108,1996.

4. Whitehead,J.C., L.C. Pittenger,NJ.Colella,Designand FlightTestingofaReciprocatingPumpFedRocket.AIAA 94-3031,1994.

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Development of a reciprocating pump for space propulsion system;Aeronautics and Aerospace Open Access Journal;2020-08-14

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

5. Mars ascent propulsion on a minimum scale;Acta Astronautica;1999-08

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