Highly Elliptical Rendezvous Orbits to Minimize Cryogenic Propellant Losses and Maximize Payload-Reference-Cited by-同舟云学术

Highly Elliptical Rendezvous Orbits to Minimize Cryogenic Propellant Losses and Maximize Payload

Published:2013-11 Issue:6 Volume:50 Page:1288-1292
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Langston Marcus¹,Sarigul-Klijn Nesrin¹,Sarigul-Klijn Marti M.¹

Affiliation:

1. Space Engineering Research and Graduate Program, Mechanical and Aerospace Engineering Department, University of California, Davis, Davis, California 95616-5294

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A32297

Reference3 articles.

1. In-Space Cryogenic Propellant Depot stepping stone

2. Mars Exploration Entry, Descent, and Landing Challenges

3. IsakowitzS. J.HopkinsJ. B.HopkinsJ. P., International Reference Guide to Space Launch Systems, 4th ed., AIAA, Reston, VA, 2004, pp. 59–109.

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