Spacecraft Propulsive Device Using Ambient Upper Atmospheric Constituents for Reaction Mass-Reference-Cited by-同舟云学术

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Spacecraft Propulsive Device Using Ambient Upper Atmospheric Constituents for Reaction Mass

Published:2006-07-09 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Dressler Gordon

Publisher

American Institute of Aeronautics and Astronautics

Reference13 articles.

1. 5Sojka, J.J. "Refuelable Atmospheric Dipper and Planetary Landing Concept,"AIAA-2001-3734, AIAA, Washington, DC, July 2001.

2. Propulsion Requirements for Drag-Free Operation of Spacecraft in Low Earth Orbit

3. Orbit Optimization for the Geospace Electrodynamic Connections (GEC) Mission

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