Optimal escape trajectory from a high earth orbit by use of solar radiation pressure.
Thesis. 1977. M.S.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. === MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO. === Bibliography : leaves 51-53. === M.S.
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| Format: | Others |
| Language: | en_US |
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Massachusetts Institute of Technology
2005
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| Online Access: | http://hdl.handle.net/1721.1/27896 |