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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.

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/27896
Date January 1977
CreatorsGreen, Andrew Joseph
ContributorsLouis A. D'Amario and Donald C. Fraser., Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
Languageen_US
Detected LanguageEnglish
TypeThesis
Formatv, 97 leaves, 4288548 bytes, 4300696 bytes, application/pdf, application/pdf, application/pdf
RightsM.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission., http://dspace.mit.edu/handle/1721.1/7582

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