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The effect of space launch vehicle trajectory parameters on payload capability and their relation to interplanetary mission design

no abstract provided by author / M. Eng.

Identiferoai:union.ndltd.org:VTETD/oai:vtechworks.lib.vt.edu:10919/90902
Date January 1969
CreatorsLovell, Julius Burt.
ContributorsEnginering Mechanics
PublisherVirginia Polytechnic Institute
Source SetsVirginia Tech Theses and Dissertation
Languageen_US
Detected LanguageEnglish
TypeReport, Text
Formatv, 37 leaves, application/pdf, application/pdf
RightsThe authors of the theses and dissertations are the copyright owners. Virginia Techs Digital Library and Archives has their permission to store and provide access to these works.
RelationOCLC# 2284619

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