The effect of space launch vehicle trajectory parameters on payload capability and their relation to interplanetary mission design
dc.contributor.author | Lovell, Julius Burt | en |
dc.contributor.department | Enginering Mechanics | en |
dc.date.accessioned | 2019-07-03T16:42:26Z | en |
dc.date.available | 2019-07-03T16:42:26Z | en |
dc.date.issued | 1969 | en |
dc.description.degree | M. Eng. | en |
dc.format.extent | v, 37 leaves | en |
dc.format.mimetype | application/pdf | en |
dc.identifier.uri | http://hdl.handle.net/10919/90902 | en |
dc.language.iso | en_US | en |
dc.publisher | Virginia Polytechnic Institute | en |
dc.relation.isformatof | OCLC# 2284619 | en |
dc.rights | In Copyright | en |
dc.rights.uri | http://rightsstatements.org/vocab/InC/1.0/ | en |
dc.subject.lcc | LD5655.V851 1969.L65 | en |
dc.subject.lcsh | Space trajectories | en |
dc.title | The effect of space launch vehicle trajectory parameters on payload capability and their relation to interplanetary mission design | en |
dc.type | Report | en |
dc.type.dcmitype | Text | en |
thesis.degree.discipline | Enginering Mechanics | en |
thesis.degree.grantor | Virginia Polytechnic Institute | en |
thesis.degree.level | masters | en |
thesis.degree.name | Master of Engineering | en |
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