Site accessibility and characteristic velocity requirements for direct-descent lunar landings
A direct descent is one in which the main descent propulsion system burns continuously from lunar approach to touchdown. The characteristic velocity requirement for direct lunar descents is presented as a function of the landing site location relative to the normal impact point. Results are included...
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce],
[1970]
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| Series: | NASA technical note ;
D-5923 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NASA TN D-5923 |
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