Study to Determine the Effects on the Scout Vehicle Structure Due to Unconventional Vehicle-Spacecraft Configurations
1965
306 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Scout launch vehicle , Spacecraft configuration , Center , Configuration , Control , Effect , Gravity , Hardware , Launch , Payload , Reentry , Spacecraft , Stability , Structure , Unconventional , Vehicle , Weight
NTRS | 1961
NTIS | 1965
|NTRS | 1965
|AIAA | 1965
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