Space system consists of boosters, transfer stage, and spacecraft vehicle required to perform mission after injection into desired trajectory; procedure required in sizing and configuration study of space vehicle is described and factors which must be considered such as aerodynamic, power plant, and other loads; material selection, design of space cabins, propellant tank design and common bulkhead or dome between two vessels are also considered.
Space technology -- Spacecraft systems
NASA SP
1965
85 pages
Report
Englisch
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Space Technology. Volume 1: Spacecraft Systems
NTIS | 1965
|Space : spacecraft, missions, technology
TIBKAT | 1.1985 - 12.1996,4
Space technology -- Spacecraft mechanical engineering
Engineering Index Backfile | 1965
|