An analysis of 26 different Spacelab experiment propulsion platform configurations is presented covering the determination of costs, mass, and the required volume in the shuttle payload bay. As a result of this analysis, three preferred configurations were selected: (1) hydrazine, super blowdown, isotensoid tank; (2) hydrazine, blowdown, inert gas attitude control, spherical tank; and (3) hydrazine, regulated pressurized gas system, inert gas attitude control, spherical tank.
SEAP - Configuration and Cost Analysis SEAP - Konfigurations- und Kostenanalyse
1977
65 pages
Report
Keine Angabe
Englisch
SEAP - Konfigurations- und Kostenanalyse
TIBKAT | 1977
|Seap - Configurations and Cost Analysis
NTIS | 1978
|