The benefits of the utilization of effluents of the Space Station Environmental Control and Life Support (ECLS) system are examined. Various ECLSS-propulsion system interaction options are evaluated and compared on the basis of weight, volume, and power requirements. Annual propulsive impulse to maintain station altitude during a complete solar cycle of eleven years and the effect on station resupply are considered.
Space Station Propulsion-Eclss Interaction Study
1986
92 pages
Report
Keine Angabe
Englisch
Space station propulsion-ECLSS interaction study
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