Cost effective approaches for placing automated payloads into circular and elliptical orbits using energy requirements significantly lower than that provided by the smallest, currently planned shuttle upper stage, SSUS-D, were investigated. Launch costs were derived using both NASA existing/planned launch approaches as well as new propulsion concepts meeting low-energy regime requirements. Candidate new propulsion approaches considered were solid (tandem, cluster, and controlled), solid/liquid combinations and all-liquid stages. Results show that the most economical way to deliver the 129 low energy payloads is basically with a new modular, short liquid bipropellant stage system for the large majority of the payloads. For the remainder of the payloads, use the shuttle with integral OMS and the Scout form for a few specialized payloads until the Shuttle becomes operational.
Low Energy Stage Study. Volume 1: Executive Summary
1978
42 pages
Report
No indication
English
Manned Spacecraft , Spacecraft Trajectories & Flight Mechanics , Low thrust propulsion , Mission planning , Orbital launching , Propulsion system configurations , Space shuttle payloads , Spacecraft propulsion , Liquid rocket propellants , Orbit maneuvering engine (Space shuttle) , Scout launch vehicle , Solid rocket propellants , Space transportation system , Space tugs