Teleoperator Maneuvering System (TMS) versus integral spacecraft propulsion, spacecraft maintenance, cost benefits, launch prices, integral propulsion length penalties, remote maintenance versus EVA, potential weight reduction benefits, basing mode, mission models and payload requirements, and program profitability are discussed.
Teleoperator Maneuvering System (TMS) benefits assessment study. Volume 1: Executive summary
01.04.1983
Report
Keine Angabe
Englisch
Teleoperator maneuvering system
NTRS | 1982
|Teleoperator maneuvering system
AIAA | 1982
|