Application of space-based interceptor propulsion technology to satellites and interplanetary vehicles

A ballistic missile defense interceptor propulsion-technology base has been accumulated which may be adapted to satellite and interplanetary mission propulsion system applications requiring substantial reductions in system weight and cost. High performance capabilities are in this way obtainable with negligible development risk. In the case of a large satellite, overall weight reduction of 5-8 percent are projected with enhanced performance, as well as lower costs due to reduced mass; in the case of a small interplanetary probe, overall weight saving is of the order of 3-6 percent.