Spinning solid propellant upper stage rocket engines designed for geosynchronous satellite payloads are investigated. Factors considered include: impact of the spinning stages on the payloads; applicability to 1981-1991 NASA mission model; and cost effectiveness.
Sts Spin-Stabilized Upper Stage Study (Study 2.6). Volume 1: Executive Summary
1975
46 pages
Report
Keine Angabe
Englisch