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
30.09.1975
Report
Keine Angabe
Englisch