NASA NTRS · 19760007073
STS spin-stabilized upper stage study (study 2.6). Volume 1: Executive summary
Abstract
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.
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1975-09-30. STS spin-stabilized upper stage study (study 2.6). Volume 1: Executive summary. https://ntrs.nasa.gov/citations/19760007073
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