NASA NTRS · 19710061319
Solid-propellant motors for high-incremental velocity low-acceleration maneuvers in space
Abstract
Low thrust long burning solid rocket propellant motor for orbit insertion maneuvers, discussing design, static tests, nozzle composition, igniter and performance
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Shafer, J. I.. 1971-09-01. Solid-propellant motors for high-incremental velocity low-acceleration maneuvers in space. https://ntrs.nasa.gov/citations/19710061319
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