NASA NTRS · 19710057228
Propulsion subsystem design for Jupiter orbiter missions
Abstract
Jupiter orbiter spacecraft propulsion system design, noting advantages of fluorine/hydrazine propellant combination
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Don, J. P., Phen, R. L.. 1971-06-01. Propulsion subsystem design for Jupiter orbiter missions. https://ntrs.nasa.gov/citations/19710057228
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