NASA NTRS · 19710010425
High specific impulse gas-core reactors
Abstract
Calculated estimates of gas core nuclear rocket engine weights for specific impulses ranging from 3000 to 7000 seconds and for engine thrusts ranging from 4400 to 440,000 newtons
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Ragsdale, R. G.. 1971-03-01. High specific impulse gas-core reactors. https://ntrs.nasa.gov/citations/19710010425
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