NASA NTRS · 19680036544
Hypergolic control fluid effects on the combustion of solid propellants.
Abstract
Solid propellants combustion characteristics under hypergolic fluid injection control conditions including burning rate, vacuum ignition, low pressure stability, etc
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Coates, R. L., Cohen, N. S., Roberts, R. W.. 1968-01-01. Hypergolic control fluid effects on the combustion of solid propellants.. https://ntrs.nasa.gov/citations/19680036544
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