NASA NTRS · 19700012887
Two-step rocket engine bipropellant valve Patent
Abstract
Solenoid two-step valve for bipropellant flow rate control to rocket engine
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Capps, J. E., Ferguson, R. E., Pohl, H. O.. 1969-01-20. Two-step rocket engine bipropellant valve Patent. https://ntrs.nasa.gov/citations/19700012887
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