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Altitude Starting Tests of a Small Solid Propellant Rocket
From Summary: "Four solid-propellant rocket engines of nominal 500-pound thrust were tested for starting characteristics at pressure altitudes ranging from 89,000 to 111,000 feet and at a temperature of -75^o F. Chamber pressures were measured on two of the runs. Average chamber pressures in these two runs were lower than expected, although action times agreed with the expected values."
Date:
June 21, 1957
Creator:
Sloop, John L. & Krawczonek, Eugene M.
System:
The UNT Digital Library