Tests conducted at High Speed Flight Station, Edwards, Calif, to determine starting characteristics of simulated rocket engine with quantity of fuel lying dormant in main thrust chamber; results indicate that when residual fuel exists in combustion chamber at time of igniter start, it does not constitute hazard to chamber structure.
Residual fuel expulsion from simulated 50,000-pound-thrust liquid-propellant rocket engine having continuous rocket-type igniter
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 2-1-59H
1959
10 pages
Report
English
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