Experimental and theoretical analysis of ablative material response in a liquid- propellant rocket engine Final report
Ablative material degradation in liquid propellant rocket engine environment of nitrogen tetroxide-aerozine
Clark, K. J.↗
Engineering topics
Publications and source records attributed to Flood, D. T..
Ablative material degradation in liquid propellant rocket engine environment of nitrogen tetroxide-aerozine
Techniques for rating performance of ablative materials in liquid-propellant rocket engines
Rocket-nozzle environment simulation with DC arc- plasma generator noting graphite and phenolic material test results