NASA NTRS · 19630011163
THRUST CHAMBER COOLING TECHNIQUES FOR SPACECRAFT ENGINES. VOLUME I- EVALUATION PROCEDURE AND ANALYSES
Abstract
Liquid propellant rocket engine - cooling system, ablation, and heat sink
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Batha, D. R., Campbell, J. G., Carey, M. D., Coulbert, C. D.. 1963-07-15. THRUST CHAMBER COOLING TECHNIQUES FOR SPACECRAFT ENGINES. VOLUME I- EVALUATION PROCEDURE AND ANALYSES. https://ntrs.nasa.gov/citations/19630011163
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