NASA NTRS · 19630023320
SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES
Abstract
Regenerative and radiation cooling, transpiration or film cooling, ablation and inert or endothermic heat sink, used in selecting optimum spacecraft engine thrust chamber cooling techniques
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Coulbert, C. D.. 1963-06-20. SELECTING A THRUST CHAMBER COOLING TECHNIQUE FOR SPACECRAFT ROCKET ENGINES. https://ntrs.nasa.gov/citations/19630023320
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