EFFECT OF AFT CHAMBER VOLUME ON HYBRID ROCKET COMBUSTION EFFICIENCY

EFFECT OF AFT CHAMBER VOLUME ON HYBRID ROCKET COMBUSTION EFFICIENCY

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Bibliographische Detailangaben
Veröffentlicht in:AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Hybrid rockets
1. Verfasser: Kageyama, L. (VerfasserIn)
Weitere Verfasser: Kamps, L. (VerfasserIn), Nagata, H. (VerfasserIn)
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Sprache:eng
Veröffentlicht: 2019
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