PERFORMANCE OF SOLID STATE EMULSIONS OF ISOAMYL ALCOHOL IN EVA-STABILIZED LOW-MW POLYETHYLENE, STRUCTURED BY LASER-SINTERED NYLON SCAFFOLDS AS FUELS IN N2O HYBRID ROCKET ENGINE

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Veröffentlicht in:	AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Hybrid rockets
1. Verfasser:	Zdybal, D. (VerfasserIn)
Weitere Verfasser:	Klos, W. (VerfasserIn), Drozdz, P. (VerfasserIn), Rydz, Z. (VerfasserIn), Kobus, K. (VerfasserIn), Wyciszkiewicz, B. (VerfasserIn), Zwolak, A. (VerfasserIn), Wyzlinski, M. (VerfasserIn), Tatara, T. (VerfasserIn), Guzik, A. (VerfasserIn)
Format:	UnknownFormat
Sprache:	eng
Veröffentlicht:	2019
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FUEL REGRESSION CHARACTERISTICS IN HYBRID ROCKETS USING N2O/HDPE	2019	Ito, S.
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DIODE LASER IGNITION MECHANISM FOR HYBRID PROPULSION SYSTEMS	2019	Dyrda, D. M.
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