EXPLORATORY PROPELLANT RESEARCH

This report summarizes the efforts on continued stability testing of aluminum-hydrazine-carbopol combinations and preparation for formulation and characterization of liquid metalized propellants containing LM-2 and LMH-2. It also summarizes the analytical and experimental investigation of the N2H4/N...

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Bibliographische Detailangaben
Hauptverfasser:	Christensen, Robert C, Summers, W H, McMullen, E T, Selph, C C
Format:	Report
Sprache:	eng
Schlagworte:	ALUMINUM CARBOPOL COLLOIDS FLAMES FLUORIDES HEAT OF FORMATION HIGH PRESSURE HIGH TEMPERATURE HYDRAZINES HYDROGEN COMPOUNDS LIQUID METALS Liquid Rocket Propellants LMH-2 PROPELLANT NITROGEN COMPOUNDS REACTION KINETICS ROCKET ENGINES SCIENTIFIC RESEARCH STABILITY TOXICITY VELOCITY XENON HEXAFLUORIDE XENON LAMPS
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Beschreibung
Zusammenfassung:	This report summarizes the efforts on continued stability testing of aluminum-hydrazine-carbopol combinations and preparation for formulation and characterization of liquid metalized propellants containing LM-2 and LMH-2. It also summarizes the analytical and experimental investigation of the N2H4/N2O4 propellant system which was undertaken to determine its reaction kinetics at rocket chamber conditions. The background atmospheric flame studies on H2/NO2 and NH3/O2 are complete and the results are reported. Also reported is the engine performance (characteristic velocity C) of the liquid-liquid combustor and the preliminary reaction mechanism for the N2H4/N2O4 propellant system. Preliminary background information is given on a heat-of-formation study on XeF6. (Author)