Ignition of hydrogen-oxygen rocket combustor with chlorine trifluoride and triethylaluminum. [Ignition characteristics of 125-lb thrust cold gaseous hydrogen liquid oxygen rocket combustor]
Technical Report
·
OSTI ID:5167131
None
- OSTI ID:
- 5167131
- Report Number(s):
- NASA-TN-D-684
- Country of Publication:
- United States
- Language:
- English
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Related Subjects
08 HYDROGEN
080600* -- Hydrogen-- Industrial & Commercial Use-- (-1989)
ALUMINIUM COMPOUNDS
CHLORINE COMPOUNDS
CHLORINE FLUORIDES
CRYOGENIC FLUIDS
ELEMENTS
FLUIDS
FLUORIDES
FLUORINE COMPOUNDS
FUELS
HALIDES
HALOGEN COMPOUNDS
HYDROGEN FUELS
NONMETALS
ORGANIC COMPOUNDS
ORGANOMETALLIC COMPOUNDS
OXYGEN
PROPULSION
ROCKETS
SYNTHETIC FUELS
080600* -- Hydrogen-- Industrial & Commercial Use-- (-1989)
ALUMINIUM COMPOUNDS
CHLORINE COMPOUNDS
CHLORINE FLUORIDES
CRYOGENIC FLUIDS
ELEMENTS
FLUIDS
FLUORIDES
FLUORINE COMPOUNDS
FUELS
HALIDES
HALOGEN COMPOUNDS
HYDROGEN FUELS
NONMETALS
ORGANIC COMPOUNDS
ORGANOMETALLIC COMPOUNDS
OXYGEN
PROPULSION
ROCKETS
SYNTHETIC FUELS