Experimental investigation of the problems associated with restarting hybrid rocket motors (i.e., motors wherein a liquid or gaseous oxidizer is injected into the port of a solid fuel grain with subsequent mixing and combustion of the oxidizer and fuel) following a brief period of extinguishment. The results include the finding that the ignition delay on restart is decreased because less energy is absorbed by the fuel before the surface reaches the ignition point.
Restart transients of hybrid rocket engines.
01.03.1973
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Englisch
Restart transients of hybrid rocket engines.
AIAA | 1973
|Springer Verlag | 2012
|Online Contents | 1995
Restart of theory of air-breathing engines
AIAA | 1992