Preignition phenomena in small A-50/NTO pulsed rocket engines.
Preignition phenomena in small Aerozine-50/ nitrogen tetroxide pulsed rocket engines shown partly due to hydrazine nitrate accumulation
Christos, T.↗
Engineering topics
Christos, T.
Publications and source records attributed to Christos, T..
Preignition phenomena in small A-50/NTO pulsed rocket engines.
Preignition phenomena in small Aerozine- 50/nitrogen tetroxide pulsed rocket engines shown partly due to hydrazine nitrate accumulation
PROPELLANT COMBUSTION↗
Exploratory study of hypergolic ignition spike phenomena, phase 2, part 2, July 1 to September 30, 1966
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrate
Christos, T.↗
Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965
Summary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket engines
HYPERGOLIC PROPELLANT↗