Transients influencing rocket engine ignition and popping Interim report
Engine design and operating parameters studied for effects on rocket engine ignition and popping
Breen, B. P.↗
Engineering topics
Publications and source records attributed to Tkachenko, E. A..
Engine design and operating parameters studied for effects on rocket engine ignition and popping
Ignition mechanism of hydrazine-nitrogen dioxide hypergolic propellant system
Measurement of heat release rate for liquid phase reaction of nitrogen tetroxide and hydrazine
Analytical model for describing combustion chamber disturbances during start transient and steady state operations of hypergolic liquid rocket engines