Computer modeling of rocket engine ignition transients Final report
Computer modeling of rocket engine ignition transients
Breen, B. P.↗
Engineering topics
Breen, B. P.
Publications and source records attributed to Breen, B. P..
A basic study of the ignition of hypergolic liquid propellants Final report
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction products of dimethylhydrazines with nitrogen dioxide
Breen, B. P.↗
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.↗
Combustion instability response with asymmetric pressure disturbances
Combustion stability in rocket engines affected by pressure disturbances
Breen, B. P.↗
A Basic Study on the Ignition of Hypergolic Liquid Propellants Interim Report
Ignition mechanism of hydrazine-nitrogen dioxide hypergolic propellant system
Breen, B. P.↗
Hypergolic stream impingement phenomena nitrogen tetroxide/hydrazine
Mechanism and design parameter effects in stream mixing and separation of nitrogen tetroxide-hydrazine impingement
Breen, B. P.↗
A basic study of ignition of hypergolic liquid propellants.
Liquid hydrazine ignition by nitrogen tetroxide gas based on stagnation flow principle, presenting threshold measurements
Breen, B. P.↗
Combustion instability prediction using a nonlinear bipropellant vaporization model
Combustion instability prediction using nonlinear bipropellant vaporization model
Breen, B. P.↗
The effect of additives on droplet hydrazine burning.
Effect of additives on hydrazine nitrogen trioxide droplet flame structure and burning rate
ADDITIVE↗
A mathematical model of random wave phenomena in hypergolic propellant combustion.
Physical and chemical conditions in rocket combustion chamber during starting transients and steady operation described by mathematical model intended for parametric studies
COMBUSTION CHAMBER↗
Investigation of the Flame Structure of a Thermally Unstable Fuel
Flame structure of hydrazine droplet burning in nitrogen tetroxide vapor
BURNING RATE↗
Study of random wave phenomena in hypergolic propellant combustion
Analytical model for describing combustion chamber disturbances during start transient and steady state operations of hypergolic liquid rocket engines
LIQUID PROPELLANT ROCKET ENGINE↗
Effect of additives on the ignition delay time of hypergolic propellants.
Additives effect on ignition delay and pressure of hypergolic hydrazine-nitrogen tetroxide propellant systems.
TIME DELAY↗
Measurement of the flame structure of a thermally unstable fuel in an oxidizing atmosphere.
Flame structure of hydrazine burning in oxidizing atmosphere determined by measuring temperature and specific contractions at 90 degrees from stagnation point
TEMPERATURE MEASUREMENT↗