APPLICATION OF A COMPACT COMBUSTOR IN SMALL-SCALE JETCAT ENGINES
A SIMPLIFIED MODEL FOR THE THRUST PERFORMANCE OF POROUS HEAT EXCHANGER (PHX) LASER ROCKET PROPULSION
DEFLAGRATION TO DETONATION TRANSITION IN CHEMICAL ROCKETS WITH SUDDEN EXPANSION/DIVERGENCE REGION
POSSIBLE EFFECTS OF TURBINE/FUEL CELL INTEGRATION ON COMBUSTOR OPERATION