Quenching of solid rocket propellants by depressurization.
Solid rocket propellant quenching by depressurization, noting gas-side heat transfer coefficient
PRESSURE EFFECT↗
Engineering topics
Publications and source records attributed to Paulson, R. A..
Solid rocket propellant quenching by depressurization, noting gas-side heat transfer coefficient
Chamber pressure balanced piston nozzle for fast depressurization to bring about combustion quenching
Multiple start-stop solid propellant rocket motor using highly aluminized ammonium perchlorate annular propellant grains