THE EXAMINATION OF CHOSEN BALLISTIC PARAMETERS OF IGNITER CHARGE BKNO{sub}3 FOR IGNITERS OF SOLID PROPELLANT ROCKET MOTORS

摘要

The preliminary results ofpyrostatic investigations of ignition tablets BKNO{sub}3 were prestented. The investigations were performed in especially designed for this purpose rocket engine with established constant loading density. The time of burning and dynamics of process were estimated.