Aluminized solid propellant transient burning rate augmentation during acceleration loads
Effects of the acceleration vector on transient burning-rate augmentation of an aluminized solid propellant
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, AEROSPACE SCIENCES MEETING, 8TH ; 1970 ; NEW YORK, NY
01.01.1970
Aufsatz (Konferenz)
Keine Angabe
Englisch