Characteristics of solid propellant motor aft- end ignitionAft-end igniter design and placement for solid propellant rocket motors avoiding overpressurization and nozzle pressure oscillations
Document ID
19700064776
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fitch, R. E.
Kilgroe, J. D.
Date Acquired
August 5, 2013
Publication Date
July 1, 1970
Subject Category
Propulsion Systems
Meeting Information
Meeting: JOINT ARMY-NAVY-AIR FORCE SOLID PROPULSION MEETING, 26TH
Location: WASHINGTON, DC
Start Date: July 14, 1970
End Date: July 16, 1970
Sponsors: JOINT ARMY NAVY AIR FORCE SOLID PROPULSION MEETING