Accession Number : AD0884746
Title : Explosive Impulse Calculations.
Descriptive Note : Final rept.,
Corporate Author : PHYSICS INTERNATIONAL CO SAN LEANDRO CA
Personal Author(s) : Gross, Michael
Report Date : NOV 1970
Pagination or Media Count : 77
Abstract : The specific impulse of an explosive-plate system was calculated using a one-dimensional hydrodynamic computer code. Parameters affecting the delivered impulse, including charge-to-mass ratio, explosive composition, plate material, and stand-off distance, were varied. Calculations were compared to available experimental data which verified their accuracy. The computed impulse from conventional military explosives was less than 250 seconds. Increased efficiency resulted from the use of a nozzle which produced an impulse of approximately 270 seconds and from a high energy, aluminized explosive model with an impulse of 321 seconds. (Author)
Descriptors : (*SOLID PROPELLANT ROCKET ENGINES, SPECIFIC IMPULSE), ALUMINIZED EXPLOSIVES, SOLID ROCKET PROPELLANTS, BURNING RATE, KINETIC ENERGY, METAL PLATES, STRESSES, YIELD POINT, COMPUTER PROGRAMMING, APPROXIMATION(MATHEMATICS), EXPERIMENTAL DATA.
Subject Categories : Solid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE