Accession Number : ADA137199

Title :   A Calculation of Descent Segment of Internal Ballistics in Solid Rocket Motors,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Dingyou,F

PDF Url : ADA137199

Report Date : 05 Jan 1984

Pagination or Media Count : 16

Descriptors :   *Interior ballistics, *Descent, *Solid propellant rocket engines, *Predictions, Guided missiles, Performance(Engineering), Combustion chamber gases, Parameters, Combustion chambers, Isentrope, Models, Numerical methods and procedures, Entropy, Gas flow, Velocity, Pressure, Temperature, Translations, China

Subject Categories : Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE