Accession Number : AD0701998

Title :   THERMODYNAMIC AND BALLISTIC PRINCIPLES FOR THE DESIGN OF SOLID-PROPELLANT ROCKET ENGINES (SELECTED CHAPTERS),

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Orlov,B. V. ; Mazing,Yu. G.

Report Date : 14 JAN 1970

Pagination or Media Count : 284

Abstract : This book, on the basis of materials published in the domestic and foreign press, presents the thermogasodynamics principles of the design of engines, the engineering methods of calculating heat exchange processes, the principles of solid propellant combustion, and the calculation of the indicator curve of pressure in the engine combustion chamber. The book gives basic information on solid propellants used in solid rocket engines. Thrust regulation in solid rocket engines and the ballistic principles of solid rocket engines are examined. The book is intended for students in higher technical education institutes and for engineers-technicians specializing in solid fuel rocket engines. (Author)

Descriptors :   (*SOLID PROPELLANT ROCKET ENGINES, INTERIOR BALLISTICS), CONVECTION(HEAT TRANSFER), THERMAL RADIATION, ABLATION, ROCKET ENGINE CASES, ROCKET PROPELLANT GRAINS, EROSIVE BURNING, ROCKET NOZZLES, COMBUSTION PRODUCTS, BURNING RATE, PROTECTIVE TREATMENTS, USSR, TEXTBOOKS

Subject Categories : Ballistics
      Solid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE