Accession Number : AD0688729

Title :   FUNDAMENTALS OF THEORY AND CALCULATION OF LIQUID-PROPELLANT ROCKET ENGINES, VOLUME II,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Vasilev,A. P. ; Kudryavtsev,V. M. ; Kuznetsov,V. A. ; Kurpatenkov,V. D. ; Obelnitskii,A. M.

Report Date : 03 JAN 1969

Pagination or Media Count : 308

Abstract : The report presents theory and calculations of mechanics involved in operation of a liquid rocket engine.

Descriptors :   (*LIQUID PROPELLANT ROCKET ENGINES, THEORY), COMBUSTION CHAMBERS, INJECTORS, LIQUID ROCKET PROPELLANTS, COMBUSTION, SPECIFIC IMPULSE, HEAT TRANSFER, GAS GENERATING SYSTEMS, ROCKET IGNITERS, COMBUSTION CHAMBER GASES, NOZZLE GAS FLOW, LAVAL NOZZLES, TURBOPUMPS, USSR

Subject Categories : Liquid Propellant Rocket Engines
      Liquid Rocket Propellants

Distribution Statement : APPROVED FOR PUBLIC RELEASE