Accession Number:

AD0645793

Title:

THERMODYNAMIC AND BALLISTIC DESIGN FUNDAMENTALS OF SOLID-PROPELLANT ROCKET ENGINES,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

• Orlov,B. V.
• Mazing,G. Yu.

Report Date:

1966-06-16

Pagination or Media Count:

397.0

Abstract:

In this book, on the basis of materials published in the Soviet and foreign press, there are expounded thermo-gas-dynamic principles of designing of rocket engines, engineering methods of calculation of processes of heat exchange, principles of the theory of burning of solid fuels and calculation of the indicated pressure curve in the combustion chamber of the engine. In it there is given basic information about solid rocket propellants applied in solid-propellant rocket engines SPRE. There is considered regulation of thrust in SPRE in magnitude and direction, and also a general method of ballistic designing of solid-fuel rockets. Author

Descriptors:

• *SOLID PROPELLANT ROCKET ENGINES
• THERMODYNAMICS
• EXTERIOR BALLISTICS
• FLUID MECHANICS
• NOZZLES
• GAS FLOW
• HEAT TRANSFER
• SOLID ROCKET PROPELLANTS
• DOUBLE BASE ROCKET PROPELLANTS
• COMPOSITE PROPELLANTS
• ROCKET PROPELLANT GRAINS
• COMBUSTION
• COMBUSTION PRODUCTS
• ABLATION
• THRUST VECTOR CONTROL SYSTEMS
• THRUST
• SPECIFIC IMPULSE
• BURNING RATE
• LAUNCHING
• USSR

Subject Categories:

• Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE