Solid-Propellant Rocket Engines,

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Abstract:

The book describes the motion of combustion products in the chamber and nozzle of solid-propellant rocket engine. The spreads of intrachamber and output characteristics of RDTT, caused by random and systematic deviations of the loading parameters are analyzed. The effect of the engine and propellant characteristics on the ideal velocity of the rocket is also analyzed. The book also examines the procedure for profiling of nozzles, the motion of two-phase combustion products, and the calculation and design of charges from solid rocket propellants.

Author(s):
Vinitskii, A. M.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited machine trans. of mono. Raketnye Dvigateli na Tverdom Toplive, Moscow, 1973 p1-348, by Robert Allen Potts.
Annotation:
Solid-Propellant Rocket Engines--Translation.
Pagination:
0454

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-MT-24-328-74
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application; JCA_3.2.1_Kinetic Means
Communities of Interest:
Weapons Technologies
Descriptor(s):
*Solid propellant rocket engines, Translations, Equations of motion, Combustion chambers, Combustion products, Solid rocket propellants, Rocket nozzles, Thrust, Interior ballistics, Gas dynamics, USSR
Field(s)/Group(s):
Solid Propellant Rocket Engines
Report Date:
1974 Apr 09