Accession Number:

AD0601547

Title:

THE THEORY OF ROCKET ENGINES.

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1964-03-20

Pagination or Media Count:

619.0

Abstract:

The subject of the book is the general theory and design of thermal rocket engines of various kinds. The writer discusses the operation, characteristics, and parameters of engines using chemical energy derived from liquid and solid rocket propellants. The book is intended for use as a textbook by students in colleges of aviation and other university-level institutions specializing in aircraft power plants. Engineers working in this field will also find it helpful. Soviet editors note

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE