Accession Number:

AD0616129

Title:

Calculation of Processes in the Combustion Chamber and Nozzle of a Liquid-Propellant Rocket Engine

Descriptive Note:

[Technical Report, Monograph]

Corporate Author:

AIR FORCE SYSTEMS COMMAND WRIGHT-PATTERSON AFB OH

Personal Author(s):

• Bolgarskii, A. V.

Report Date:

1959-10-01

Pagination or Media Count:

123

Abstract:

The book is devoted to questions of combustion and discharge at high temperatures in a liquid-propellant rocket engine. It gives the detailed technique for the thermodynamic calculation of the working process, illustrated by the solution of a series of practical problems. The book offers the bases for the possibility of applying a graphical method for calculating the parameters of the liquid-propellant rocket engine, which greatly facilitates this calculation. It gives a detailed exposition of the technique of constructing such nomograms. Two nomograms for two types of propellant, constructed by the author, are appended at the end of the book.

Descriptors:

Subject Categories:

• Liquid Propellant Rocket Engines
• Liquid Rocket Propellants

Distribution Statement:

[A, Approved For Public Release]