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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
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.
Distribution Statement:
[A, Approved For Public Release]