Accession Number : ADA118931

Title :   Method of Calculating Rocket Engine Nozzle Contour for Optimum Thrust,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH

Personal Author(s) : Minhua,Tian

PDF Url : ADA118931

Report Date : 03 Aug 1982

Pagination or Media Count : 8

Descriptors :   *Rocket nozzles, *Rocket engines, *Thrust, Configurations, Computations, Translations, China, Optimization

Subject Categories : Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE