Accession Number : ADA310522

Title :   Aerodynamic Design Research of the Gas Vane of a Solid Rocket,

Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH

Personal Author(s) : Zhiheng, Liu

PDF Url : ADA310522

Report Date : JUL 1996

Pagination or Media Count : 25

Abstract : Several issues involved in the aerodynamic design of the gas vane of a solid rocket, such as jet flowfield analysis, material selection and property analysis, theoretical configuration and aerodynamic characteristics design, as well as wind tunnel tests of the gas vane model and force measurement tests of a full-scale vane during rocket engine firing, etc., are presented. Integration of aerodynamic characteristics with strength, stiffness, as well as ablation value of the vane will make development of gas vanes more smooth.

Descriptors :   *AERODYNAMIC CONFIGURATIONS, *SOLID PROPELLANT ROCKET ENGINES, TEST AND EVALUATION, ABLATION, MEASUREMENT, CONTROL SYSTEMS, FOREIGN TECHNOLOGY, MATERIALS, STIFFNESS, STRENGTH(MECHANICS), FLOW FIELDS, INTEGRATION, AERODYNAMIC CHARACTERISTICS, WIND TUNNEL TESTS, TRANSLATIONS, SELECTION, JET FLOW, CHINA, FORCE(MECHANICS), CHINESE LANGUAGE, FOREIGN LANGUAGES.

Subject Categories : Solid Propellant Rocket Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE