Accession Number : ADA310488
Title : Design and Development of Large Model Dual Component Exhaust Propulsion Systems,
Corporate Author : NATIONAL AIR INTELLIGENCE CENTER WRIGHT-PATTERSON AFB OH
Personal Author(s) : Wang, Dong ; Yang, Ruiting
PDF Url : ADA310488
Report Date : MAY 1996
Pagination or Media Count : 19
Abstract : As far as super charging improvements carried out on large model dual component propulsion systems are concerned, they make the new systems completely different from the pressure regulated systems at the present time. From considerations of the three areas of thrust chamber design, performance, and system structure, operating conditions associated with new designs all have important technological advances. Test measurements have been carried out with regard to system levels through thrust chamber thermal tests. In conjunction with this, verifications have been carried forward in respect to propulsion system exhaust design life limits.
Descriptors : *THRUST CHAMBERS, *EXHAUST SYSTEMS, TEST AND EVALUATION, THERMAL PROPERTIES, MEASUREMENT, TRANSLATIONS, CHINA, CHINESE LANGUAGE, DUAL THRUST ROCKET ENGINES.
Subject Categories : Rockets
Distribution Statement : APPROVED FOR PUBLIC RELEASE