Accession Number : ADA254232


Title :   Studies on the Combustion Efficiency of Liquid Fuel Rockets with Variable Thrust


Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OH


Personal Author(s) : Xiaobin, Li ; Qizhi, Chen ; Yunqin, Chen


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a254232.pdf


Report Date : 03 Dec 1991


Pagination or Media Count : 29


Abstract : This article carries out studies on the stability characteristics of liquid fuel rocket engines within a relatively large range of variations. The research work was carried out centering around the speed and efficiency characteristics of combustion chambers. This article sets out the results of relevant experiments and theoretical calculations. From the angle of the combustion processes within combustion chambers, there were clear indications of the status of the effects of various processes (for example, evaporation or vaporization, mixing, chemical reactions, etc.) following along with changes in the operational status of variable thrust engine combustion efficiency.


Descriptors :   *EFFICIENCY , *COMBUSTION CHAMBERS , *LIQUID ROCKET FUELS , *THRUST , *ROCKET ENGINES , ENERGY TRANSFER , CHINA , CHINESE LANGUAGE , TRANSLATIONS , NITRIC ACID , EVAPORATION , PROPELLANTS , LENGTH


Subject Categories : Combustion and Ignition
      Liquid Rocket Propellants


Distribution Statement : APPROVED FOR PUBLIC RELEASE