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- W2393069709 abstract "An investigation of throttle capability was conducted on foreign liquid rocket engines,including applications of RD-180,SSME for Atlas series and space shuttle respectively. A series of launch vehicles were presented in this paper. A 2500 kN LOX-kerosene engine was used as the liftoff power and 4 types of launch vehicles were designed with modularization methods. In order to optimize the performance of launch vehicle series,the throttle influence was studied. The influence includes launch capacity,impact zone adjustment,off-load design. Finally,the demand for throttle capability of the 2500 kN LOX-kerosene engine was proposed." @default.
- W2393069709 created "2016-06-24" @default.
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- W2393069709 date "2014-01-01" @default.
- W2393069709 modified "2023-09-23" @default.
- W2393069709 title "Effects of Throttle Capability on Overall Performance of Launch Vehicle Series" @default.
- W2393069709 hasPublicationYear "2014" @default.
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