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Tan Songlin(The North West Polytechnology University, Xi′an 710072)Wang Hongrang(Airspace Propulsion Technology Institute, Xi′an 710100)
Published:
Abstract: The parameter of tripropellants engine for SSTO is optimized on the basis of performance calculation with respect to dry mass of launcher. The optimized parameters and transfer time of engine are obtained corresponding to the dry mass of the least launcher, which will lay the foundation of the detailed design of engine in the future.
Tan Songlin(The North West Polytechnology University, Xi′an 710072)Wang Hongrang(Airspace Propulsion Technology Institute, Xi′an 710100). The Parameter Optimization of Tripropellant′s Engine for SSTO[J]. .
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http://zgkj.cast.cn/EN/Y2003/V23/I03/
