A method to calculate the dry mass of single-stage vehicle is proposed in this paper. A baseline vehicle is presented for the given flight mission, and the effects of the tank material, the thermal protection system and the design margin on the vehicle dry mass are calculated. The calculation results show that the advanced material and design can decrease the vehicle dry mass and its sensitivity to the design margin.
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黄卫东,王克昌,陈启智.单级入轨运载器干质量影响因素分析. The Analysis of the Effects of the Dry Mass of Single-Stage-to-Orbit Vehicle[J].国防科技大学学报,1997,19(3):89-91.