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[1]严博燕,吕江彦,刘元敏.固体火箭发动机喷管扩张段壳体结构优化设计[J].火箭推进,2019,45(03):54-58.
 YAN Boyan,LYU Jiangyan,LIU Yuanmin.Optimal design on solid rocket motor nozzle divergent cone[J].Journal of Rocket Propulsion,2019,45(03):54-58.
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固体火箭发动机喷管扩张段壳体结构优化设计

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备注/Memo

收稿日期:2017-11-19
基金项目:973项目(613184)
作者简介:严博燕(1988—),女,硕士,研究领域为固体火箭发动机喷管设计

更新日期/Last Update: 2019-06-30