[1]李高春,李树谦,郭宇,等.不同温度和拉伸速率下复合推进剂力学性能及破坏模式分析[J].固体火箭技术,2019,42(03):297-302.
 LI Gaochun,LI Shuqian,GUO Yu,et al.Mechanical properties and failure mode of composite solid propellant under different temperatures and tensile rates[J].Journal of Solid Rocket Technology,2019,42(03):297-302.
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不同温度和拉伸速率下复合推进剂力学性能及破坏模式分析

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更新日期/Last Update: 2019-07-11
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