An Analysis of Structural Integrity for Solid Propellant Grain at Extreme Temperature Launching

YANG  Junhui; LEI  Yongjun; MENG  Shangyang

doi:10.15892/j.cnki.djzdxb.2014.06.025

YANG Junhui, LEI Yongjun, MENG Shangyang

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2014, Vol. 34 ›› Issue (6) : 95-98.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2014, Vol. 34 ›› Issue (6) : 95-98. DOI: 10.15892/j.cnki.djzdxb.2014.06.025

PROJECTILES TECHNOLOGY

An Analysis of Structural Integrity for Solid Propellant Grain at Extreme Temperature Launching

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2014, 34(6): 95-98 https://doi.org/10.15892/j.cnki.djzdxb.2014.06.025

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Received	Published
2013-12-23	2014-12-20
Issue Date
2025-05-30

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