Temperature Control System Design for a Certain Missile Launch Canister Based on Semiconductor Refrigeration

ZHANG  Zhili; HOU  Chuanxun; JIANG  Yi; QI  Yuejing

doi:10.15892/j.cnki.djzdxb.2011.01.024

ZHANG Zhili, HOU Chuanxun, JIANG Yi, QI Yuejing

Journal of Projectiles, Rockets, Missiles and Guidance ›› 2011, Vol. 31 ›› Issue (1) : 231-236.

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Journal of Projectiles, Rockets, Missiles and Guidance ›› 2011, Vol. 31 ›› Issue (1) : 231-236. DOI: 10.15892/j.cnki.djzdxb.2011.01.024

CORRELATION TECHNOLOGY

Temperature Control System Design for a Certain Missile Launch Canister Based on Semiconductor Refrigeration

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{{article.zuoZheEn_L}}. {{article.title_en}}[J]. {{journal.qiKanMingCheng_EN}}, 2011, 31(1): 231-236 https://doi.org/10.15892/j.cnki.djzdxb.2011.01.024

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Received	Published
2010-03-16	2011-02-20
Issue Date
2025-05-30

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