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《Tactical Missile Technology》 1990-01
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METHOD FOR ANALYSING AND CALCULATING STRUCTURAL DEVIATION CHARACTER OF BALISTIC MISSILE

First Academy of MAS Zhao Shaokui  
A method for analysing and calculating basic structural deviation charactors of a missile was proposed. For illustrating present method, a two-stagy liquid-propellant missile, as an example, was analysed. A method can rationalize the design of missile system further, therefor, can be extended to design for the carrier rocket and other kinds of missile.
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【Citations】
Chinese Journal Full-text Database 1 Hits
1 Zhao shaokui;AN ANALYSIS AND MEASUREMENT METHOD FOR THRUST LINE DEVIATION OF LAUNCH VEHICLE[J];Journal of Astronautics;1984-01
【Co-citations】
Chinese Journal Full-text Database 1 Hits
1 ZHANG Chun-fu1,TANG Wen-yan1,LI Hui-peng1,WANG Jun1,CHEN Jin-cun2 (1.Harbin Institute of Technology,Harbin 150001,China;2.Capital Aerospace Machinery Corp.,Beijing 100076,China);Application of laser tracker to thrust line measurement of solid rocket motor[J];Journal of Solid Rocket Technology;2007-06
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