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LM-3B Successfully Launched Communications Technology Test Satellite 2
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作者 GUO Qian 《Aerospace China》 2017年第1期58-58,共1页
At 23:18 Beijing time on January 5,a LM-3B carrier rocket lifted off from the Xichang Satellite Launch Center,sending a communication technology test satellite into its preset orbit.This successful launch was a good s... At 23:18 Beijing time on January 5,a LM-3B carrier rocket lifted off from the Xichang Satellite Launch Center,sending a communication technology test satellite into its preset orbit.This successful launch was a good start for China’s launch missions in 2017.The Communications Technology Test Satellite 2 was developed by the Shanghai Academy of Spaceflight Technology.It is a next-generation telecom- 展开更多
关键词 LM-3B Successfully Launched Communications technology Test Satellite 2 TEST DATA
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China Academy of Launch Vehicle Technology
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作者 Jin Yishan China Academy of Launch Vehicle Technology 《Aerospace China》 2011年第2期14-16,共3页
OVERVIEW China Academy of Launch Vehicle Technology (CALT) was founded on November 16, 1957. It was the first research unit devoted to the development of launch
关键词 CALT China Academy of Launch Vehicle technology
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GERBER TECHNOLOGY LAUNCHES FIRST OF NEW SERIES OF CUTTING SOLUTIONS
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《China Textile》 2008年第7期9-10,共2页
Precision, Productivity and Performance def ine the GERBERcutter? Z7Tolland, Conn., USA – Gerber Technology, a business unit of Gerber Scientific, Inc. (NYSE: GRB), and the world leader in providing innovative integr... Precision, Productivity and Performance def ine the GERBERcutter? Z7Tolland, Conn., USA – Gerber Technology, a business unit of Gerber Scientific, Inc. (NYSE: GRB), and the world leader in providing innovative integrated software and hardware automation systems to 展开更多
关键词 GERBER technology LAUNCHES FIRST OF NEW SERIES OF CUTTING SOLUTIONS VOC
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Effects of Wind on Steady-state Scan Characteristics and Hit Probability of Terminal-sensitive Projectile 被引量:4
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作者 郭锐 刘荣忠 +1 位作者 王宇波 黄风华 《Defence Technology(防务技术)》 SCIE EI CAS 2010年第1期16-19,共4页
The wind effects on steady-state scan characteristics and hit probability of terminal-sensitive projectile were discussed in this paper. Considering wind as the constitutions of the average wind and the impulsive wind... The wind effects on steady-state scan characteristics and hit probability of terminal-sensitive projectile were discussed in this paper. Considering wind as the constitutions of the average wind and the impulsive wind, a simplified wind field model was established for the ballistic calculation of the steady-state scan phase; under the windy condition, the effects of the range wind and the beam wind on the steady-state scan characteristics of the terminal-sensitive projectile were analyzed in detail and its hit probabilities for a certain armored target were calculated. The calculated results show that, when the wind speed exceeds a certain value, the hit probabilities of terminal-sensitive projectile drop rapidly; the wind effects must be considered in the application of the terminal-sensitive projectiles. This paper provides some theoretical references for the fire wind speed correction and the global structure optimization of the terminal-sensitive projectile. 展开更多
关键词 launch and flight technology of aerocraft terminal-sensitive projectile steady-state scan characteristics wind speed correction hit probability
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Modeling and Simulation of Aerial Dispersion on Piston Dispersal Mechanism
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作者 陶如意 王浩 黄蓓 《Defence Technology(防务技术)》 SCIE EI CAS 2011年第4期197-203,共7页
For the aerial dispersing interior ballistic process and submunition exterior ballistic initial conditions of cluster munition with piston maximum travel limit, a novel model is established, and the numerical simulati... For the aerial dispersing interior ballistic process and submunition exterior ballistic initial conditions of cluster munition with piston maximum travel limit, a novel model is established, and the numerical simulation is performed. The piston maximum travel limit and the effect of reaction force on carrier body are researched using the internal ballistic model. Guide tube, cluster munition rotating and submunition assembly are analyzed using the submunition initial external ballistic model. The computational results are consistent with the practical process and the experimental data, and prove the rationality of this model. The theoretical methods are presented for the construction design and dispersion analysis of piston dispersal mechanism. 展开更多
关键词 launch and flight technology of aerocraft piston dispersion interior ballistics of aerial dispersion piston maximum travel assembly angle of submunition
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