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Test Technique in Ballistic Range for Missile Models

《南京理工大学学报》(自然科学版)[ISSN:1005-9830/CN:32-1397/N]

Issue:
2007年05期
Page:
537-540
Research Field:
Publishing date:
2007-10-30

Info

Title:
Test Technique in Ballistic Range for Missile Models
Author(s):
YI Wen-jun1WANG Zhong-yuan1QIAN Ji-sheng1SONG Cheng-jun2
1.National Key Laboratory of Transient Physics,NUST,Nanjing 210094,China;2.Naval Ammunition Mission at Shenyang Zone,Shenyang 110045,China
Keywords:
ballistic range m issile models theory of sim ilarity aerodynam ics characteristics
PACS:
TJ760.6
DOI:
-
Abstract:
On the basis o f the essent ial condition o f ba llist ic range experimen,t th is paper ana lyzes the motion pattern and test measuring methods of m issile models. flight exper iment under non-contro l condit ion. The paper studies comparability relat ions and cond itions betw een m issile model and orig inalmodel in ballistic parameters and flight stab ility. The feasib ility of app ly ing m issile model range experimen tal data inm issilemo tion and aerodynam ics characteristic is ana lyzed. Tak ing an essent ialm issile for example, am issile model in ballistic range experim ent is designed, the proper arithmetic is chosed and experiments aremade many t imes. The fina l exper iment proves that the experim ent scheme described in this paper is effective and reliab le.

References:

[ 1] 刘世平, 易文俊, 顾金良. 弹道靶道数据判读与处理方法研究[ J]. 兵工学报, 2000( 3): 201- 204.
[ 2] 宋丕极. 枪炮与火箭外弹道学[M ] . 北京: 兵器工业出版社, 1993.
[ 3] 浦发, 芮筱亭. 外弹道学[M ]. 北京: 北京工业学院出版社, 1987.
[ 4] 吕学富. 飞行器飞行力学[M ]. 西安: 西北工业大学出版社, 1995.
[ 5] 刘世平. 弹丸速度测量与数据处理[M ] . 北京: 兵器工业出版社, 1994.

Memo

Memo:
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Last Update: 2007-10-30