[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]
ROCKETS TECHNOLOGY

The Study on Load Technique for Rocket Sled Experiment

  • LI Jinhe ,
  • PANG Yong ,
  • ZHAO Jibo
Expand
  • Laboratory for Shock Wave and Detonation Physics, Institute of Fluid Physics, China Academy of Engineering Physics, Sichuan Mianyang 621900, China

Received date: 2009-09-29

  Online published: 2025-05-28

Abstract

The rocket sled loading technique is very important for rocket sled experiment.The rocket sled running process was estimated by fourth-order Runge-Kutta based on rocket’s fitting force curve and average force curve applying with the aerodynamics theory.The velocity history and displacement in the supersonic running process were calculated,and the maximum velocity and the derailment velocity were achieved.The estimated results are well in accordant with the experimental results,which indicates that the calculated results based on fitting force curve can reflect the rocket sled running process very well.

Cite this article

LI Jinhe , PANG Yong , ZHAO Jibo . The Study on Load Technique for Rocket Sled Experiment[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(5) : 137 -139,146 . DOI: 10.15892/j.cnki.djzdxb.2010.05.007

[an error occurred while processing this directive]

References

[1]
Andrew J L.Computational aerodynamic analysis of the flow field about a hypervelocity test sled[D].Air Force Institute of Technology Graduate School of Engineering and Management,2002
[2]
Gregory L F. Dynamic analysis of a sled traveling along a rough rail. 6585th test group (AFSC) test track division, 1985.
[3]
韩永, 郑伟, 汤建国. 火箭橇试验技术发展综述[J]. 导航与控制, 2006, 5(3): 64- 71.
[4]
James L L. Critical velocities for rocket sled excitation of rail resonance[J]. Johns Hopkins APL Technical Digest, 2000, 21(3): 448- 458.
[5]
周真学, 周绍慧. 国外火箭滑车图册[M]. 北京: 国防工业出版社, 1979.
[6]
吴国强. 中国襄北火箭滑轨试验场[J]. 国际航空, 1996(1): 49- 50.
[7]
韩振江, 张建平. 051基地火箭滑车轨道设计要点分析[J]. 中国铁路, 2004(11): 31- 32.
[8]
赵继波, 赵峰, 谭多望, 等. 火箭橇加载试验技术研究[J]. 爆炸与冲击, 2007, 27(6): 572- 576.
[9]
王元友. 固体火箭发动机设计[M]. 北京: 国防工业出版社, 1984.
Outlines

/

[an error occurred while processing this directive]