Simulation of Missile Head Cover Separation and Landing Locations

Authors

Tian Hao, 1.School of Astronautics, Harbin Institute of Technology, Harbin 150001, China; ;
Mu Zhou, 2.Beijing Institute of Aerospace Systems Engineering, Beijing 100076, China; ;
Huitong Li, 3.Beijing Institute of Mechanical Equipment, Beijing 100854, China;
Zhao Yang, 1.School of Astronautics, Harbin Institute of Technology, Harbin 150001, China; ;

Abstract

Abstract: Some missiles use head cover to protect the internal equipment during the launching process. In order to prevent the head cover from damaging the people or equipment after separation, researchers need to predict the landing position range and take protective measures. This paper designs a separation scheme for a missile head cover separation based on solid propellant gas generator and solid rocket. In this study, we establish a dynamic simulation model of head cover separation and falling procedure. The simulation calculation of the head cover location range considering multiple factors using Monte-Carlo method is developed. And the motional curve of separation bodies and the danger zone of head cover landing location are obtained. The simulation results in this paper will provide technical support for rocket launcher and personnel protection design.

Recommended Citation

Hao, Tian; Zhou, Mu; Li, Huitong; and Yang, Zhao (2019) "Simulation of Missile Head Cover Separation and Landing Locations," Journal of System Simulation: Vol. 30: Iss. 3, Article 36.
DOI: 10.16182/j.issn1004731x.joss.201803036
Available at: https://dc-china-simulation.researchcommons.org/journal/vol30/iss3/36

First Page

1056

DOI Link

https://doi.org/10.16182/j.issn1004731x.joss.201803036

Last Page

1062

CLC

V475.1

Recommended Citation

Tian Hao, Mu Zhou, Li Huitong, Zhao Yang. Simulation of Missile Head Cover Separation and Landing Locations[J]. Journal of System Simulation, 2018, 30(3): 1056-1062.

DOI

10.16182/j.issn1004731x.joss.201803036