Research on safety judgment method of forward separation of protective shield

  • ZOU Dong-Yang ,
  • WU An-Ping ,
  • LIN Jing-Zhou
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Received date: 2024-07-29

  Revised date: 2024-10-07

  Online published: 2024-10-11

Abstract

The purpose of the research on safety boundary of multi-body separation is to find suitable safety design criterion or system analysis method, and to provide reference for relevant professional design, so as to provide optimization basis and solution for safety separation design. In this paper, the safety boundary of high Mach number forward separation of protective shield is studied, and the criterion of safety boundary of typical forward separation between protective shield and projectile and the inequality of back-pursuing collision of protective shield are put forward. The judge criterion of safety boundary can be used to research on the safety of shields during the axial direction separation stage. It can also provide a basis for the design of separation schemes and the selection of engine types. The back-pursuing collision inequality establishes the relationship between the motion parameters at the initial moment of free motion and the motion acceleration of the protective shield, which provides a reference for predicting the later motion of the protective shield. According to the initial state, the safety of the separation process of the protective cover can be judged by using the safety boundary criterion and the back-pursuing collision inequality, which provides reference for the separation design related majors.

Cite this article

ZOU Dong-Yang , WU An-Ping , LIN Jing-Zhou . Research on safety judgment method of forward separation of protective shield[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 0 : 0 -0 . DOI: 10.7527/S1000-6893.2024.31005

References

[1]钟俊, 林敬周, 解福田, 等.高超声速大动压下整流罩分离测力风洞试验[J].实验流体力学, 2022, 36(X):1-9 [2]ZHONG J, LIN J Z, XIE F T, et al.Wind tunnel force test of fairing separation in hypersonic and high dynamic pressure situation[J].Journal of Experiments in Fluid Mechanics, 2022, 36(X):1-9 [3]王海清, 杨正才, 刘海旭, 等.某头罩分离装置分离全过程仿真计算[J].兵工自动化, 2020, 39(02):68-72 [4]WANG H Q, YANG Z C, LIU H X, et al.Simulation Calculation of the Whole Separation Process for a Shroud Separation Device[J].Ordnance Industry Automation, 2020, 39(02):68-72 [5]UNAL K, BARAN O U.A modeling and simulation tool for safe store separation envelope generation using Monte Carlo simulations[C]. 2018 AIAA Modeling and Simulation Technologies Conference, 2018, Florida. [6]ROSHANIAN J, TALEBI M.Monte Carlo simulation of stage separation dynamics of a multistage launch vehicle.[J].Applied Mathematics and Mechanics(English Edition), 2008, —(11):1411-1426 [7]陈波, 刘刚, 肖涵山, 等.基于蒙特卡罗模拟的导弹分离边界计算方法研究[J].空气动力学学报, 2012, 30(04):508-513 [8]CHEN B, LIU G, XIAO H S, et al.Application of Monte Carlo simulation for the boundary of separation trajectories of a missile[J].Acta Aerodynamica Sinica, 2012, 30(04):508-513 [9]VADDI S S, NGUYEN J, MENON P K.Data mining and knowledge discovery from store separation tragectories[C]. AIAA Atmospheric Flight Mechanics Conference, 10-13 August 2009, Chicago. [10]张永杰, 孙秦.整体式头罩分离运动轨迹可靠性分析[J].弹箭与制导学报, 2011, 31(1):19-22 [11]ZHANG Y J, SUN Q.Reliability analysis on separation trajectory of integral nose cap[J].Journal of Projectiles Rockets Missile and Guidance, 2011, 31(1):19-22 [12]COVERT E E.Conditions for safe separation of external stores[J].Journal of Aircraft, 1980, 18(8):624-630 [13]彭兢, 王衍洋, 金长江.飞机外挂物发射投放运动的数值仿真方法[J].飞行力学, 1997, 15(3):24-29 [14]Peng J, Wang X Y, Jin C J.Numerical simulation method of mot ion of external stores ejected dropped from an aircraft[J].Flight Dynamics, 1997, 15(3):24-29 [15]王慧哲.机载导弹安全分离研究[D]. 北京理工大学, 2016. WANG H Z. Safety separation of airborne missile[D]. Beijing Institue of Technology, 2016 (in Chinese). [16]王慧哲, 李响, 王晓鹏, 等.机载导弹安全分离评估方法研究[J].上海航天, 2017, 34(5):124-129 [17]WANG H Z, LI X, WANG X P, et al.Safety assessment for store separation[J].Aeraspace Shanghai, 2017, 34(5):124-129 [18]张杰.机载导弹的分离安全性分析和制导律研究[D]. 北京理工大学, 2018. [19]ZHANG J.Separation safety analysis and guidance law of airborne missile[D]. Beijing Institue of Technology, 2018 (in Chinese). DOI:10.26948/d.cnki.gbjlu.2018.002016. [20]宋威, 秦汉, 廖鹏.外挂物分离安全性的近似评估方法及验证[J].气动研究与试验, 2023, 1(3):56-63 [21]SONG W, QIN H, LIAO P.Approximate evaluation method and verification of external store separation safety[J].Aerodynamic Research & Experiment, 2023, 01(03):56-63
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