留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

多级运载火箭动态级间分离的MonteCarlo仿真

J·柔沙尼安 M·塔利班

J·柔沙尼安, M·塔利班. 多级运载火箭动态级间分离的MonteCarlo仿真[J]. 应用数学和力学, 2008, 29(11): 1279-1292.
引用本文: J·柔沙尼安, M·塔利班. 多级运载火箭动态级间分离的MonteCarlo仿真[J]. 应用数学和力学, 2008, 29(11): 1279-1292.
J. Roshanian, M. Talebi. Monte Carlo Simulation of Stage Separation Dynamic of a Multistage Launch Vehicle[J]. Applied Mathematics and Mechanics, 2008, 29(11): 1279-1292.
Citation: J. Roshanian, M. Talebi. Monte Carlo Simulation of Stage Separation Dynamic of a Multistage Launch Vehicle[J]. Applied Mathematics and Mechanics, 2008, 29(11): 1279-1292.

多级运载火箭动态级间分离的MonteCarlo仿真

详细信息
  • 中图分类号: V421.7;O242.2

Monte Carlo Simulation of Stage Separation Dynamic of a Multistage Launch Vehicle

  • 摘要: 提出了研究多级运载火箭级间冷、热分离的计算公式.利用Monte Carlo仿真,考虑箭体分离时,采用远离正常设计值的参数去评估分离失败的风险.分析了各种扰动,如动态不平衡,剩余推力,分离机构引起的分离扰动,以及冷、热分离未对准的影响,得到分离箭体不会发生碰撞的条件.结果表明,当前设计满足分离要求.
  • [1] Chubb W.The collision boundary between the two separating stages of the SA-4 Saturn Vehicle[R]. NASA-TND-598,1961.
    [2] Palmer G D,Mitchell D H.Spring separation of spacecraft[R]. NASA-CR-64009,1963.
    [3] Dwork M.Coning effects caused by separation of spin stabilized stages[J].AIAA Journal,1963,1(11):2639-2640. doi: 10.2514/3.2131
    [4] Wilke R O.Comments on coning effects caused by separation of spin stabilized stages[J].AIAA Journal,1964,2(7):1358. doi: 10.2514/3.2932
    [5] Pugisi A G.Saturn IB/S-IVB stage separation controllability report[R]. Douglas report SM-46758,1964.
    [6] Decker J P,Pierpont P K.Aerodynamic separation characteristics of conceptual parallel-staged reusable launch vehicle at Mach 3 to 6[R]. NASA-TMX-1051,1965.
    [7] Decker J P.Aerodynamic abort-separation characteristics of a parallel staged reusable launch vehicle from Mach 0.60 to 1.20[R]. NASA-TMX-1174,1965.
    [8] Decker J P,Gera J.An exploratory study of Parallel-stage separation of reusable launch vehicles[R]. NASA-TND-4765,1968.
    [9] Christensen K L,Narahara R M.Spacecraft separation[J].Space Aeronautics,1996,46(7):74-82.
    [10] Palmer G D,Mitchell D H.Analysis and simulation of a high accuracy spacecraft separation system[J].Journal of Spacecraft and Rockets,1996,3(4):458-463.
    [11] Waterfall A P.A Theoretical study of the multi-spring stage separation system of the black arrow satellite launcher[R]. Royal Aerospace Establishment,TR-682016, Farnborough Hants,UK., 1968.
    [12] Bolster W J,Googins G G.Design, development and testing of a series of Air-Launched sounding rockets[J].Journal of Spacecraft and Rockets,1969,6(4):460-465. doi: 10.2514/3.29679
    [13] Longren D R.Stage separation dynamics of spin stabilized rockets[J].Journal of Spacecraft and Rockets,1970, 7(4):434-439. doi: 10.2514/3.29959
    [14] Hurley M J Jr,Carrie G W.Stage separation of parallel-staged shuttle vehicles: A capability assess- ment[J].Journal of Spacecraft and Rockets,1972, 9(10):764-771. doi: 10.2514/3.30393
    [15] Michael W S,Charles R M.Plume impingement force during tandem stage separation at high altitudes[J].J Spacecraft,1972, 9:715-717. doi: 10.2514/3.61786
    [16] Subramanyam J D A.Separation dynamics analysis for a multistage rocket[A].In: Kobayashi S,Ed.Proceedings of the International Symposium of Space Science and Technology[C]. Tokyo:AGNE Publishing,1973,383-390,
    [17] Kalesnikof K S.Dynamic Separation[M], 1977.(in Russian)
    [18] Saxena S K.Upper stage jet impingement on separated booster[J].Aeronautical Journal,1979,(616):71-74.
    [19] Lochan R, Adimurthy V, Kumar K.Separation dynamics of strap-on boosters[J].Journal of Guidance, Control and Dynamics,1992,15(1):137-143. doi: 10.2514/3.20811
    [20] Lochan R.Dynamics of bodies separating from launch vehicles[D].Ph.D. Dissertation.Kanpur:Department of Aerospace Engineering, Indian Institute of Technology,1993.
    [21] Lochan R,Adimurthy V, Kumar K.Separation dynamics of ullage rockets[J].Journal of Guidance, Control and Dynamics,1994,17(3):426-434. doi: 10.2514/3.21217
    [22] Lochan R,Adimurthy V.Separation dynamics of strap-on boosters in the atmosphere[J].Journal of Guidance, Control and Dynamics, 1997,20(4):633-639. doi: 10.2514/2.4110
    [23] Cheng S C.Payload fairing separation dynamics[J].Journal of Spacecraft and Rockets, 1999,36(4):511-515,1999. doi: 10.2514/3.27193
    [24] Reubush David E, Martin J G.Hyper-x stage separation simulation development and results[A].In:10th International Space Planes and Hypersonic Systems and Technologies Conference[C].Kyoto, Japan, 2001.
    [25] Jeyakumar D,Biswas K K.Design and analysis of the stage separation system of a massive liquid rocket stage[A].In:Proceedings of the International Conference on Modelling Simulation and Optimization for Design of Multidisciplinary Engineering Systems[C].Goa, India, 2003.
    [26] Jeyakumar D,Biswas K K.Stage separation system design and dynamic analysis of ISRO launch vehicles[J].Journal of Aerospace Sciences and Technologies,2003, 55(3):211-222.
    [27] Jeyakumar D,Biswas K K.Stage separation dynamic analysis of upper stage of a multistage launch vehicle using retro rocket[J].Mathematical and Computer Modelling,2005,41(819):849-866. doi: 10.1016/j.mcm.2005.02.001
    [28] Mitchell D H.Flight Separation Mechanism[R]. NASA-SP-8056, 1970.
    [29] Papoulis A.Probability,Random Variables,and Stochastic Processes[M].McGraw-Hill, 1991.
    [30] Logan J W.DSV-3E First-Second stage separation analysis[R]. Rept SM-46446, Douglas Aircraft co., 1965.
    [31] Ball K J,Osborne G F.Space Vehicle Dynamics[M].Oxford:Oxford University Press, 1967,59-61.
    [32] Orlik-Rukemann K J,Iyengar S.Example of dynamic interference effects between two oscillating vehicles[J].Journal of Spacecraft and Rockets, 1973,10(9):617-619. doi: 10.2514/3.61937
    [33] YU Xue.Separation between stages of multistage carrier rocket[R]. FTD-ID (RS) T-1143-83,1983.
    [34] Naftel J C,Wilhite A W,Cruz C I.Analysis of separation of a two-stage winged launch vehicle[A].In:24th AIAA Aerospace Sciences Meeting[C].Reno,NV,Jan,1986.
  • 加载中
计量
  • 文章访问数:  2494
  • HTML全文浏览量:  96
  • PDF下载量:  690
  • 被引次数: 0
出版历程
  • 收稿日期:  2007-06-19
  • 修回日期:  2008-08-07
  • 刊出日期:  2008-11-15

目录

    /

    返回文章
    返回