Design and simulation of hydraulic system for launch vehicle holding device

被引:0
|
作者
Kim, Dae Rae [1 ]
Yang, Seong Pil [1 ]
Lee, Jaejun [2 ]
Kim, Bum Suk [2 ]
Lee, Young-Shin [3 ]
机构
[1] Korea Aerosp Res Inst, Daejeon, South Korea
[2] Hyundai Heavy Ind, Ulsan, South Korea
[3] Chungnam Natl Univ, Daejeon, South Korea
关键词
Vehicle Holding Device; Launch Vehicle Lift-off; Ka Doing a Doing a Doing Mode; Hydraulic Cylinder Velocity; Amesim;
D O I
10.5139/JKSAS.2016.44.12.1087
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The responsibility of the vehicle holding device (VHD) is to hold the launch vehicle while it is stayed on launch pad and release the holding mechanism to allow a lift-off of launch vehicle at a moment of lift-off. During a release of the holding mechanism, in order to prevent the Ka doing a doing a doing mode which is vertical oscillation of entire liquid propellant and very severe for vehicle structure, gradual release of holding force is required. Also, a release operation of all 4 VHD should be synchronized very precisely. In this study, to comply the "gradual release and synchronized operation requirement", concept of VHD hydraulic system using an accumulator, pyro valve and orifice to control speed of hydraulic cylinder is proposed instead of using complicated hydraulic components. Then through multi-body dynamic analysis and computational hydraulic analysis, a size of orifice to meet a target speed of hydraulic cylinder is calculated. Through this study, simple and reliable VHD hydraulic system complying requirements is designed.
引用
收藏
页码:1087 / 1094
页数:8
相关论文
共 50 条
  • [41] THE IMPLEMENTATION OF MAXIMUM LIKELIHOOD ESTIMATION IN SPACE LAUNCH SYSTEM VEHICLE DESIGN
    Stein, W. B.
    Thompson, S. B.
    Statham, T. L.
    Craig, A. S.
    SPACEFLIGHT MECHANICS 2019, VOL 168, PTS I-IV, 2019, 168 : 265 - 280
  • [42] Control Allocation Design of Reaction Control System for Reusable Launch Vehicle
    Mu, Rongjun
    Zhang, Xin
    ABSTRACT AND APPLIED ANALYSIS, 2014,
  • [43] Hydraulic system design and simulation of the forging manipulator
    The State Key Lab of Fluid Power Transmission and Control, Zhejiang University, Hangzhou 310027, China
    Jixie Gongcheng Xuebao, 11 (49-54):
  • [44] An Open Integrated Electronic System Software Architecture Design for Launch Vehicle
    Zhang, Feng
    Yao, Guo-wei
    Wang, Qian
    Xia, Yun
    COMMUNICATIONS, SIGNAL PROCESSING, AND SYSTEMS, CSPS 2018, VOL III: SYSTEMS, 2020, 517 : 673 - 682
  • [45] Design optimisation of a hydraulic clamping system by simulation
    Pinet, PJ
    Martin, HR
    PROCEEDINGS OF THE 47TH NATIONAL CONFERENCE ON FLUID POWER, VOL II, 1996, : 105 - 120
  • [46] Design Research on Hydraulic System of Working Device of a Forklift
    Pan, Liai
    Du, Qiulei
    He, Chunshan
    PROCEEDINGS OF THE 5TH INTERNATIONAL CONFERENCE ON ADVANCED DESIGN AND MANUFACTURING ENGINEERING, 2015, 39 : 1813 - 1817
  • [47] Design of Low-Cost Simulation Space Micro Debris Launch Device
    Yang, Renjie
    Tang, Kai
    Lang, Xuqiang
    He, Cheng
    Liu, Yu
    Liu, Yue
    AEROSPACE, 2024, 11 (07)
  • [48] Collaborative approach to launch vehicle design
    NASA Langley Research Cent, Hampton, United States
    J Spacecr Rockets, 4 (478-486):
  • [49] Collaborative approach to launch vehicle design
    Braun, RD
    Moore, AA
    Kroo, IM
    JOURNAL OF SPACECRAFT AND ROCKETS, 1997, 34 (04) : 478 - 486
  • [50] On the design of adaptive autopilots for a launch vehicle
    Roshanian, J.
    Saleh, A. R.
    Jahed-Motlagh, M. R.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2007, 221 (I1) : 27 - 38