Advanced Search
Volume 42 Issue 8
Aug.  2016
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(8): 1612-1618.
HAO Feng, CHANG Min, TANG Shuoet al. Comparative analysis on primary parameters of loitering munitions of different propulsion systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1612-1618. doi: 10.13700/j.bh.1001-5965.2015.0490(in Chinese)
Citation: HAO Feng, CHANG Min, TANG Shuoet al. Comparative analysis on primary parameters of loitering munitions of different propulsion systems[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(8): 1612-1618. doi: 10.13700/j.bh.1001-5965.2015.0490(in Chinese)
shu

Comparative analysis on primary parameters of loitering munitions of different propulsion systems

doi: 10.13700/j.bh.1001-5965.2015.0490
  • 1.

    School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China

  • 2. Xi'an Modern Control Technology Research Institute, Xi'an 710065, China

  • Received Date: 20 Jul 2015
  • Publish Date: 20 Aug 2016
    Abstract
  • As to loitering munitions, the propulsion system significantly influences design missions of flight endurance, cruising velocity, range and the mass of payloads. Based on the constraint of energy balance, the estimation formulation of loitering munitions of three types of propulsion systems is established, including electric-motor type, piston type and jet type. Then the influences of performance parameters on design missions for different types of propulsion systems are analyzed comparatively and individually by the sensitivity analysis method. The characteristics of equivalentenergy density for each kind of fuel material of three propulsion system types are compared from the perspective of energy supply to conclude the original reasons for those three types. These conclusions could provide useful guidelines for selection of propulsion systems for different military operations in the phase of preliminary design of loitering munitions.

     

    • FullText(HTML)
  • loading
    • References(15)
  • [1]
    AKRAM G.Loitering munitions:Revolutionizing indirect fire support[J].RUSI Defence Systems, 2008(2):36-38.
    [2]
    郭美芳,范宁军,袁志华.巡飞弹战场运用策略[J].兵工学报,2006,27(5):944-947.GUO M F,FAN N J,YUAN Z H.Battlefield operational strategy of loitering munition[J].Acta Armamentarii,2006,27(5):944-947(in Chinese).
    [3]
    庞艳珂,韩磊,张民权,等.攻击型巡飞弹技术现状及发展趋势[J].兵工学报,2010,31(增刊2):149-152.PANG Y K,HAN L,ZHANG M Q,et al.Status and development trends of loitering attack missiles[J].Acta Armamentarii,2010,31(Suppl.2):149-152(in Chinese).
    [4]
    彭翠枝,郭美芳,樊琳,等.巡飞弹用动力装置与技术发展初探[J].飞航导弹,2011(10):84-88.PENG C Z,GUO M F,FAN L,et al.Preliminary exploration on dvelopment of propulsion systems of loitering munitions[J].Cruising Missiles,2011(10):84-88(in Chinese).
    [5]
    秦楠,马亮,秦庚申."弹簧折刀"新型潜射无人机的出现与启示[J].舰船电子工程,2013,33(11):11-13.QIN N,MA L,QIN G S.Emergence of new submarine-launched UAV switchblade and its revelations[J].Ship Electronic Engineering,2013,33(11):11-13(in Chinese).
    [6]
    FOSS C F.R-90 thrusts smerch into reconnaissance[J].Jane's Defence Weekly,1997(1):15.
    [7]
    ZUGEL K.Loiter attack munition flight test program:AIAA-2003-6644[R].Reston:AIAA,2003.
    [8]
    RAYMER D P.Aircraft design:A conceptual approach[M].Reston:AIAA,1999:11-100.
    [9]
    刘斌,马晓平,王和平,等.小型电动无人机总体参数设计方法研究[J].西北工业大学学报,2005,23(3):396-400.LIU B,MA X P,WANG H P,et al.Design analysis methodology for electric-powered mini-UAV[J].Journal of Northwestern Ploytechnical University,2005,23(3):396-400(in Chinese).
    [10]
    康桂文,胡雨,李亚东,等.超轻型电动飞机电动力系统的参数匹配[J].航空动力学报,2013,28(12):2641-2647.KANG G W,HU Y,LI Y D,et al.Parameters matching of ultra-light electric aircraft propulsion system[J].Journal of Aerospace Power,2013,28(12):2641-2647(in Chinese).
    [11]
    NOTH A.Design of solar powered airplanes for continuous flight[D].Zurich:Swiss Federal Institute of Technology,2008:17-66.
    [12]
    刘沛清.空气螺旋桨理论及其应用[M].北京:北京航空航天大学出版社,2006:56-59.LIU P Q.Theory and application of aerodynamic propeller[M].Beijing:Beihang University Press,2006:56-59(in Chinese).
    [13]
    赵阳旭,陈伟博,刘晓凌,等.航空活塞发动机高空台试验性能分析[J].航空工程进展,2013,4(3):364-368.ZHAO Y X,CHEN W B,LIU X L,et al.Altitude simulation test analysis for a piston aero-engine[J].Advanced in Aeronautical Science and Engineering,2013,4(3):364-368(in Chinese).
    [14]
    《世界无人机大全》编写组.世界无人机大全[M].北京:航空工业出版社,2004:1-116.Write Group of the World's UAVs.The world's UAVs[M].Beijing:Aviation Industry Press,2004:1-116(in Chinese).
    [15]
    谭汉清.国外微型涡喷发动机应用现状及未来发展趋势[J].飞航导弹,2013(3):76-80.TAN H Q.Application situation and developing trends of foreign micro jet[J].Cruising Missiles,2013(3):76-80(in Chinese).
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(1745) PDF downloads(1106) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return