Secure tightening of a CMC fastener for the heat shield of re-entry vehicles

被引:46
|
作者
Boehrk, H. [1 ]
Beyermann, U. [1 ]
机构
[1] DLR, Inst Struct & Design, German Res Ctr, Deutsch Zentrum Luft & Raumfahrt, D-70569 Stuttgart, Germany
关键词
CMC; Ceramic; Fastener; Re-entry; Heat-shield;
D O I
10.1016/j.compstruct.2009.07.002
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The results of static and hot tests of ceramic matrix composite fasteners for heat shield attachment to a re-entry vehicle are presented. Herein, the effect of the high temperature cycle occurring during atmospheric re-entry on the reduction of the tightening torque of the CMC fasteners is investigated. From cold testing, it is found that the Young's modulus of the material decreases with first-time loading and, therefore, previous loading of the fasteners before their application is recommended. In hot testing of a fully integrated fastener connection, the material temperatures within the connection are experimentally simulated. It is shown that with previous straining, a significant improvement of the fastener is achieved. The loosening torque is no longer reduced by thermally induced stretching of the fastener. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:107 / 112
页数:6
相关论文
共 50 条
  • [11] Model surface conductivity effect for the electromagnetic heat shield in re-entry flight
    Matsuda, Atsushi
    Otsu, Hirotaka
    Kawamura, Masaaki
    Konigorski, Detlev
    Takizawa, Yuji
    Abe, Takashi
    PHYSICS OF FLUIDS, 2008, 20 (12)
  • [12] Millimeterwave communications for atmospheric re-entry vehicles
    Christopher, P
    WIRELESS TECHNOLOGIES AND SYSTEMS: MILLIMETER-WAVE AND OPTICAL, 1998, 3232 : 21 - 32
  • [13] MANEUVERING PERFORMANCE OF LIFTING RE-ENTRY VEHICLES
    MANDELL, DS
    ARS JOURNAL, 1962, 32 (03): : 346 - 354
  • [14] THE SEARCH FOR OPTIMUM CONFIGURATIONS FOR RE-ENTRY VEHICLES
    LIN, TC
    GRABOWSKY, WR
    YELMGREN, KE
    JOURNAL OF SPACECRAFT AND ROCKETS, 1984, 21 (02) : 142 - 149
  • [15] Optimal trajectories for maneuvering re-entry vehicles
    Undurti, Aditya
    Proulx, Ronald J.
    Shearer, James A.
    Setturlund, Roy H.
    ASTRODYNAMICS 2007, PTS I-III, 2008, 129 : 879 - +
  • [16] Re-entry trajectory design of inflatable thermal shield
    Xia, Gang
    Cheng, Wen-Ke
    Qin, Zi-Zeng
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2002, 24 (03):
  • [17] Aerodynamics and Aerothermodynamics of undulated re-entry vehicles
    Kaushikh, K.
    Arunvinthan, S.
    Pillai, S. Nadaraja
    ACTA ASTRONAUTICA, 2018, 142 : 95 - 102
  • [18] Development of a new cost-effective ceramic composite for re-entry heat shield applications
    Muhlratzer, A
    Handrick, K
    Pfeiffer, H
    ACTA ASTRONAUTICA, 1998, 42 (09) : 533 - 540
  • [19] Drag and Heat Flux Reduction on Hypersonic Re-entry Vehicles in Combination with Different Aerospikes
    Mudaliar, Karan Ravi
    Gomes, Malcolm Cajetan
    Chareesh, M.V.
    Thakur, Amritapkumar
    Gowrishankar
    Dineshkumar, G.
    Vishnukumar, G.C.
    International Journal of Vehicle Structures and Systems, 2022, 14 (01) : 110 - 115
  • [20] An optimal heat-flux targeting procedure for LEO re-entry of reusable vehicles
    Aprovitola, Andrea
    Montella, Nicolina
    Iuspa, Luigi
    Pezzella, Giuseppe
    Viviani, Antonio
    AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 112