X-34 test curtailed by panel vibrations

被引：0
|
作者：
Smith, BA
机构：
来源：
AVIATION WEEK & SPACE TECHNOLOGY | 1999年 / 151卷 / 01期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：28 / 29
页数：2
相关论文
共 50 条
  • [31] X-34 in virtual shutdown as OSC ponders pullout
    不详
    AVIATION WEEK & SPACE TECHNOLOGY, 1996, 144 (06): : 86 - 86
  • [32] X-34 experimental aeroheating at Mach 6 and 10
    Berry, SA
    Horvath, TJ
    DiFulvio, M
    Glass, C
    Merski, NR
    JOURNAL OF SPACECRAFT AND ROCKETS, 1999, 36 (02) : 171 - 178
  • [33] X-34 experimental aeroheating at Mach 6 and 10
    Berry, Scott A.
    Horvath, Thomas J.
    DiFulvio, Michael
    Glass, Christopher
    Merski, N. Ronald
    Journal of Spacecraft and Rockets, 36 (02): : 171 - 178
  • [34] NASA SPEEDS SELECTION OF X-33, X-34 PLANS
    SMITH, BA
    ASKER, JR
    AVIATION WEEK & SPACE TECHNOLOGY, 1995, 142 (11): : 107 - 109
  • [35] 美取消X-33和X-34计划
    中国航天, 2001, (04) : 24 - 24
  • [36] Temperature-dependent modal test/analysis correlation of X-34 FASTRAC composite rocket nozzle
    Brown, AM
    COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 5, 2000, : 410 - 416
  • [37] Heating analysis of the nosecap and leading edges of the X-34 vehicle
    Palmer, G
    Polsky, S
    JOURNAL OF SPACECRAFT AND ROCKETS, 1999, 36 (02) : 199 - 205
  • [38] X-34 auto-landing guidance, navigation and control
    Ruth, M
    Fernandez, J
    Tracy, C
    GUIDANCE AND CONTROL 2001, 2001, 107 : 171 - 192
  • [39] New methodologies for assessing the robustness of the X-34 autolanding trajectories
    Barton, GH
    GUIDANCE AND CONTROL 2001, 2001, 107 : 193 - 214
  • [40] Temperature-dependent modal test/analysis correlation of X-34 FASTRAC composite rocket nozzle
    Brown, AM
    JOURNAL OF PROPULSION AND POWER, 2002, 18 (02) : 284 - 288
12345