首页> 外文会议>International astronautical congress;IAC 2008 >FEASIBLITY STUDY OF FLIGHT EXPERIMENT FOR ELECTRODYNAMIC HEATSHIELD TECHNOLOGY
【24h】

FEASIBLITY STUDY OF FLIGHT EXPERIMENT FOR ELECTRODYNAMIC HEATSHIELD TECHNOLOGY

机译:电热屏蔽技术飞行实验的可行性研究

获取原文

摘要

The electrodynamic heatshield technique is a promising technique which can replace the current heat-shield system. In addition, the technique can provide us a way to maneuver the vehicle without moving parts. So far, much research has been devoted to this technique. Nevertheless the technology is remained to be verified by a flight experiment which is necessary since the existing ground facility can not provide the flight condition. The feasibility of the flight experiment in a ballistic flight is critically discussed. Especially the super-conducting magnetic filed generator and the measurement system onboard the vehicle are discussed in detail.
机译:电动热屏蔽技术是一种有前途的技术,可以替代当前的热屏蔽系统。另外,该技术可以为我们提供一种无需移动部件即可操纵车辆的方法。迄今为止,已经对该技术进行了大量研究。然而,由于现有地面设施无法提供飞行条件,因此仍有必要通过飞行实验来验证该技术。严格讨论了在弹道飞行中进行飞行实验的可行性。特别地,详细讨论了车辆上的超导磁场发生器和测量系统。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号