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

FEASIBLITY STUDY OF FLIGHT EXPERIMENT FOR ELECTRODYNAMIC HEATSHIELD TECHNOLOGY

机译:电动散热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:电动热屏幕技术是一种有希望的技术,可以代替当前的隔热系统。此外,该技术可以为我们提供一种在没有移动部件的情况下操纵车辆的方法。到目前为止,这种技术已经致力于许多研究。然而,由于现有地面设施无法提供飞行条件,因此仍然需要通过飞行实验进行验证。批判性地讨论了弹道飞行中飞行试验的可行性。特别是,详细讨论了车辆上的超导磁性发电机和测量系统。

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