期刊文献+

轨道试验飞行器X-37B再入飞行关键技术 被引量:2

原文传递
导出
摘要 首先阐述了X-37B研制历程,然后展示了X-37B气动外形、控制布局和部分子系统。作为再入飞行的关键技术,重点分析了X-37B的防热技术、推进技术以及导航、制导与控制技术,最后简要给出了X-37B成功的三个因素。
出处 《飞航导弹》 北大核心 2012年第11期38-43,共6页 AERODYNAMIC MISSILE JOURNAL
  • 相关文献

参考文献19

  • 1Boeing, X-37B Orbital Test Vehi- cle Overview. http://www, boe- ing. corn/defence-space/ic/sis/ x37b_otv/x37b_otv, html, 2011- 06.
  • 2Jameson A D. X-37 Space Vehicle: Starting a New Age in Space Con- trol. Air Command and Staff Col- lege, Air University, April 2001: 1-29.
  • 3Stephen Cook, Daniel Dumbacher. NASA Integrated Space Transpor- tation Plan. Acta Astronautica, 2001, 48(5-12) : 869-883.
  • 4Kip Mikula D F, Holthaus M, Jensen T, et al. X-37 Flight Demonstrator system safety pro- gram and challenges. AIAA Space 2000 Conference and Exposition, Long Beach, California, 19-21 September 2000 : 1-11.
  • 5Paez C A. The development of the X-37 re-entry vehicle 40th AIAA/ ASME/SAE/ASEE Joint Propul- sion Conference and Exhibit, Fort Lauderdale, Florida, 11-14 July 2004 : 1-10.
  • 6许红英,侯丹,陈杰,屠空.美空军发射X-37B飞行器简析[J].中国航天,2010(6):21-25. 被引量:15
  • 7Turner S. Learning Lessons from the X-37 Project AIAA: Continu- ing the Voyage of Discovery, Jan- uary 30 - February 1, 2005 : 1-2.
  • 8陈婧.美军X-37B挑战宇宙安全[J].中国民兵,2010(5):58-59. 被引量:3
  • 9Chaudhary A, Nguyen V, Iran H, et al. Dynamics and Stability and Control Characteristics of the X-37. AIAA Guidance, Naviga- tion, and control Conference and Exhibit, Montreal, Canada, 6-9 August 2001 : 1-10.
  • 10Jacobson D. X-37 Flight Demon- strator: orbital vehicle technolo- gy development approach NASA Marshall Space Flight Center, February 11, 2004:1-18.

共引文献15

同被引文献19

引证文献2

二级引证文献7

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部