Modeling and Validation of Thermal Radiation Acceleration on Interplanetary Spacecraft

著录项

• 来源
  《Journal of Spacecraft and Rockets》 |2012年第2期|p.212-219|共8页
• 作者

  Michael A. Shoemaker; Jozef C. van der Ha; Trevor Morley;

  展开▼
• 作者单位

  Kyushu University, Fukuoka 819-0395, Japan Department of Aeronautics and Astronautics, West Zone Building 4, 744 Motooka Nishi-ku. Senior Member AIAA.;

  Mission Design and Operations, Deming, Washington, 98244 Consultant, 5808 Bell Creek Road. Senior Member AIAA.;

  European Space Agency, 64293 Darmstadt, Germany Senior Flight Dynamics Specialist, European Space Operations Centre, Robert-Bosch Strasse 5.;

  展开▼
• 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  A: surface area; m~2; A_(Al): ratio of aluminum and honeycomb densities; a: acceleration vector; m/s~2; a_‖: component of a_(obs) parallel to s; m/s~2; a_⊥: component of a_(obs) normal to s; m/s~2 et al;

  机译：A：表面积;m〜2;A_（Al）：铝与蜂窝密度之比;a：加速度矢量;m / s〜2;a_”：平行于s的a_（obs）的分量;m / s〜2;a_⊥：a_（obs）垂直于s的分量;m / s〜2等;