首页> 外文会议>AIAA Astrodynamics Specialist Conference >Trajectory Design of Solar Probe+ Using Multiple VenusGravity Assists
【24h】

Trajectory Design of Solar Probe+ Using Multiple VenusGravity Assists

机译:太阳能探头+使用多个venusgravity助攻的轨迹设计

获取原文

摘要

A new trajectory for the Solar Probe+ mission is developed, which uses seven unpowered Venus gravity assist flybys to reach the Sun with repeated near-Sun passes in 6 years, at a closest approach distance of 8.5 solar radii (R_S) from the Sun's surface. The trajectory consists of 24 solar passes whose perihelion gradually decreases from 35 R_S down to 9.5 R_S, enabling thorough, timely, direct in situ measurements of the inner heliosphere region during 3 to 4 solar passes per year over more than half of the solar cycle. As the top mission enabler, the trajectory design introduced a new mission concept for the long-studied Solar Probe mission and made it possible for Solar Probe to move on to NASA's mission plan for anticipated launch in 2015.
机译:开发了一个新的太阳能探头+任务的轨迹,它使用七个无力的金星重力助攻氟比斯在6年内重复近天过渡,以8.5太阳线(R_S)的最近的距离。轨迹由24个太阳能通过,其透过率从35 r_s逐渐减少到9.5 r_s,使其能够彻底,及时,直接直接在每年在太阳循环中超过一半的太阳能期间的内部光际区域的原位测量。作为顶级任务推动者,轨迹设计为长期学习的太阳能探针使命推出了新的任务概念,使太阳能探头能够在2015年预期推出的美国国家航空航天局的任务计划。

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