相关文档

《航天推进 Space Propulsion》(英文版)Lecture 2: Mission Analysis for Low Thrust

1. Constant Power and Thrust: Prescribed Mission Time Starting with a mass M0 , and operating for a time t an electric thruster of jet speed c, such as to accomplish an equivalent (force-free) velocity change of ∆V , the final
团购合买资源类别:文库,文档格式:PDF,文档页数:19,文件大小:474.78KB
点击进入文档下载页(PDF格式)
共19页,试读已结束,阅读完整版请下载
点击下载(PDF格式)