摘要: This paper examines the use of discontinuous low thrust for orbital transfers between two non-coplanar, circular orbits. The vehicle is assumed to be a solar-powered, ion rocket that cannot operate when it is within the earth's sh... 展开
作者 | Cass, J. R. | ||
---|---|---|---|
原报告号 | ADA136908 | 总页数 | 64 |
报告类别/文献类型 | AD / NTIS科技报告 | ||
关键词 | Electric propulsion Spacecraft Payload Specific impulse Thrusters Circular orbits Shadows Sunlight Thrust Mass flow |