| タイトル | Places Only Sails Can Go |
| 本文（外部サイト） | http://hdl.handle.net/2060/20030065927 |
| 著者（英） | Garbe, Gregory P.; Montgomery, Edward E., IV; Heaton, Andrew F. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2003-04-01 |
| 言語 | eng |
| 内容記述 | Solar sails are a near term, low thrust, propellantless propulsion technology suitable for orbital maneuvering, station keeping, and attitude control applications for small payloads. Furthermore, these functions can be highly integrated, reducing mass, cost and complexity. The solar sail concept is based on momentum exchange with solar flux reflected from a large, deployed thin membrane. Thrust performance increases as the square of the distance to the sun. In comparison to conventional chemical systems, there are missions where solar sails are vastly more and less economical. The less attractive applications involve large payloads, outer solar system transfers, and short trip times. However, for inclination changes and station keeping at locations requiring constant thrust, the solar sail is the only economical option for missions of more than a few weeks duration. We compare the location and energies required for these applications between solar sails, advanced electric propulsion, and conventional rockets. We address the effect on mass fraction to understand solar sail mission cost and capability. Finally, the benefit of potential applications to near term science missions is reported. |
| NASA分類 | Spacecraft Propulsion and Power |
| 権利 | No Copyright |
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