Geoscientific Instrumentation, Methods and Data Systems | |
Electric solar wind sail mass budget model | |
A. A.Quarta1  P.Janhunen1  G.Mengali1  | |
DOI : 10.5194/gi-2-85-2013 | |
学科分类:天文学(综合) | |
来源: Copernicus Publications | |
【 摘 要 】
The electric solar wind sail (E-sail) is a new type of propellantlesspropulsion system for Solar System transportation, which uses the naturalsolar wind to produce spacecraft propulsion. The E-sail consistsof thin centrifugally stretched tethers that are kept charged by an onboardelectron gun and, as such, experience Coulomb drag through the high-speedsolar wind plasma stream. This paper discusses a mass breakdown and aperformance model for an E-sail spacecraft that hosts amission-specific payload of prescribed mass. In particular, themodel is able to estimate the total spacecraft mass and its propulsiveacceleration as a function of various design parameters such as thenumber of tethers and their length. A number of subsystem masses arecalculated assuming existing or near-term E-sail technology. In light of theobtained performance estimates, an E-sail represents a promising propulsionsystem for a variety of transportation needs in the Solar System.
【 授权许可】
Unknown
【 预 览 】
Files | Size | Format | View |
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RO201912130860163ZK.pdf | 884KB | download |