DESIGN CONCEPT AND MODELING OF AN ADVANCED SOLAR PHOTON THRUSTER

被引：0

作者：

Dachwald, Bernd ^{[1
]}

Wurm, Patrick ^{[2
]}

机构：

[1] FH Aachen Univ Appl Sci, Dept Aerosp Technol, Hohenstaufenallee 6, D-52064 Aachen, Germany

[2] Rhein Westfal TH Aachen, Inst Aeronaut & Astronaut, D-52062 Aachen, Germany

来源：

SPACEFLIGHT MECHANICS 2009, VOL 134, PTS I-III | 2009年 / 134卷

关键词：

EVOLUTIONARY NEUROCONTROL; OPTICAL-PROPERTIES; SAIL; TRAJECTORIES; OPTIMIZATION; PERFORMANCE; SPACECRAFT; DEFLECTION; SAILCRAFT; MISSIONS;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The so-called "compound solar sail", also known as "Solar Photon Thruster" (SPT), holds the potential of providing significant performance advantages over the flat solar sail. Previous SPT design concepts, however, do not consider shadowing effects and multiple reflections of highly concentrated solar radiation that would inevitably destroy the gossamer sail film. In this paper, we propose a novel advanced SPT (ASPT) design concept that does not suffer from these oversimplifications. We present the equations that describe the thrust force acting on such a sail system and compare its performance with respect to the conventional flat solar sail.

引用

页码：723 / +

页数：2

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