作者: E Luther , S Okumura
DOI:
关键词: Effective diameter 、 Photovoltaic system 、 Optics 、 Surface (mathematics) 、 Engineering 、 Spacecraft
摘要: A deployable spacecraft solar array having an annular thin-film panel circumferentially surrounding a body and supported on the by hinged frames which are swingable inwardly to retracted positions against contract launch configuration with effective diameter approximating outwardly radial extended expand deployed substantially greater than hence surface area exceeding area.