首页 /研究 /Deployable Optics for Future Space Observatories
OTHER

Deployable Optics for Future Space Observatories

Charles F. Lillie, William Whiddon

发表年份
2004
引用次数
5

摘要

Nomenclature JWST = James Webb Space Telescope RSF = Robotic space flight TPF = Terrestrial Planet Finder PMS = Probability of mission success ELV = Expendable launch vehicle Si = Cost savings for the ith item Mechanisms = Joints providing deployment capability Ci = Cost increase for the ith item HARD = High Accuracy Reflector Development ORU = orbital replacement unit RTJ = Rotational translational joint Pi = Conditional probability of success for the ith term PSI = Pounds per square inch Ni = Number of interfaces in a system RF = Radio frequency Ns = Number of segments in a primary mirror CTE = Coefficient of thermal expansion D = Aperture of the primary mirror, or objective OTA = Optical telescope assembly d = Maximum clear aperture of a mirror segment OHP = Octagonal hub pancake EVA = extravehicular activity HSF = Human space flight PLOC = Probable loss of crew (injury or fatality of one or more members) LEO = Low Earth orbit CG = Center of gravity

关键词

Space (punctuation)Computer scienceRemote sensingComputer graphics (images)GeologyOperating system

相关论文

查看 OTHER 分类全部论文