Nanosat power system planning and analysis

碩士 === 國立中央大學 === 機械工程研究所 === 90 === The goal of this thesis is design a power system to fit the Nanosat use to reach the mission requirement. The weight of Nanosat is 10 kilograms, sun-synchronous circular orbit, orbit altitude is 800 km, orbit inclination is 98.6 degree, orbit period is 101 minut...

Full description

Bibliographic Details
Main Authors: Chi-Hao Hsieh, 謝其浩
Other Authors: none
Format: Others
Language:zh-TW
Published: 2002
Online Access:http://ndltd.ncl.edu.tw/handle/50272426659053957996