Effect of configuration and orbital position on spacecraft charging predictions using ATS-6 maximum sunlight charging environment and theGEOCAT engineering analysis tool
2008 ◽
Vol 36
(5)
◽
pp. 2350-2359
◽
2008 ◽
Vol 36
(5)
◽
pp. 2336-2349
◽
2009 ◽
Vol 64
(5-6)
◽
pp. 495-500
◽