Galileo System Design for Orbital Operations

George, J.; Kunstmann, G.; Southard, S.; Upchurch, E.

dc.contributor.author	George, J.	en_US
dc.contributor.author	Kunstmann, G.	en_US
dc.contributor.author	Southard, S.	en_US
dc.contributor.author	Upchurch, E.	en_US
dc.date.accessioned	2004-10-05T21:13:31Z
dc.date.available	2004-10-05T21:13:31Z
dc.date.issued	1994-10-31	en_US
dc.identifier.citation	IEEE/AIAA, 13th Digital Avionics Systems Conference	en_US
dc.identifier.citation	Phoenix, Arizona, USA	en_US
dc.identifier.clearanceno	94-0435	en_US
dc.identifier.uri	http://hdl.handle.net/2014/33708
dc.description.abstract	In April 1991, Galileo's X-band high gain antenna failed to deploy. An alternate approach which utilizes the spacecraft's S-band low gain antenna was conceived and is in development.	en_US
dc.format.extent	132158 bytes
dc.format.mimetype	application/pdf
dc.language.iso	en_US
dc.subject.other	Galileo high gain antenna X-/S-band data dependent compression	en_US
dc.title	Galileo System Design for Orbital Operations	en_US