Integrated Utility Module for Future NASA Miniature Spacecraft

Venneri, S.L.; Wada, B.K.; Lou, M.C.

dc.contributor.author	Venneri, S.L.	en_US
dc.contributor.author	Wada, B.K.	en_US
dc.contributor.author	Lou, M.C.	en_US
dc.date.accessioned	2004-10-03T06:14:57Z
dc.date.available	2004-10-03T06:14:57Z
dc.date.issued	1995-10	en_US
dc.identifier.citation	Oslo, Norway	en_US
dc.identifier.clearanceno	95-1272	en_US
dc.identifier.uri	http://hdl.handle.net/2014/31695
dc.description.abstract	NASA initiated a program for space-validation of selected technologies relating to miniature spacecraft and microinstruments. Addressed is the proposed development of the Integrated Utility Module (IUM) which integrates structural integrity, thermal management, power distribution, data & signal transmission, radiation & meteoroid protection, etc. into a lightweight, compact, cableless package.	en_US
dc.format.extent	951589 bytes
dc.format.mimetype	application/pdf
dc.language.iso	en_US
dc.subject.other	NASA IUM Microspacecraft Miniaturization Technology	en_US
dc.title	Integrated Utility Module for Future NASA Miniature Spacecraft	en_US