Workshop on Design Approaches and Development Philosophiesof Small Satellites

dc.contributor.corpauthor	Kenya Agriculture Research Institute
dc.contributor.institution	Technical University of Berlin
dc.date.accessioned	2015-08-12T09:57:36Z
dc.date.available	2015-08-12T09:57:36Z
dc.date.issued	1992	en
dc.description.abstract	fhe primary structure (Fig. 2) consists of a fraRle of aluminium profiles of 38 x 38 x 38 cm dimensions and weighs less than 3 kg. Electrical power is provided by 10 Ni Cd batteries (SAFr, Vo 7 s) supporting a regulated 12 V bus to the satellite and to the payload. The batteries are sandwiched between two 5 mm thick aluminium plates to assure high thermal capacity of the battery block and low thermal gradients between individual cells.	en
dc.format.pages	16	en
dc.identifier.citation	Kenya Soil Survey. (1992). Workshop on Design Approaches and Development Philosophiesof Small Satellites
dc.identifier.uri	http://kalroerepository.kalro.org/handle/0/9271
dc.language.iso	en	en
dc.publisher	Kenya Agriculture Research Institute	en
dc.publisher.place	Nairobi	en
dc.rights.uri	http://creativecommons.org/licenses/by/3.0/	en
dc.subject.agrovoc	Workshops	en
dc.subject.agrovoc	Power	en
dc.subject.agrovoc	Cells	en
dc.subject.agrovoc	alluminium	en
dc.title	Workshop on Design Approaches and Development Philosophiesof Small Satellites	en
dc.type	Book	*
dc.type.refereed	Refereed	en
dc.type.specified	Article	en

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