Abstract:
The Satellite Launch Vehicle electrical network, which is currently being developed in Brazil, is sub-divided for analysis in the following parts: Service Electrical Network, Controlling Electrical Network, Safety Electrical Network and Telemetry Electrical Network. During the pre-launching and launching phases, these electrical networks are associated electrically and mechanically to the structure of the vehicle. In order to succeed in the integration of these electrical networks it is necessary to employ techniques of electrical power distribution, which are proper to Launch Vehicle systems. This work presents the most important techniques to be considered in the characterization of the electrical power supply applied to Launch Vehicle systems. Such techniques are primarily designed to allow the electrical networks, when submitted to the single-phase fault to ground, to be able of keeping the power supply to the loads.
Keywords:
SLV; Electrical network; Power distribution
Full text is available only in PDF.
REFERENCES
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- Kindermann, G., 1992, "Curto-circuito", Sagra/DC Luzzatto, Porto Alegre.
- Mulville, D.R., 1998, "Electrical grounding architecture for unmanned spacecraft: Nasa technical handbook", Nasa, Washington.
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Publication Dates
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Publication in this collection
Sep-Dec 2010
History
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Received
25 Aug 2010 -
Accepted
08 Sept 2010
