TECHNIQUE APPLIED IN ELECTRICAL POWER DISTRIBUTION FOR SATELLITE LAUNCH VEHICLE DOI 10.5028/jatm.2010.02038410

Authors

  • Francisco Carlos P. Bizarria Institute of Aeronautics and Space São José dos Campos, Brazil
  • José Walter Parquet Bizarria University of Taubaté Taubaté, Brazil
  • Fábio Duarte Spina Institute of Aeronautics and Space São José dos Campos, Brazil
  • João Maurício Rosário University of Campinas Campinas, Brazil

Keywords:

SLV, Electrical network, Power distribution.

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.

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Published

2011-07-29

Issue

Vol. 2 No. 3 (2010): Sep./Dec. 2010

Section

Original Papers

License

This work is licensed under a Creative Commons — Attribution 4.0 International — CC BY 4.0. Authors are free to Share (copy and redistribute the material in any medium or format) and Adapt (remix, transform, and build upon the material for any purpose, even commercially). JATM allow the authors to retain publishing rights without restrictions.