Rapid sizing tool for a low cost university microsatellite structure subsystem

Ravanbakhsh, Alí y Franchini, Sebastian Nicolas (2011). Rapid sizing tool for a low cost university microsatellite structure subsystem. En: "5th International Conference on Recent Advances in Space Technologies (RAST), 2011", 09/06/2011 - 11/06/2011, Estambul, Turquia. ISBN 978-1-4244-9616-7.

Descripción

Título: Rapid sizing tool for a low cost university microsatellite structure subsystem
Autor/es:
  • Ravanbakhsh, Alí
  • Franchini, Sebastian Nicolas
Tipo de Documento: Ponencia en Congreso o Jornada (Artículo)
Título del Evento: 5th International Conference on Recent Advances in Space Technologies (RAST), 2011
Fechas del Evento: 09/06/2011 - 11/06/2011
Lugar del Evento: Estambul, Turquia
Título del Libro: Proceedings of 5th International Conference on Recent Advances in Space Technologies (RAST), 2011
Fecha: 2011
ISBN: 978-1-4244-9616-7
Materias:
Escuela: E.U.I.T. Aeronáutica (UPM) [antigua denominación]
Departamento: Tecnologías Especiales Aplicadas a la Aeronáutica [hasta 2014]
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

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Resumen

In recent decays university class small satellites are creating many opportunities for space research and professional trainings while at the same time responding to constrained budgets. In this work the main focus is on developing a simple and rapid structural sizing tool considering the main objectives of a low cost university class microsatellite project. In satellite projects, structure subsystem is one of the influential subsystems as a driver of the cost and acceptance of the final design. At the first steps of such projects there is no confirmed data regarding the launch vehicle or even in some cases there is no data for the satellite payload. Due to these facts, developing simple sizing tools at conceptual design phase for obtaining an over view of the effect of different variables is useful before entering complex calculations in detailed design phases. In this study, after developing a simple analytical model of satellite structure subsystem, a design space is evaluated with practical boundaries considering mass and dimensions constraints of such projects. The results are useful to give initial insight to establish the system level structural sizing

Más información

ID de Registro: 12635
Identificador DC: http://oa.upm.es/12635/
Identificador OAI: oai:oa.upm.es:12635
URL Oficial: http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=5966943&tag=1
Depositado por: Memoria Investigacion
Depositado el: 06 Ago 2012 07:56
Ultima Modificación: 21 Abr 2016 11:54
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