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Cuernorejado, CAutor (correspondencia)Lopezdiez, JAutor o CoautorSanzandres, AAutor o CoautorRAPID METHOD FOR SPACECRAFT SIZING
Publicado en:Proceedings Of The Institution Of Mechanical Engineers Part G-Journal Of Aerospace Engineering. 209 (3): 165-169 - 1995-01-01 209(3), DOI: 10.1243/PIME_PROC_1995_209_286_02
Autores: CUERNOREJADO, C; LOPEZDIEZ, J; SANZANDRES, A;
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Resumen
In this paper, a rapid method for spacecraft sizing is presented. This method is useful in both the conceptual and preliminary design phases of scientific and communication satellites. The aim of this method is to provide a sizing procedure similar to the ones used in the design of aircraft; actually by determining the mass of all the spacecraft subsystems. In the Introduction, the importance of an accurate initial mass budget in the design of satellites is emphasized. Literature about this topic is not very extensive and most of the existing methods have been recapitulated. The methodology followed in the proposed procedure for spacecraft mass sizing is based on these methods. Data from 26 existing satellites have been considered to obtain correlations between each subsystem mass and the mass of the whole spacecraft.
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2025-07-20:
- WoS: 1
- Scopus: 1
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Análisis de liderazgo de los autores institucionales
Existe un liderazgo significativo ya que algunos de los autores pertenecientes a la institución aparecen como primer o último firmante, se puede apreciar en el detalle: Primer Autor (CUERNO REJADO, CRISTINA) y Último Autor (SANZ ANDRES, ANGEL PEDRO).
el autor responsable de establecer las labores de correspondencia ha sido CUERNO REJADO, CRISTINA.