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The Effects of Using Solar Radiation Pressure to Alleviate Fuel Requirements for Orbit Changing and Maintenance of the Dscs II F-13 Satellite - Tapa blanda

Paris, Jody A.

 
9781249595779: The Effects of Using Solar Radiation Pressure to Alleviate Fuel Requirements for Orbit Changing and Maintenance of the Dscs II F-13 Satellite
Tapa blanda
ISBN 10: 1249595770 ISBN 13: 9781249595779
Editorial: BiblioScholar, 2012

Sinopsis

Orbit disposal and maintenance of aging satellites has become a significant concern over the past few years, as the increasing number of orbiting objects in high-value orbits (e.g. geosynchronous) threatens to limit the launching of future satellites and spacecraft. Many of the satellites currently in orbit, however, were not built with disposal considerations. The DSCS II series, for example, was launched into orbit beginning in the 1970s, and many satellites are now without the fuel required to conventionally transition to a sanctioned disposal orbit. In geosynchronous orbit, however, the largest non-gravitational perturbation is solar radiation pressure (SRP). By adjusting the position of the satellite with a controller to maximize the perturbing acceleration due to the force of SRP, the satellite can be slowly raised into an appropriate disposal orbit. The results from this study, along with validation results propagated with Satellite Tool Kit, are presented. After making several simplifying assumptions (primarily a cylindrical Earth shadow, flat plate geometry, and constant cross-sectional area of the satellite), the time required to raise the modelled DSCS II F-13 satellite 400 km into a disposal orbit is approximately 33 years. This time-to-disposal can be reduced by using a larger area-to-mass ratio and more reflective surface materials.

"Sinopsis" puede pertenecer a otra edición de este libro.

Reseña del editor

Orbit disposal and maintenance of aging satellites has become a significant concern over the past few years, as the increasing number of orbiting objects in high-value orbits (e.g. geosynchronous) threatens to limit the launching of future satellites and spacecraft. Many of the satellites currently in orbit, however, were not built with disposal considerations. The DSCS II series, for example, was launched into orbit beginning in the 1970s, and many satellites are now without the fuel required to conventionally transition to a sanctioned disposal orbit. In geosynchronous orbit, however, the largest non-gravitational perturbation is solar radiation pressure (SRP). By adjusting the position of the satellite with a controller to maximize the perturbing acceleration due to the force of SRP, the satellite can be slowly raised into an appropriate disposal orbit. The results from this study, along with validation results propagated with Satellite Tool Kit, are presented. After making several simplifying assumptions (primarily a cylindrical Earth shadow, flat plate geometry, and constant cross-sectional area of the satellite), the time required to raise the modelled DSCS II F-13 satellite 400 km into a disposal orbit is approximately 33 years. This time-to-disposal can be reduced by using a larger area-to-mass ratio and more reflective surface materials.

"Sobre este título" puede pertenecer a otra edición de este libro.

Editorial
BiblioScholar
Año de publicación
2012
Idioma
Inglés
ISBN 10 
1249595770
ISBN 13 
9781249595779
Encuadernación
Tapa blanda
Número de páginas
158
Contacto del fabricante
no disponible
Persona responsable
no disponible