Large Deployable Space Antennas Based on Usage of Polygonal Pantograph
Publication: Journal of Aerospace Engineering
Volume 18, Issue 3
Abstract
This paper describes large space antenna projects based on application of a closed polygonal pantograph truss used for transforming, deploying, and prestressing the reflector structure. Their reflecting surfaces represent a flexible mesh fabric. Two means of maintaining the surface are discussed herein. The first technique is associated with employment of forces of the gravity field gradient. The second is based on the use of a flexible carcass prestressed by internal forces applied to the pantograph. Reflectors of the second kind have a rather complicated mechanical structure depending on the way of their attachment to a carrier. Provisions are made for supporting the reflector by an articulated arm linked with its central interface and through the use of tube beams, supporting the reflector periphery structures. During the design of the reflectors, special attention was paid to the problems of their structural simulations at the stages of their launching, deployment, and orbital motion. The deployable antennas considered can be enabling elements for many space missions ranging from communications to other satellite systems, including radar, remote sensing, interferometry, wireless power transmission, etc. They exhibit an enhanced stiffness of structure, required for the digit tele- and radio-communication and navigation, which makes it possible to diminish ray scattering, to raise the power of the accepted signals, and to prevent frequency losses.
Get full access to this article
View all available purchase options and get full access to this article.
References
Chernyavsky, A., et al. (2002). “Large deployable space antenna.” Proc., 25th ESA Antenna Workshop on Satellite Antenna Technology, European Space Research and Technology Center, Noordwijk, The Netherlands, 215–222.
Gulyayev, V. I., Chernyavsky, A. G., Kravchenko V., Gaidaichuk V., Koshkin, V. L., and Kotenko, E. E. (1990). “Dynamics of the system of solid body and flexible elongated rings moving in the gravity field.” Cosmic Res., 28(5), 655–663 (in Russian).
Gulyayev, V. I., Efremov, I. S., Chernyavsky, A. G., Koshkin, V. L., Bondar, V. K., and Shinkar, Y. A. (1994). “Dynamics of orbital station with elongated truss.” Cosmic Res., 31(2), 61–70 (in Russian).
Medzmariashvili, E., et al. (2000).“Theoretical and ground experimental investigations of a large-scale deployable space antenna reflector by space experiment program ‘Reflector’.” Proc., Millennium Conf. on Antennas and Propagation, European Space Research and Technology Center, Noordwijk, The Netherlands, 281–287.
Information & Authors
Information
Published In
Copyright
© 2005 ASCE.
History
Received: Jul 6, 2004
Accepted: Jul 6, 2004
Published online: Jul 1, 2005
Published in print: Jul 2005
Authors
Metrics & Citations
Metrics
Citations
Download citation
If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.