Large deployable antennas for space applications become essential in the fields of communications, radio astronomy and Department of Defence (DOD) space-based radar. Since the antenna should be installed in a cargo space of a rocket vehicle during the launch phase, an inflatable deployment concept is inevitable to overcome the size limitation. A newly developed class of space structures, called inflatable-deployable structures, has great potential for satisfying these stringent user requirements. Among the many antenna types available, the parabolic reflector antenna is the most common one mainly due to its high gain, which enable high data rate transmission at low power. Large parabolic reflectors and solar concentrators are of great interest for the applications of satellite. This paper presents the finite element modelling of the parabolic shaped reflector to know the static and dynamic behaviour under the various inflation pressures. Purpose of this study is to highlight the dynamic characteristics of parabolic structures used in space application. The challenge is to assure that inflatable parabolic surfaces have significantly high efficiency and accuracy to satisfy the system requirements. Even the smart material is used for the control of the geometry of the reflecting surfaces and the study is done for the optimal size and placement of actuators and sensors the control of the shape of the reflecting surfaces. So this study is required to understand the dynamic characteristics i.e. frequency and mode shapes of these structures so that we can find out the maximum deflection and deformed shape of the parabolic surfaces.
Skip Nav Destination
ASME 2012 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 12–15, 2012
Chicago, Illinois, USA
Conference Sponsors:
- Design Engineering Division
- Computers and Information in Engineering Division
ISBN:
978-0-7918-4500-4
PROCEEDINGS PAPER
Vibration Analysis of Inflatable Parabolic Structure for Space Application
Y. Sardhara Dipan,
Y. Sardhara Dipan
Indian Institute of Technology-Roorkee, Roorkee, UT, India
Search for other works by this author on:
S. H. Upadhyay,
S. H. Upadhyay
Indian Institute of Technology-Roorkee, Roorkee, UT, India
Search for other works by this author on:
S. P. Harsha
S. P. Harsha
Indian Institute of Technology-Roorkee, Roorkee, UT, India
Search for other works by this author on:
Y. Sardhara Dipan
Indian Institute of Technology-Roorkee, Roorkee, UT, India
S. H. Upadhyay
Indian Institute of Technology-Roorkee, Roorkee, UT, India
S. P. Harsha
Indian Institute of Technology-Roorkee, Roorkee, UT, India
Paper No:
DETC2012-70828, pp. 873-877; 5 pages
Published Online:
September 9, 2013
Citation
Sardhara Dipan, Y, Upadhyay, SH, & Harsha, SP. "Vibration Analysis of Inflatable Parabolic Structure for Space Application." Proceedings of the ASME 2012 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 1: 24th Conference on Mechanical Vibration and Noise, Parts A and B. Chicago, Illinois, USA. August 12–15, 2012. pp. 873-877. ASME. https://doi.org/10.1115/DETC2012-70828
Download citation file:
7
Views
Related Proceedings Papers
Related Articles
Inflatable Concentrators for Solar Propulsion and Dynamic Space Power
J. Sol. Energy Eng (November,1990)
Surface Precision of Inflatable Membrane Reflectors
J. Sol. Energy Eng (November,1998)
Hot Stuff
Mechanical Engineering (December,2002)
Related Chapters
DETECTING AND QUANTIFYING GROUND SUBSIDENCE FOR PIPELINE GEOHAZARD MANAGEMENT USING SATELLITE RADAR INTERFEROMETRY - POTASH MINE SUBSIDENCE EXAMPLE
Pipeline Integrity Management Under Geohazard Conditions (PIMG)
3D Frame Structural Analysis Based on Imported Geometry at Preprocessing
International Conference on Mechanical and Electrical Technology 2009 (ICMET 2009)
PSA Level 2 — NPP Ringhals 2 (PSAM-0156)
Proceedings of the Eighth International Conference on Probabilistic Safety Assessment & Management (PSAM)