This paper is published in Volume-4, Issue-3, 2018
Area
Kinematic And Dynamic Analysis Of Deploy Able Structure
Author
Santoshkumar Ganeshnavar, Shreeshial B, Ajai Kumar Shrivastava, Sivakumar S., Jai Kumar V
Org/Univ
Electronics And Radar Development Establishment (DRDO), Bengaluru, Karnataka, India
Keywords
Unfurlable mechanism, Rim truss, Offset fed paraboloid reflector, Simulation
Citations
IEEE
Santoshkumar Ganeshnavar, Shreeshial B, Ajai Kumar Shrivastava, Sivakumar S., Jai Kumar V. Study of unfurlable mechanism for space radars, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.
APA
Santoshkumar Ganeshnavar, Shreeshial B, Ajai Kumar Shrivastava, Sivakumar S., Jai Kumar V (2018). Study of unfurlable mechanism for space radars. International Journal of Advance Research, Ideas and Innovations in Technology, 4(3) www.IJARIIT.com.
MLA
Santoshkumar Ganeshnavar, Shreeshial B, Ajai Kumar Shrivastava, Sivakumar S., Jai Kumar V. "Study of unfurlable mechanism for space radars." International Journal of Advance Research, Ideas and Innovations in Technology 4.3 (2018). www.IJARIIT.com.
Santoshkumar Ganeshnavar, Shreeshial B, Ajai Kumar Shrivastava, Sivakumar S., Jai Kumar V. Study of unfurlable mechanism for space radars, International Journal of Advance Research, Ideas and Innovations in Technology, www.IJARIIT.com.
APA
Santoshkumar Ganeshnavar, Shreeshial B, Ajai Kumar Shrivastava, Sivakumar S., Jai Kumar V (2018). Study of unfurlable mechanism for space radars. International Journal of Advance Research, Ideas and Innovations in Technology, 4(3) www.IJARIIT.com.
MLA
Santoshkumar Ganeshnavar, Shreeshial B, Ajai Kumar Shrivastava, Sivakumar S., Jai Kumar V. "Study of unfurlable mechanism for space radars." International Journal of Advance Research, Ideas and Innovations in Technology 4.3 (2018). www.IJARIIT.com.
Abstract
Unfurlable rim truss antennae are considered to be the most suitable for developing large size aperture structures for space antenna. They have largely deployed to stowed volume ratio, precision, and reliability in its operation. The mechanism is capable of altering its configuration from a stowed to deployed shape to meet specific operational requirements of space-borne radar. The proposed study of unfurlable mechanism for paraboloid reflector antenna is made up number of parallelogram units comprised of links with appropriate hinge joints, which concatenate in a repeatable fashion to form the desired structure. This study include geometric modeling, kinematic simulation and preliminary structural analysis of unfurlable rim truss