Sandesh Rathnavarma Hegde
Sandesh Rathnavarma Hegde
Professional
Verified email at encs.concordia.ca
Title
Cited by
Cited by
Year
Thermally induced microcracks and mechanical property of composite honeycomb sandwich structure: experiment and finite element analysis
SR Hegde, M Hojjati
Journal of Sandwich Structures & Materials 22 (8), 2544-2566, 2020
82020
Design and development of 3-axis reaction wheel for STUDSAT-2
S Kumar, D Sahay, SR Hegde, S Sandya, AK Jha, TC Mahalingesh
2015 IEEE Aerospace Conference, 1-13, 2015
62015
Effect of thermal cycling on composite honeycomb sandwich structures
SR Hegde, M Hojjati
12th International Conference on Sandwich Structures ICSS-12: Proceedings …, 2018
22018
Design and development of inter-satellite separation mechanism for Twin Nano satellite—STUDSAT-2
SR Hegde, D Sahay, S Sandya, GM Sandeep, KV Nikhilesh
2016 IEEE Aerospace Conference, 1-8, 2016
22016
Operational flow of twin satellite mission
K Lamichhane, M Kiran, T Kannan, D Sahay, HG Ranjith, SR Hegde, ...
2015 IEEE Metrology for Aerospace (MetroAeroSpace), 362-366, 2015
22015
Thermal cycling of composite honeycomb sandwich structure for space application
SR Hegde
Concordia University, 2019
12019
Effect of core and facesheet thickness on mechanical property of composite sandwich structures subjected to thermal fatigue
SR Hegde, M Hojjati
International Journal of Fatigue 127, 16-24, 2019
12019
Performance of composite sandwich structures under thermal cycling
SR Hegde, M Hojjati
Journal of Composite Materials 54 (2), 271-283, 2020
2020
Thermo-orbital analysis of STUDSAT-2, A Twin Nano satellite
M Rȧ, KA Sḃ, PK AV, KH Kornaya, S Dȧ, S Hegde
2014
Design of Thermal Control Subsystem of a Twin Nano Satellite STUDSAT-2
A Gaurav, U Makam, GK Das, SR Hegde, S Sandya
Effect of Thermal Cycling on Composite Honeycomb Sandwich Structures for Space Applications
SR Hegde, M Hojjati
EFFECT OF MICROCRACKS ON MECHANICAL PROPERTY OF COMPOSITE HONEYCOMB SANDWICH STRUCTURE SUBJECTED TO THERMAL CYCLING
SR Hegde, M Hojjati
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