DocumentCode
3663701
Title
Development and design challenges in VELOX-I nanosatellite
Author
L. S. Lim;T. D. V. Bui;Z. Lau;M. S. C. Tissera;J. J. Soon;J. M. Lew;H. Aung;C. Ye;K. S. Low;S. T. Goh;S. S. Chen
Author_Institution
Satellite Research Centre, School of Electrical and Electronic Engineering, Nanyang Technological University, Singapore
fYear
2015
Firstpage
158
Lastpage
163
Abstract
VELOX-I is a student built 3U Cubesat in Nanyang Technological University, Singapore. It has been successfully launched in 30 June 2014. The VELOX-I development process has been improved through the past picosatellite development and operation experience. However, the design of several key components has to be carefully considered as the VELOX-I have more complex missions and payloads. This paper discusses the challenges of VELOX-I design, and the alternative solution proposed by the team. These challenges include the in-house design deployment mechanism, optical extension tube, multi-layer insulator and impact of 3U Cubesat structure on the communication system. Each design is required to meet several requirements such as operating temperature, overall thickness and satellite mass. In summary, the success of VELOX-I ground contact and primary payload mission have proven the flight heritage of the presented design solutions.
Keywords
"Satellites","Optical sensors","Heating","Optical imaging","Electron tubes","Solar panels","Wires"
Publisher
ieee
Conference_Titel
Space Science and Communication (IconSpace), 2015 International Conference on
Electronic_ISBN
2165-431X
Type
conf
DOI
10.1109/IconSpace.2015.7283826
Filename
7283826
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