• 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