• The structure is made of Aluminum 60-61 T; with hard anodization 20 micrometer.
  • Two options are available for the structure; the first one is fitting the requirements of CubeSat Design Specification (CDS) REV 13 suitable for NASA mission launching opportunities; while the other is fitting with JEM Payload Accommodation Handbook - Vol. 8 - Small Satellite Deployment from JAXA.
  • Both structure options achieved high confidence during vibration testing carried out according to vibration test profile for launchers: HTV, SpX Dragon, and Orbital Cygnus.

Academy of Scientific Research and Technology-Egypt,

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