CUBESAT TECHNOLOGY PROJECT

Toward Developing the First Lebanese NanoSatellite.

Design of Nanosatellites for Space Applications on Low Earth Orbit

Design of Nanosatellites for Space Applications on Low Earth Orbit

The part B of the Traning "Technology and Design of CubeSats/Nanosatellites for Space Applications on Low Earth Orbit" will include the following items.

Description:

  • Example CubeSat Missions and Payloads
  • CubeSat Design and CubeSat Subsystems
  • Orbital Mechanics
  • Orbital Perturbations
  • Mass and Power Budgets
  • Design drivers and budgeting
  • Structure subsystem specifications and design
  • Hands on CubeSat Training/Development of a CubeSat Table Top Model
  • Hands on CubeSat Training/Orbital Mechanics using STK

Duration: 5 days

Nb. of attendees: in average 60 participants in the Lectures Sessions and 45 participants have been selected to participate to the Hands-on Sessions

Target audience: the training is directed to the researchers and the selected students from the CNRS-L and 12 Lebanese Universities: UL, AUB, LAU, USJ, NDU, LIU, BAU, UOB, RHU, IUL, USEK, UA

Direct application: hands-on exercises on table top model and on STK tool