3U CubeSat Launch

3U CubeSat Launch. This requirement is for the launch of a CubeSat mission which would make in situ measurements of the lower thermosphere, measure thermospheric winds, and carry out spacecraft aerodynamic characterisation and control tests. This requirement has specific Orbit Injection, and launch period. The Space Systems Engineering research group has a wide range of interests and expertise in the development of novel technologies and methods for space system design and state-of-the-art research in orbital and h...