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06STC

Structures & Thermal Control

From geometric centres to thermal extremes, this team makes sure the satellite holds together and keeps cool.

01About STC

Mechanical design, assembly and thermal.

  • CAD
  • FEA
  • Thermal analysis
  • Materials
  • Mechanical testing
  • 4Members
  • 1Leader
  • 5Responsibilities
  • 5Engineering areas

02Video

InsideSTC.

A look inside Structures & Thermal Control: the people, the work, and their part of LISAT-01.

Video coming soon

03Team

The peoplebehind STC.

4 people building Structures & Thermal Control.

A render of LISAT-01 and its internal subsystemsLISAT-01 · render

04Spacecraft platform / STC

Our part ofthe mission.

The department's main mission is to guarantee the satellite's structural integrity: studying geometric centres, centres of mass and material behaviour.

It also designs and tests ventilation and energy-dispersion systems to manage the extreme temperatures the spacecraft will face in orbit.

On LISAT-01

Holds every subsystem inside a 10 × 10 × 10 cm envelope and keeps it within its temperature limits.

In the flight systemHolds the stack together and keeps it inside its temperature limits.

R.01Structural design of the 1U bus
R.02Mass properties and centre-of-mass control
R.03Material selection and behaviour
R.04Thermal modelling and dissipation design
R.05Structural and thermal simulation

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