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University of Glasgow

Thermal-vacuum and vibration test facility

Where a payload finds out what it is. Chamber time, a vibration table, and staff who will not let you test without a written procedure.

The facility supports qualification and acceptance testing for small spacecraft and payloads: thermal-vacuum cycling, thermal balance and vibration to launch environments.

Its most valuable service to a first-time team is the insistence on procedure. Before a chamber is pumped down, there is a written test procedure with pass criteria, instrumentation locations, abort conditions and a named person authorised to stop the test. Teams find this laborious in advance and are grateful for it at two in the morning when a thermocouple reads something unexpected.

Booking behaviour is the commonest failure mode. Chamber slots are finite, campaigns take longer than teams project, and a procedure takes weeks to write and review. Programmes that book a slot early and design towards it succeed; programmes that finish the design and then look for a chamber wait, sometimes for months.

Staff are experienced with academic payloads, commercial platforms and the particular anxieties of a team testing flight hardware for the first time.

Specification

  • Thermal-vacuum chamber suitable for payloads up to 12U class
  • Vibration table for sine, random and shock profiles
  • Multi-channel thermocouple and instrumentation logging
  • Thermal balance test capability with solar simulation
  • Clean assembly and integration area adjacent to the chambers
  • Contamination monitoring during chamber operations

What it is the right answer to

Jobs this facility genuinely suits.

  • Thermal-vacuum qualification and acceptance campaigns
  • Thermal balance testing to correlate a thermal model
  • Vibration qualification against a launcher environment
  • Bake-out of assemblies ahead of delivery
  • Anomaly investigation after an unexpected first campaign result

What to bring

Turning up without these costs facility hours rather than bench hours.

  • A draft test procedure, or the intention to write one with facility staff
  • Your thermal model and the predictions the test is meant to check
  • Instrumentation plan, including where thermocouples will actually fit
  • A named test conductor and a person authorised to stop the test

What you leave with

  • Full instrumented logs across every cycle, with anomalies annotated
  • A test report against the agreed pass criteria
  • Correlation data for updating your thermal model
  • A pass, a fail, or a clear description of what remains unproven

Limitations

Worth knowing before you write the proposal.

  • Payload size is limited; larger spacecraft need a commercial facility
  • No testing proceeds without an approved procedure, whatever the schedule pressure
  • A failed campaign consumes the slot, and the next one may be months away