Aerospace propulsion testing use case

Aerospace propulsion testing

  • Case objective: Enable continuous torque, strain, and vibration measurement on high‑pressure‑turbine and accessory‑drive shafts during endurance runs with local buffering to ride through RF shadowing.
  • Other information: Installation on critical shaft sections; low mass to preserve balance. Multi‑channel acquisition synchronised to facility timing for modal/thermal correlation. Operates through thermal transients and harsh environments common in test cells. Mechanical integration engineered to minimise structural impact for post‑test teardown.

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