ROTORCRAFT

HELICOPTER, ROTORCRAFT & MULTIROTOR TESTING

DYNAMIC IN-FLIGHT TESTING FOR ROTORCRAFT VEHICLES

Testing Challenges:

  • Collecting physical measurements on helicopters and rotorcraft including force, vibration, shock, strain, and temperature
  • Varied test scenarios: laboratory, sled, flight testing/in situ
  • Harsh test environments
  • Remote locations with limited or restricted comm access
  • Size, mass, and power constraints
  • Complex, time-intensive test setups
  • Costly and noisy slip rings for rotating applications

DTS Key Features:

  • SWaP (size, weight & power)-optimized data acquisition units and sensors
  • Embeds in the test article near the sensors, no long cable runs
  • Significantly reduces or eliminates the need for slip rings
  • High-shock rated, IP68 rated solutions available
  • MIL-STD rated systems for temperature, altitude, shock & vibration
  • Wide range of analog sensor support, plus built-in sensor options
  • Onboard memory and real-time streaming options
  • Standalone, network, or integrate into an existing FTI solution
  • COTS products; standard 4-6 week delivery
DTS ADVANCED MEASUREMENT SOLUTIONS - MINIATURE | RUGGED | HIGH-SPEED

RECOMMENDED DTS PRODUCTS FOR ROTORCRAFT

DTS SLICE6 Data Acquisition System

SLICE6 AIR

SLICE NANO Data Acquisition System

SLICE NANO

DTS SLICE6 Data Acquisition System

SLICE MICRO

DTS SLICE6 Data Acquisition System

SLICE IP68

EV Crash Test Photo Credit IIHS

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