PTERA

Prototype • Technology • Evaluation & Research • Aircraft ©

9

Weight

150-300 lbs

9

Payload Capacity

25-50 lbs

9

Endurance

45 minutes on turbine

9

Airframe

Fuselage and wings are configurable

Flying Laboratory

PTERA exists to bridge the gap between wind tunnel test and manned flight. The platform is a low-cost, low risk intermediary for evaluating and refining technologies and analytical prediction methods before transitioning to full scale flight testing. PTERA uses modular tooling to accommodate a wide variety of aircraft configurations that reduces platform costs. PTERA aims to provide a versatile flying laboratory to test aerodynamic treatments, and to support and validate experiments in aero-efficiency, aeroelasticity, controls and dynamics, health management systems, structures, and acoustics. PTERA features a large payload capacity for sensors, flight data acquisition systems, and flight experiment support equipment.

PTERA-BL

Baseline

  • 200 lbs Gross Takeoff Weight (40 lb payload)
  • Roughly based on 11% scale of 737
  • 12 ft Length
  • 11.3 ft wingspan

PTERA-SAW

Spanwise Adaptive Wing

  • Articulating wing tip in flight
  • Shape memory alloy actuator
  • Swept wings
  • 200lbs Gross Takeoff Weight

PTERA-GMATT

Generic Modular Aircraft T-Tail

  • Dynamically ballasted to mimic CRJ aircraft
  • Swept and tapered wings
  • Tail nacelles
  • 300lbs Gross Takeoff Weight

PTERA-C3

Combined Circulation Control

  • Active circulation control to test Coanda Effect 
  • Blowing over leading and trailing edge of wing
  • Electric fan intake ducts
  • 200lbs Gross Takeoff Weight