PTERA
Prototype • Technology • Evaluation & Research • Aircraft ©
Weight
150-300 lbs
Payload Capacity
25-50 lbs
Endurance
45 minutes on turbine
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