Equator P2 Excursion
The EQP2 Excursion is a Carbon Composite Construction, Hybrid / Electric Powered Amphibian Aircraft. Aiming for the Experimental category first – followed by the ultra light, ELA & LSA markets.
SPECIFICATIONS
- Seats: 2
- Emty Wheight: 390kg
- Maximum Takeoff Weight: 690kg
- Useful Load: 200kg
- Cruise Speed: 180-200km/h
- Range: 1200km
- Stall Speed: 65km/h
- Engine: Electric Enstroj – EMRAX engine. 85kW/125HP
- Generator: WST Engine and Generator Producing 60kW
DIMENSIONS
- Wing Span: 10m
- Aircraft Length: 6.0m
- Aircraft Height: 2.6m
DESIGN FEATURES
- Retractable landing gear
- Protected fender nose and Wing leading edges
- Functional Entry and Exit; sideways and over the nose.
- Equator float wing system (gangplank)
PERFORMANCE FEATURES
- High-strength, lightweight carbon / glass and aramid fiber components
- Amphibious design (flies off land and water)
- Hybrid Engine Solution
COCKPIT AND CABIN FEATURES
- Accessible Cockpit Design – Entry over the nose
- Quiet and vibration free cockpit due to engine placement and power source
- High-visibility, 200° wrap-around canopy
- Multiple Ergonomic Storage Compartments
- Storage Web (for bulky cargo like bikes, special luggage, skis, bicycles etc.) in the hull
- Glass (LCD) multifunction display
- “Sleep in cabin” foldable seating cabin solutions
SAFETY FEATURES
- Water capability
- Twin Engines
- Electric engines and Hybrid solution means increased redundancy
- Float Wing means the plane cannot capsize, no wingovers
- Power plant placement, far off the ground and safe.
- Predictable flying characteristics
- Very low stall speed
- BRS parachute option being reviewed
Specifications and features are not guaranteed to be true or accurate and are subject to change. Actual aircraft performance will vary depending on options installed on the aircraft. The list of requirements and features will be revised through the duration of the P2 development phase, the list stands as a utopia and goal for the design.
[ad#ad-2]
