• Performance:
| |
Maximum Cruise Speed
|
Sea Level |
- 195 knots |
|
|
15,000 ft. |
- 215 knots |
| |
Service Ceiling: |
Estimated |
- 25,000 feet |
| |
Rate of Climb: |
Sea Level |
- 2,100 fpm |
• Range Performance:
| |
VFR Range with max Fuel & Passenger Load: |
Goal is 1,000 mi. however actual range will
depend on final fuel tank configuration. |
| |
* Note: We do not trade off fuel load for passengers |
• Takeoff & Landing Performance:
| |
T/O Distance at Max Takeoff Weight: |
(5,600 #) |
| |
Water: |
1,200 ft. (estimated) |
| |
Land: |
960 ft. |
| |
50 ft Obstacle: |
1,300 ft. |
• Weights:
| |
Empty Weight: |
3,600 pounds (prototype – production will be lighter) |
| |
Gross Weight: |
5,600 pounds |
| |
Useful Load: |
2,000 pounds |
| |
Wing Loading: |
19.8 psf |
• External Aircraft Dimensions:
| |
Height on Wheels: |
12.3 feet |
| |
Length – Nose to Tail: |
43.0 feet |
| |
Wing Span: |
42.9 feet |
• Internal Cabin Dimensions:
| |
Internal Length from nose bulkhead to aft cabin: |
13.2 feet |
| |
Cabin Height: |
4.4 feet (net internal) |
| |
Cabin width at shoulder height while seated: |
4.1 feet (net internal) |
• Seating:
| |
Typical Crew: |
1 Pilot |
| |
Passengers: |
Five to six (aft seat is bench – might hold three across) |
• Power Plant:
| |
Walter 601 Turbine
724 SHP / 657 SHP
continuous |
NOTE: All numbers are computed performance numbers and will be verified during actual Flight Testing |
