CORNUs AIRCRAFT SPECIFICATIONS
Additional Information on the Aircraft
| |
Manufacturer/Builder: Aeronautical products
Aircraft Designation:Model 1
Country of Origin: USA
Period: 1940 -1945
Configuration: Single Main Rotor w/ Tail Rotor |
GENERAL INFORMATION |
| Contract Number: |
NA |
Seats: |
2 |
| Registration: |
NX -1270 |
Rotor Type: |
Articulated |
| Rotor Control: |
|
First Flight: |
1944 |
| Transmission: |
Gearbox |
Source: |
Rotary Wing Handbooks. Prewitt Aircraft, ca. 1950 |
MAIN ROTOR |
| Main Rotors: |
1 ft |
Rotor Disc Loading: |
unknown |
| Rotor Diameter: |
30 ft |
Rotor Power Loading: |
unknown |
| Flight RPM: |
|
Blade Area: |
|
| No. Blades: |
3 |
Blade Dimensions: |
|
| Rotor Airfoil: |
|
Rotor Blade Loading: |
unknown |
| Rotor Disc Area: |
707 ft |
Rotor Tip Speed: |
unknown |
| Rotor Solidity: |
unknown |
Collective Pitch Range: |
unknown |
TAIL ROTOR |
| Tail Rotor: |
unknown |
Tip Speed: |
unknown |
| Diameter: |
unknown |
Pitch Range: |
unknown |
| Disc Area: |
unknown |
Airfoil: |
unknown |
| Solidity: |
unknown |
Power Loss While Hovering: |
unknown |
STRUCTURE |
| Stabilizer Area: |
unknown |
Height: |
unknown |
| Aspect Ratio: |
unknown |
Width: |
unknown |
| Angle of Incidence: |
unknown |
Primary Construction: |
unknown |
| Fuselage Length: |
unknown |
|
|
ENGINE |
| Model: |
unknown |
Fuel Capacity: |
unknown |
| Max Continuous Power: |
135 hp @2750 rpm |
Fuel Consumption: |
unknown |
WEIGHT AND BALANCE |
| Gross Weight: |
unknown |
Useful Load: |
unknown |
| Empty Weight: |
unknown |
CG Range: |
unknown |
PERFORMANCE |
| Max Level Speed: |
100 mph |
Hover Alt. in Ground Effect: |
unknown |
| Cruise Speed: |
85 - 90 mph |
Hover Alt. out of Ground Effect: |
unknown |
| Range: |
unknown |
Service Ceiling |
unknown |
| Best Vertical Speed: |
unknown |
Absolute Ceiling: |
unknown |
| Rate of Descent: |
|
|
|
