Kaman HOK-1
Technical Specifications
First Flight: |
N/A |
Number Built: |
N/A |
Length: |
25 feet |
Rotor Diameter: |
47 feet |
Height: |
11 feet 10 inches |
Max Take-Off Wt.: |
N/A |
Empty Wt.: |
N/A |
Max Cruising Speed: |
109 mph 95 kts |
Normal Cruising Speed: |
75 mph 65 kts |
Service Ceiling: |
18,000 feet |
Fuel Capacity: |
N/A |
Range: |
220 miles |
Fuel Type: |
N/A |
Fuel Consumption: |
N/A |
Engine: |
1 Pratt & Whitney R-1340 rated @ 600 HP |
Seating: |
N/A |
Crew: |
1 Pilot |
Engine Specifications
|
Pratt
& Whitney R-1340
|
Type: |
8 Cylinder air cooled |
Length: |
N/A |
Diameter: |
N/A |
Bore: |
5.75 inches |
Stroke: |
5.75 inches |
Displacement: |
1344 cubic inches |
Compression Ratio: |
6 to 1 |
Dry Weight: |
650 to 938 lbs. |
Ignition: |
N/A |
Fuel Grade: |
N/A |
Carburation: |
N/A |
Performance: |
600 HP @ 2250 rpm for take-off |
|