Kaman SH-2
Technical Specifications
| First Flight: |
July 25, 1959 |
| Number Built: |
192 |
| Length: |
52 feet 7 inch |
| Rotor Diameter: |
44 feet |
| Height: |
15 feet 6 inches |
| Max Take-Off Wt.: |
12,800 lbs. |
| Empty Wt.: |
7,040 lbs. |
| Max Cruising Speed: |
165 mph 143 kts |
| Normal Cruising Speed: |
150 mph 130 kts |
| Service Ceiling: |
22,500 feet |
| Fuel Capacity: |
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| Range: |
366 miles |
| Fuel Type: |
Jet A |
| Fuel Consumption: |
N/A |
| Engine: |
2 GE T58-GE-8F Turboshaft 1350 shp |
| Seating: |
1 Tactical Coordinator |
| Crew: |
2 Pilots |
Engine Specifications
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General Electric T58-GE-8F
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| Type: |
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| Length: |
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| Diameter: |
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| Bore: |
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| Stroke: |
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| Displacement: |
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| Dry Weight: |
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| Ignition: |
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| Fuel Grade: |
Jet A |
| Carburation: |
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| Performance: |
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