Piasecki H-25
Technical Specifications
| First Flight: |
March 1948 |
| Number Built: |
339 |
| Length: |
56 feet 11 inches |
| Rotor Diameter: |
2 @ 35 feet each |
| Height: |
12 feet 6 inches |
| Max Take-Off Wt.: |
6,100 lbs. |
| Empty Wt.: |
3,928 lbs. |
| Max Cruising Speed: |
105 mph 91 kts |
| Normal Cruising Speed: |
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| Service Ceiling: |
10,000 feet |
| Fuel Capacity: |
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| Range: |
300 miles |
| Fuel Type: |
100/130 octane |
| Fuel Consumption: |
N/A |
| Engine: |
1 Continental R-975-46A rated @ 550 HP |
| Seating: |
4 Passengers |
| Crew: |
2 Pilots |
Engine Specifications
|
Wright R-975-46A
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| Type: |
9 cylinder air cooled radial |
| 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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| Compression Ratio: |
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| Dry Weight: |
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| Ignition: |
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| Fuel Grade: |
100/130 octane |
| Carburation: |
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| Performance: |
Take-Off: 550 HP @ RPM
Normal: HP @ RPM |
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