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Characteristics
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Aircraft Characteristics
Piasecki HUP-1 |
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Crew |
1 pilot, 1 copilot, 1 crewmen in some roles |
| Rotor Type | Tandem |
Engine |
HUP-1 1 Continental R-975-34
radial piston 525 HP T/O; 500 hp continuous; H-25A same horsepower with R-975-42 engine.
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HUP-1 |
Dimensions |
Length |
32ft 10in (9.7m) |
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Height |
12ft 6in (3.8m) |
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Rotor |
35ft (10.67m) |
Weight |
Empty |
4,2141bs (1,913 kg) |
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Loaded |
6,000 lbs (2,724 kg) |
Speed |
Cruise |
75 mph (121 km/h) |
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Maximum |
119.5 mph (119.5 km/h) |
Range |
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275 miles (443 km) |
Ceiling |
Hover OGE |
9,000 ft (2,743 m) |
Hover IGE |
10,200 ft (3,109 m) | |
Service |
12,700 ft (3,871 m) | |
Climb |
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1,220 ft/min (372 m/min) |
Payload |
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4 troops or 2 stretchers + 1 attendant |
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