Seibel S-4
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| Seibel YH-24 | |
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 YH-24 in flight |
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| Type | Multipurpose observation helicopter |
| Manufacturer | Seibel Helicopter Company |
| Maiden flight | 1951 |
| Primary user | United States Army |
| Number built | 2 |
The Seibel S-4 was the second helicopter type designed and built by Seibel Helicopter Company's Charles Seibel. The S-4 was evaluated by the United States Army under the designation YH-24 Sky Hawk but would be rejected for service. The S-4B would serve as the basis for the design of the Cessna CH-1 Skyhoook, the only helicopter Cessna ever produced.
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[edit] Development
Charles Seibel began development on the S-4 after forming the Seibel Helicopter Company with funding from local Kansas oil investors. The S-4 was a continuation of his work on his previous design, the Seibel S-3, which he flew as a demonstrator for his design concepts; primarily a new design for a two-bladed rotor system and a simplified transmission. These features would also be incorporated into the S-4 design.
In January 1949, the S-4 lifted off the ground for the first time, piloted by Johnny Gibbs. In March 1950, certification tests were completed and on 23 April 1950, the S-4 received civil certification by the CAA. A larger engine, the Lycoming O-290B with 125 hp, would be installed in the aircraft, making it the S-4A.
Based on feedback from the Army during the evaluation, Seibel, shortened the fuselage of the second YH-24 (51-5113) and widened the cockpit for a co-pilot's seat next to the pilot's seat. Seibel also replaced that aircraft's original wheeled, tricyle undercarriage with landing skids. This aircraft would become the S-4B.
[edit] Operational history
Both the U.S. Army and U.S. Air Force showed interest in the S-4. In early 1951, the U.S. Army ordered two examples for operational and engineering evaluation in the observation, utility, and aeromedical evacuation roles. The Army designated the S-4 as the YH-24 Sky Hawk. The first Sky Hawk, serial number 51-5112, was delivered to Fort Bragg, North Carolina in April 1951; the second YH-24, serial number 51-5113, was delivered to Wright Field.
Despite the simplicity of the S-4, the Army determined that it did not provide a sufficient payload capability and the aircraft were dropped from the inventory and returned back to Seibel in 1952.
[edit] Design
The S-4 frame was a welded steel-tube box frame, with two decks. A lower deck supported the control panel, pilot's seat, wheeled, tricyle landing gear, and a small passenger/cargo area accessible from the rear, and an upper deck carried the engine, the fuel and oil tanks, and supported the transmission and rotor assembly. A tapered, monocoque, alloy tail boom with a two-bladed antitorque tail rotor was attached at the rear of the upper deck.
[edit] Variants
- S-4
- Original design, certified by the CAA in 1950.
- S-4A
- Featured an upgraded, 125 hp Lycoming O-290B engine.
- S-4B
- Modified airframe based on Army recommendations during YH-24 evaluation. Two-seat cockpit and skid landing gear.
[edit] Specifications (YH-24)
General characteristics
- Crew: 1-2
- Capacity: 583 lbs (265 kg)
- Length: 27 ft 10 in (8.48 m)
- Rotor diameter: ()
- Height: 10 ft 1 in (3.05 m)
- Empty weight: 946 lb (430 kg)
- Max takeoff weight: 1529 lb (695 kg)
- Powerplant: 1× , 127 hp (95 kw)
Performance
- Maximum speed: 62 mph (105 km/h)
- Cruise speed: 58 mph (93 km/h)
- Service ceiling 4298 ft (1310 m)
- Power/mass: 0.08 hp/lb (0.22 kW/kg)
[edit] References
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