| Bell YFM-1 Airacuda | ||
|---|---|---|
| Description | ||
| Role | Bomber destroyer | |
| Crew | 5 | |
| First Flight | 1 September, 1937 | |
| Manufacturer | Bell | |
| Dimensions | ||
| Length | 44ft 10in | 13.67m |
| Wingspan | 69ft 10in | 21.29m |
| Height | 13ft 7in | 4.14m |
| Wing area | ft² | m² |
| Weights | ||
| Empty | lb | kg |
| Loaded | lb | kg |
| Maximum takeoff | lb | 8650kg |
| Powerplant | ||
| Engines | 2 Allison V-1710 inline | |
| Power | 1,150hp | kW |
| Performance | ||
| Maximum speed | 277mph | 446km/h |
| Combat range | miles | km |
| Ferry range | miles | km |
| Service ceiling | 30,500 ft | 9,300m |
| Rate of climb | ft/min | m/min |
| Wing loading | lb/ft² | kg/m² |
| Power/Mass | hp/lb | kW/kg |
| Avionics | ||
| Avionics | ||
| Armament | ||
| Guns | 2 37mm cannon 2 .50 and 2 .30 machine guns | |
| Bombs | 146kg | |
| Rockets | ||
A single forward firing M4 37 mm cannon with an accompanying gunner was mounted in a forward compartment on each of the engine nacelles. Although capable of aiming the cannons, the gunner's primary purpose was simply to load them with the 110 rounds of ammunition stored in each nacelle.
The Allison V-1710-13 engines, though relatively trouble free in other types, had no additional cooling systems. Like many pusher designs they were prone to overheating. On the ground the aircraft had to be towed to and from the runway, and could only be started when it was able to takeoff immediately. Even in the air it was not uncommon to experience overheating problems. Towards the end of its operational life the aircraft were flown primarily for photo opportunities, and always accompanied by a chase plane for safety.
Flight testing proved the plane virtually impossible to control on a single engine, as the aircraft would go into an immediate spin. Pitch problems were also encountered, and had to be corrected by reducing power.
The Airacuda was the only aircraft ever built to rely on an independent auxiliary power unit (APU) to power both engine fuel pumps, as well as all aircraft electrical systems. Systems usually powered by an aircraft's engines were instead powered by the single generator. The generator, with its own supercharger, was located in the belly of the aircraft. In the event of a failure the crew was instructed to begin immediate emergency restart procedures as the aircraft basically shut down.
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It uses material from the
"Bell YFM-1 Airacuda".
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