Stout Bushmaster 2000 | |
|---|---|
| País | E.e.u.u |
| Papel | Avión |
| Primer vuelo | 1964 |
| Buily | 2 |
el Bushmaster 2000 fue un pequeño avión de pasajeros construido en los Estados Unidos en un intento de revivir el diseño del Ford Trimotor. El trabajo comenzó en 1953 probando un Trimotor vintage y en 1954 Bill Stout compró los derechos de diseño del Trimotor original. Debido a problemas de licencia de "Ford Tri-Motor", el Ford 15-AT-D recibió el nombre de Bushmaster 2000. El 15 de enero de 1955, Stout y su socio Robert Hayden de Hayden Aircraft Corporation anunciaron que planeaban construir 1.000 nuevos Bushmasters, pero pasarían once años antes de que volara el primer prototipo del nuevo diseño.
Fuente: Stout Bushmaster 2000 en Wikipedia
| Bushmaster 2000 Walk Around | |
|---|---|
| Fotógrafo | Michael Benolkin |
| Localización | Unknow |
| Fotos | 18 |
Ver también:
por William T. Larkins
168 Páginas · 1992
General Characteristics and Design
The Stout Bushmaster 2000 was a small commuter airliner built in the United States during the 1960s and 1980s. It was an ambitious, modernized attempt to revive the design of the famous Ford Tri-Motor (“Tin Goose”) from the 1920s. Bill Stout, the original designer of the Tri-Motor, bought back the design rights with the intent to produce a simple, rugged, and economical transport aircraft for the “bush flying” market. Although the Bushmaster 2000 featured modern engines, hydraulic brakes, larger windows, and a lighter aluminum-alloy skin, only two examples were ever completed due to competition from contemporary designs and financial issues.
| Property | Typical Value |
|---|---|
| Papel | Commuter Airliner / Utility Transport |
| National Origin | Estados Unidos |
| Fabricante | Bushmaster Aircraft / Aircraft Hydro-Forming |
| First Flight | 1964 |
| Número construido | 2 |
| Equipo | Dos |
| Capacidad | 23 passengers (high density) |
| Longitud | 15.44 m (50 ft 8 in) |
| Envergadura | 23.75 m (77 ft 11 in) |
| Empty Weight | 3,402 kg (7,500 lb) |
| Gross Weight | 5,670 kg (12,500 lb) |
Powerplant and Performance
- Engines: 3 x Pratt & Whitney R-985-AN-1 Wasp Junior nine-cylinder, air-cooled radial engines.
- Power Output (Each): 336 kW (450 hp).
- Maximum Speed: 206 km/h (128 mph; 111 kn) Indicated Airspeed (IAS).
- Cruise Speed: Approx. 185 km/h (115 mph).
- Range: 1,127 km (700 mi; 610 nmi).
- Stall Speed: 89 km/h (55 mph; 48 kn).
Key Modernization Features
- Propellers: Used Hartzell HC-B3R30-2E fully-feathering three-blade constant-speed propellers—a significant upgrade from the original Ford Tri-Motor.
- Construction: Retained the classic corrugated aluminum skin, but used new, lighter, and stronger aluminum sheet and improved riveting.
- Brakes: Replaced the original aircraft’s unique hand-operated “Johnny Brake” system with a modern foot-operated hydraulic brake system.
- Flight Controls: Control cables were rerouted internally, and the vertical stabilizer was made taller with a dorsal fin to improve stability and reduce yaw.
- Landing Gear: Features included Goodrich single-disc brake main wheels and tubeless tires, with the option for floats or skis.
Vistas : 808
También puede ver:
McDonnell Douglas KC-10 Extender – Fotos y Video
McDonnell FH Phantom – Fotos y Video
C-130J Hércules – Fotos y Video
Macchi MC-200 - WalkAround
PZL P.11 – WalkAround
P-51 Mustang vol2 – Caminar
Bell P-63E KingCobra – WalkAround
Vought F4U Corsair – WalkAround
F4U-7 Corsair – WalkAround
Douglas A-26 Invader – WalkAround