Stearman Hammond Y-1S

Stearman Hammond Y-1S

LandUsa
RoleUtiliteit eendekker
Eerste vluchtOnbewust
Gebouwd20

De Stearman-Hammond Y-1 was een Amerikaanse eendekker uit de jaren 1930, gebouwd door de Stearman-Hammond Aircraft Corporation en geëvalueerd door de Amerikaanse marine en de Britse Royal Air Force

Bron: Stearman Hammond Y-1S op Wikipedia
Stearman Hammond Y-1S Walk Around
Fotograaf Vladimir Yakubov
Lokalisatie Het Museum van de Lucht van Hiller, San Carlos, Californië
Foto 's 47
Wacht, Zoeken Stearman Hammond Y-1S voor u...

Fms Rc Vliegtuigen voor Volwassenen Afstandsbediening Vliegtuig 1300MM (52

Zie ook:

Tweede Wereldoorlog: de definitieve visuele geschiedenis van Blitzkrieg tot de atoombom (DK Definitive Visual Histories) - Amazon Kaart voor kaart van de Tweede Wereldoorlog (DK History Map by Map) - Amazon


General Characteristics

The Stearman-Hammond Y-1S was a unique, two-seat experimental aircraft designed in the mid-1930s with safety and ease of control as its primary goals. Its unusual pusher propeller configuration and tricycle landing gear were radical for the time.

Property Value (Y-1S Production Model)
Role Experimental Light Aircraft, Safety Design
Fabrikant Stearman-Hammond Aircraft Corporation
First Flight 1934
Bemanning 1 pilot
Passenger Capacity 1 passenger (side-by-side seating)
Maximum Take-Off Weight 950 kg (2,090 lb)
Aantal gebouwd 20 (Approximate)

Design and Powerplant

  • Engine: One Menasco B6S six-cylinder air-cooled inverted in-line engine.
  • Power Output: 150 hp (112 kW).
  • Propeller: Two-bladed propeller mounted behind the wing trailing edge in a pusher configuration.
  • Landing Gear: Featured a tricycle landing gear (nose wheel and two main wheels), a highly advanced and rare feature in the 1930s, designed to prevent ground looping.
  • Flight Controls: Simplified three-control system. Notably, yaw and roll were controlled by combined rudders/ailerons (“rudderons”), intended to be easier for non-professional pilots.
  • Configuration: High-wing, twin-boom monoplane.

Performance and History

  • Maximum Speed: 204 km/h (127 mph).
  • Cruise Speed: 185 km/h (115 mph).
  • Operational Range: Approximately 725 km (450 miles).
  • Historical Note: The Y-1S won the U.S. Bureau of Air Commerce’s competition for a safe, low-cost private aircraft, but poor sales due to its high price and unusual configuration led to the company’s collapse.
  • Legacy: Although a commercial failure, its innovative design elements, particularly the pusher engine and tricycle gear, influenced later aircraft safety and general aviation design.

Bekeken : 618

Het is niet meer mogelijk om te reageren.