Fieseler Fi 333

The Fieseler Fi 333 was a project of a military multi - purpose transport aircraft the Gerhard Fieseler Werke in 1939. It was the company's internal name Project P 30

Interpretation

Airborne Data Sheet of the Reich Air Ministry (RLM) this aircraft was presented in two versions, with and without load space.

In the version of the Fi 333 with load space under the hull flattened a replaceable transport module could be attached. Through this module, the aircraft should be adapted for use as a troop and load transporters, skydiver aircraft, air ambulance and tow plane. The chassis in tandem design was very high in order to ensure the ground clearance of the transport module. In addition, it had better take a special landing position to the loads during landing impact in addition to a roll and flight position.

The version without load space was intended for use as a rescue aircraft fuselages and structure. It also serves to engineer equipment, storm or motor boats and flyable fighters should be transported. Similarly, one had thought to use as a flying tanker. In this version of the Fi 333 of the fuselage should get a fully glazed nose and have a rigid single chassis.

For both versions of the Fi 333 two BMW Bramo were provided 323 D radial engines with 1,000 horsepower than drive.

The project was aborted after the design phase.

Specifications

  • Wingspan: 30.0 m
  • Length: 20.0 m
  • Height: 5.8 m
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