Girish Mahajan (Editor)

Bücker Bü 133

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Top speed
  
220 km/h

Length
  
6 m

Manufacturer
  
Bücker Flugzeugbau

Wingspan
  
6.6 m

Engine type
  
Reciprocating engine

Designer
  
Carl Bücker

Bücker Bü 133 imgwpscnrucammsar141pics21jpg

The Bücker Bü 133 Jungmeister (Young master) was an advanced trainer of the Luftwaffe in the 1930s. It was a single-engine, single-seat biplane of wood and tubular steel construction and covered in fabric.

Contents

B cker b 133 jungmeister


Development

Bücker Bü 133 Bcker B133 Jungmeister Photos AirplanePicturesnet

The Bü 133 was a development of the Bücker Bü 131 Jungmann two-seat basic trainer. First flown in 1935 (by Luise Hoffmann, the first female works pilot in Germany), it was slightly smaller than the Bü 131. The prototype, D-EVEO, was powered by a 140 hp (104 kW) Hirth HM506 inverted, air-cooled inline-6 engine.

Bücker Bü 133 Bcker B133 Jungmeister Photos AirplanePicturesnet

The aircraft showed "astonishing agility" at its first public appearance, the 1936 International Aerobatic Championship at Rangsdorf, but the Bü 133A garnered no orders; only two Bü 133Bs, with 160 hp (119 kW) version of that same Hirth HM506 inline-6 engine, were built.

Bücker Bü 133 Bcker B 133 Wikipedie

The main production type was the 160 hp (119 kW) Siemens-Bramo Sh 14A radial powered Bü 133C, which had a distinctive cowling and a 13 cm (5.1 in)-shorter fuselage, and the same fine aerobatic performance as the Bü 133A.

Bücker Bü 133 Paolo Severin Bcker Jungmeister 33 scale

Fifty-two were manufactured under licence by Dornier for the Swiss Air Force (which kept it in service until 1968),. A similar number were built for the Spanish air force by CASA, and were designated the CASA 1-133.

Operational history

Bücker Bü 133 Bcker B 133 Wikipedia

The Bü 133C racked up numerous victories in international aerobatic competition, and by 1938 was the Luftwaffe's standard advanced trainer. At the Brussels meet that year, a three-man Luftwaffe team made a strong impression on Reichsmarschall Hermann Göring, who ordered a nine-man team be formed. It dazzled the crowds at the International Flying meet in Brussels the next year.

The Jungmeister design remained competitive in international aerobatic competition into the 1960s.

Variants

Bücker Bü 133A
Hirth HM 6 inline engine: 135-hp (101-kW)
Bücker Bü 133B
applied to licence-built aircraft (only two versions were ever constructed of this variant).
Bücker Bü 133C
Siemens Sh 14A-4 engine
CASA 1.133
Spanish-built variant.
Price/American Tiger Club Jungmeister
Plans for homebuilt construction.

Operators

 Independent State of Croatia
  • Zrakoplovstvo Nezavisne Države Hrvatske
  •  Nazi Germany
  • Luftwaffe
  •  Slovakia
  • Slovak Air Force (1939-1945)
  •  South Africa
  • South African Air Force
  • Spanish Republic
  • Spanish Republican Air Force
  • Spanish State
  • Spanish Air Force
  •   Switzerland
  • Swiss Air Force
  •  Yugoslavia
  • SFR Yugoslav Air Force - Postwar.
  •  Hungary
  • Hungarian Air Force
  • http://avia-info.hu/talalat.php?Funkcio=osszetett&KeresettSzo=&Keresolista=mind&GTA=t72&Uzem=&Hazai=&Fajta=&Uzemkezdet=&Uzemveg=&Hely=&Megszunes=&Megjelenes=&Frisseseg=&Sorrend=jel&Darab=15&kEgyszerusitett=N&B1=K%FCld%E9s

    Specifications (Bücker Bü 133C)

    Data from The Concise Guide to Axis Aircraft of World War II - David Mondey

    General characteristics

  • Crew: one, pilot
  • Length: 6.0 m (19 ft 8.25 in)
  • Wingspan: 6.60 m (21 ft 7.75 in)
  • Height: 2.20 m (7 ft 2.5 in)
  • Wing area: 12.0 m² (129.17 ft²)
  • Empty weight: 425 kg (937 lb)
  • Max. takeoff weight: 585 kg (1,290 lb)
  • Powerplant: 1 × Siemens-Halske Sh.14A-4 radial piston engine, 119 kW (160 hp)
  • Performance

  • Maximum speed: 220 km/h (137 mph)
  • Cruise speed: 200km/h (124mph)
  • Range: 500 km (311 mi)
  • Service ceiling: 4,500 m (14,765 ft)
  • References

    Bücker Bü 133 Wikipedia