Bü 133 Jungmeister @·AIRCRAFTUBE

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    Benoit's Jungmeister
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    Bücker Bü 133 Jungmeister
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    Flugplatzfest Hamm
  • Alex Papana's plane at the 1938 Oakland air races Alex Papana's plane at the 1938 Oakland air races
    Alex Papana's plane at the 1938 Oakland air races
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    Jungmeister
  • CASA 1-133C<br>Jungmeister<br>(1957) CASA 1-133C<br>Jungmeister<br>(1957)
    CASA 1-133C
    Jungmeister
    (1957)
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    Bü 133C Jungmeister
  • Jungmeister Jungmeister
    Jungmeister
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    Hirth Bü-133D-1 Jungmeister
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    Bü 133C (2013 Shoreham Airshow)
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    Bücker Bü 133
  • Bü 133C Bü 133C
    Bü 133C
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    Bücker Bü 133 Jungmeister
  • In formation In formation
    In formation
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    Jungmeister of the Military Air Museum (USA)
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    Bü 133
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    Bü 133C Jungmeister
  • Bü 133C Bü 133C
    Bü 133C
  • Bü 133C (Shoreham, 2013) Bü 133C (Shoreham, 2013)
    Bü 133C (Shoreham, 2013)
  • Bü 133C Jungmeister Bü 133C Jungmeister
    Bü 133C Jungmeister
  • Bü 133C Bü 133C
    Bü 133C

Bücker Bü 133

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.

Development

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.

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.

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.

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

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). Hirth HM 6 inline: 160 hp (119 kW) engine.
  • Bücker Bü 133C : Siemens Sh 14A-4: 160 hp (119 kW) radial 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
  • Germany : Luftwaffe
  • Slovakia : Slovak Air Force (1939-1945)
  • South Africa : South African Air Force
  • Spain Spanish Republic : Spanish Republican Air Force
  • Spain Spanish State : Spanish Air Force
  • Switzerland : Swiss Air Force
  • Yugoslavia : SFR Yugoslav Air Force - Postwar.
  • Hungary : Hungarian Air Force

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This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Bücker Bü 133 of Wikipedia ( authors )

Specifications (Bücker Bü 133C)

  • Crew : one pilot.
  • Length : 6.0 m (19 ft 8.25 in).
  • Height : 2.20 m (7 ft 2.5 in).
  • Wingspan : 6.60 m (21 ft 7.75 in).
  • Wing area : 12.0 m² (129.17 ft²).
  • Empty weight : 425 kg (937 lb).
  • Max. takeoff weight : 585 kg (1,290 lb).
  • Maximum speed : 220 km/h (137 mph).
  • Cruise speed : 200 km/h (124 mph).
  • Range : 500 km (311 mi).
  • Service ceiling : 4,500 m (14,765 ft).
  • Powerplant : One Siemens-Halske Sh.14A-4 radial piston engine.
  • Power : 119 kW (160 hp).

— — — = = — — —

This text is available under the Creative Commons Attribution-ShareAlike License
Source : Article Bücker Bü 133 of Wikipedia ( authors )
Bücker Bü 133 Jungmeister : Your comments on this subject
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