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Beneš-Mráz Be-50 Beta-Minor

The Beneš-Mráz Be-50 Beta-Minor was a light airplane manufactured in Czechoslovakia shortly before World War II.

Be-50 Beta-Minor
Be-50 Beta-Minor
Role Sports plane
Manufacturer Beneš-Mráz
Designer Pavel Beneš and Jaroslav Mráz
First flight 1935

Design and development edit

First flown in 1935, it was a low-wing cantilever monoplane of wooden construction, with tandem open cockpits and fixed tailwheel undercarriage. The aircraft proved popular with Czechoslovakia's aeroclubs and was successful in international competitions. In 1937, the designers created a modernised version, the Be-51, which featured a reduced wingspan and fully enclosed cockpits. A final variant, the Be-52 Beta-Major retained the Be-50's open cockpits but featured improved aerodynamics and a more powerful Walter Major engine.

Operational history edit

Like other Czechoslovakian aircraft, all available machines were impressed into Air Force service at the outbreak of war. Several Be-51s survived to be used by the Luftwaffe as liaison aircraft and trainers during the occupation.[1]

In 2015, replica of Be-50 started operating. It crashed at airshow in August 2018, killing its pilot. [2]

Variants edit

Be-50 Beta-Minor
Tandem open cockpits and 12.66 m (41.5 ft) span wings.
Be-51 Beta-Minor
tandem seats in an enclosed cabin and 11.44 m (37.5 ft) span wings.
Be-52 Beta-Major
Strengthened and more powerful two-seat aerobatic trainer, with 10.66 m (35.0 ft) span wings.
Be-56 Beta-Major
Strengthened and more powerful single-seat aerobatic trainer, with 10.66 m (35.0 ft) span wings.

Operators edit

  Independent State of Croatia
  Germany
  Slovakia

Specifications (Be-51 Beta-Minor) edit

Data from [3]

General characteristics

  • Crew: 2
  • Length: 7.76 m (25 ft 6 in)
  • Wingspan: 11.44 m (37 ft 6 in)
  • Height: 2.05 m (6 ft 9 in)
  • Wing area: 15.3 m2 (165 sq ft)
  • Empty weight: 480 kg (1,058 lb)
  • Max takeoff weight: 760 kg (1,676 lb)
  • Powerplant: 1 × Walter Minor 4-cyl. inverted air-cooled in-line piston engine, 71 kW (95 hp) for take-off
  • Propellers: 2-bladed fixed pitch propeller

Performance

  • Maximum speed: 205 km/h (127 mph, 111 kn) at sea level
  • Cruise speed: 180 km/h (110 mph, 97 kn)
  • Range: 800 km (500 mi, 430 nmi)
  • Service ceiling: 5,000 m (16,000 ft)
  • Time to altitude: 1,000 m (3,300 ft) in 6 minutes

Notes edit

  1. ^ Ketley, Barry, and Rolfe, Mark. Luftwaffe Fledglings 1935–1945: Luftwaffe Training Units and their Aircraft (Aldershot, GB: Hikoki Publications, 1996), p.11.
  2. ^ Na Prachaticku spadlo unikátní letadlo Be 50 Beta Minor, pilot zemřel – iDNES.cz
  3. ^ Green, William (2010). Aircraft of the Third Reich (1st ed.). London: Aerospace Publishing Limited. p. 105. ISBN 978-1-900732-06-2.

References edit

  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 152.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 890 Sheet 25.
  • Němeček, V. (1968). Československá letadla. Praha: Naše Vojsko.
  • Green, William (2010). Aircraft of the Third Reich (1st ed.). London: Aerospace Publishing Limited. p. 105. ISBN 978-1-900732-06-2.

beneš, mráz, beta, minor, help, expand, this, article, with, text, translated, from, corresponding, article, czech, february, 2020, click, show, important, translation, instructions, view, machine, translated, version, czech, article, machine, translation, lik. You can help expand this article with text translated from the corresponding article in Czech February 2020 Click show for important translation instructions View a machine translated version of the Czech article Machine translation like DeepL or Google Translate is a useful starting point for translations but translators must revise errors as necessary and confirm that the translation is accurate rather than simply copy pasting machine translated text into the English Wikipedia Do not translate text that appears unreliable or low quality If possible verify the text with references provided in the foreign language article You must provide copyright attribution in the edit summary accompanying your translation by providing an interlanguage link to the source of your translation A model attribution edit summary is Content in this edit is translated from the existing Czech Wikipedia article at cs Benes Mraz Be 50 Beta Minor see its history for attribution You should also add the template Translated cs Benes Mraz Be 50 Beta Minor to the talk page For more guidance see Wikipedia Translation The Benes Mraz Be 50 Beta Minor was a light airplane manufactured in Czechoslovakia shortly before World War II Be 50 Beta MinorBe 50 Beta MinorRole Sports planeManufacturer Benes MrazDesigner Pavel Benes and Jaroslav MrazFirst flight 1935 Contents 1 Design and development 2 Operational history 3 Variants 4 Operators 5 Specifications Be 51 Beta Minor 6 Notes 7 ReferencesDesign and development editFirst flown in 1935 it was a low wing cantilever monoplane of wooden construction with tandem open cockpits and fixed tailwheel undercarriage The aircraft proved popular with Czechoslovakia s aeroclubs and was successful in international competitions In 1937 the designers created a modernised version the Be 51 which featured a reduced wingspan and fully enclosed cockpits A final variant the Be 52 Beta Major retained the Be 50 s open cockpits but featured improved aerodynamics and a more powerful Walter Major engine Operational history editLike other Czechoslovakian aircraft all available machines were impressed into Air Force service at the outbreak of war Several Be 51s survived to be used by the Luftwaffe as liaison aircraft and trainers during the occupation 1 In 2015 replica of Be 50 started operating It crashed at airshow in August 2018 killing its pilot 2 Variants editBe 50 Beta Minor Tandem open cockpits and 12 66 m 41 5 ft span wings Be 51 Beta Minor tandem seats in an enclosed cabin and 11 44 m 37 5 ft span wings Be 52 Beta Major Strengthened and more powerful two seat aerobatic trainer with 10 66 m 35 0 ft span wings Be 56 Beta Major Strengthened and more powerful single seat aerobatic trainer with 10 66 m 35 0 ft span wings Operators edit nbsp Independent State of CroatiaAir Force of the Independent State of Croatia nbsp GermanyLuftwaffe nbsp SlovakiaSlovak Air Force 1939 45 Specifications Be 51 Beta Minor editData from 3 General characteristicsCrew 2 Length 7 76 m 25 ft 6 in Wingspan 11 44 m 37 ft 6 in Height 2 05 m 6 ft 9 in Wing area 15 3 m2 165 sq ft Empty weight 480 kg 1 058 lb Max takeoff weight 760 kg 1 676 lb Powerplant 1 Walter Minor 4 cyl inverted air cooled in line piston engine 71 kW 95 hp for take off Propellers 2 bladed fixed pitch propellerPerformance Maximum speed 205 km h 127 mph 111 kn at sea level Cruise speed 180 km h 110 mph 97 kn Range 800 km 500 mi 430 nmi Service ceiling 5 000 m 16 000 ft Time to altitude 1 000 m 3 300 ft in 6 minutesNotes edit Ketley Barry and Rolfe Mark Luftwaffe Fledglings 1935 1945 Luftwaffe Training Units and their Aircraft Aldershot GB Hikoki Publications 1996 p 11 Na Prachaticku spadlo unikatni letadlo Be 50 Beta Minor pilot zemrel iDNES cz Green William 2010 Aircraft of the Third Reich 1st ed London Aerospace Publishing Limited p 105 ISBN 978 1 900732 06 2 References edit nbsp Wikimedia Commons has media related to Be 50 Beta Minor Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions p 152 World Aircraft Information Files London Bright Star Publishing pp File 890 Sheet 25 Nemecek V 1968 Ceskoslovenska letadla Praha Nase Vojsko Green William 2010 Aircraft of the Third Reich 1st ed London Aerospace Publishing Limited p 105 ISBN 978 1 900732 06 2 Retrieved from https en wikipedia org w index php title Benes Mraz Be 50 Beta Minor amp oldid 1044846572, wikipedia, wiki, book, books, library,

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