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Rogožarski Brucoš

Rogožarski Brucoš (Serbian Cyrillic:Рогожарски Бруцош) was a single-engine, two-seat, low wing monoplane aircraft designed as a trainer in Yugoslavia before World War II. It was designed and built in the Rogožarski aircraft factory in Belgrade.[2]

Rogožarski Brucoš
Rogožarski Brucoš
Role trainer
National origin Yugoslavia
Manufacturer Prva Srpska Fabrika Aeroplana Živojin Rogožarski, Belgrade
Designer Miroslav Nenadović and Milenko Mitrović-Spirta
First flight 1940
Retired 1941
Primary user Yugoslav Royal Air Force
Number built 1[1]
de Havilland Gipsy Major engine

Design and development

In order to replace its obsolete pilot training aircraft, the Zmaj Fizir FN biplane, the Yugoslav Royal Air Force (YRAF) Command held a competition in mid-1936 to develop a new aircraft for training pilots. The new aircraft was to be a low wing aircraft so that Yugoslavian pilots could get accustomed to piloting the fighters that the Yugoslav Royal Air Force was using, the Hawker Hurricane, Messerschmitt Bf 109 and the Rogožarski IK-3.

The Rogožarski Factory decided to participate in the competition and engaged two well-known aerospace engineers, Miroslav Nenadović and Mitrović Milenko-Spirta, who began working on the design. Building of the prototype started the same year, and it flew for the first time in May 1940. It was handed over to the YRAF for examination, and aircraft functionality.[3]

Operational history

During the testing done in the aircraft repair plant all deficiencies observed were remedied and the plane was able to fly again before October 1940. Simultaneously with the repairs the wings underwent reconstruction so they could enter into reverse - this was the first Yugoslav aircraft with folding wings. Unfortunately, the Commission had already given an unfavorable opinion on the Brucoš. Factory Rogožarski objected to this view, and formed a new commission to re-examine all the additional aircraft that participated in the contest. The second Commission declared the Ikarus Aero 2 aircraft as the best.

Desiring, however, to sell his plane, and in cooperation with Royal Yugoslav Navy aviation, the factory re-designed the Rogožarski "Brucoš" as a floatplane with a 140 kW Walter Six engine and floats from the Canadian Edo Aircraft Corporation. This aircraft was offered to the Navy command as a floatplane for basic training.

At the beginning of April, the single Brucoš was in the hangar of the Experiment Aero Group at Zemun airport, only to be flown on 10 April 1941 to the war airfield in Veliki Radinci where the first fighter brigade had been relocated. The Brucoš is believed to have been burnt with other aircraft to keep them from falling into enemy hands.[4]

Operators

  Kingdom of Yugoslavia

Specifications

Data from Janić, Čedomir. "Rogožarski "Brucoš""

General characteristics

  • Crew: 2
  • Length: 8.10 m (26 ft 7 in)
  • Wingspan: 10.00 m (32 ft 10 in)
  • Height: 3.10 m (10 ft 2 in)
  • Wing area: 16.00 m2 (172.2 sq ft)
  • Empty weight: 615 kg (1,356 lb)
  • Gross weight: 872 kg (1,922 lb)
  • Powerplant: 1 × de Havilland Gipsy Major I four-cylinder inline piston engine, 96 kW (130 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 185 km/h (115 mph, 100 kn) 210 km/h at sea level
  • Range: 840 km (520 mi, 450 nmi)
  • Service ceiling: 4,000 m (13,000 ft)
  • Rate of climb: 2.54 m/s (500 ft/min)

See also

Notes

  1. ^ Петровић, O. (2004). Војни аероплани Краљевине СХС/Југославије (Део II: 1931–1941.). Београд: МВЈ Лет 3.
  2. ^ "Рогожарски Бруцош".
  3. ^ Janić, Čedomir. "Rogožarski "Brucoš"" (in (Serbian)). Aeromagazin (-{YU}--Београд: BB Soft). ISSN 1450-6068.
  4. ^ Петровић, Огњан М. (3/2004.). "Војни аероплани Краљевине СХС/Југославије (Део II: 1931–1941.)" (in (Serbian)). Лет - Flight (-{YU}--Београд: Музеј југословенског ваздухопловства) 3: 60.. ISSN 1450-684X.

References

  • Grey, C.G. (1972). Jane's All the World's Aircraft 1938. London: David & Charles. ISBN 0-7153-5734-4.
  • Gunston, Bill (1989). World Encyclopaedia of Aero Engines (2 ed.). Wellingborough: Patrick Stephens Ltd. ISBN 1-85260-163-9.
  • Janić, Čedomir; O. Petrović (2011). Short History of Aviation in Serbia. Beograd: Aerokomunikacije. ISBN 978-86-913973-2-6.
  • Петровић, Огњан М. (March 2004). "Војни аероплани Краљевине СХС/Југославије (Део II: 1931–1941.)". Лет - Flight (in Serbian). YU-Београд: Музеј југословенског ваздухопловства. 3: 60. ISSN 1450-684X.
  • Станојевић, Драгољуб.; Чедомир Јанић (December 1982). Животни пут и дело једног великана нашег ваздухопловства - светао пример и узор нараштајима. Машинство (in Serbian). YU-Београд: Савез инжењера и техничара Југославије. 31: 1867–1876.
  • Janić, Čedomir. "Rogožarski "Brucoš"". Aeromagazin (in Serbian). YU-Београд: BB Soft. ISSN 1450-6068.

External links

  • www.airwar.ru - in Russian
  • Rogožarski Brucoš

rogožarski, brucoš, serbian, cyrillic, Рогожарски, Бруцош, single, engine, seat, wing, monoplane, aircraft, designed, trainer, yugoslavia, before, world, designed, built, rogožarski, aircraft, factory, belgrade, role, trainernational, origin, yugoslaviamanufac. Rogozarski Brucos Serbian Cyrillic Rogozharski Brucosh was a single engine two seat low wing monoplane aircraft designed as a trainer in Yugoslavia before World War II It was designed and built in the Rogozarski aircraft factory in Belgrade 2 Rogozarski BrucosRogozarski BrucosRole trainerNational origin YugoslaviaManufacturer Prva Srpska Fabrika Aeroplana Zivojin Rogozarski BelgradeDesigner Miroslav Nenadovic and Milenko Mitrovic SpirtaFirst flight 1940Retired 1941Primary user Yugoslav Royal Air ForceNumber built 1 1 de Havilland Gipsy Major engine Contents 1 Design and development 2 Operational history 3 Operators 4 Specifications 5 See also 6 Notes 7 References 8 External linksDesign and development EditIn order to replace its obsolete pilot training aircraft the Zmaj Fizir FN biplane the Yugoslav Royal Air Force YRAF Command held a competition in mid 1936 to develop a new aircraft for training pilots The new aircraft was to be a low wing aircraft so that Yugoslavian pilots could get accustomed to piloting the fighters that the Yugoslav Royal Air Force was using the Hawker Hurricane Messerschmitt Bf 109 and the Rogozarski IK 3 The Rogozarski Factory decided to participate in the competition and engaged two well known aerospace engineers Miroslav Nenadovic and Mitrovic Milenko Spirta who began working on the design Building of the prototype started the same year and it flew for the first time in May 1940 It was handed over to the YRAF for examination and aircraft functionality 3 Operational history EditDuring the testing done in the aircraft repair plant all deficiencies observed were remedied and the plane was able to fly again before October 1940 Simultaneously with the repairs the wings underwent reconstruction so they could enter into reverse this was the first Yugoslav aircraft with folding wings Unfortunately the Commission had already given an unfavorable opinion on the Brucos Factory Rogozarski objected to this view and formed a new commission to re examine all the additional aircraft that participated in the contest The second Commission declared the Ikarus Aero 2 aircraft as the best Desiring however to sell his plane and in cooperation with Royal Yugoslav Navy aviation the factory re designed the Rogozarski Brucos as a floatplane with a 140 kW Walter Six engine and floats from the Canadian Edo Aircraft Corporation This aircraft was offered to the Navy command as a floatplane for basic training At the beginning of April the single Brucos was in the hangar of the Experiment Aero Group at Zemun airport only to be flown on 10 April 1941 to the war airfield in Veliki Radinci where the first fighter brigade had been relocated The Brucos is believed to have been burnt with other aircraft to keep them from falling into enemy hands 4 Operators Edit Kingdom of YugoslaviaRoyal Yugoslav Air Force 1 aircraftSpecifications EditData from Janic Cedomir Rogozarski Brucos General characteristicsCrew 2 Length 8 10 m 26 ft 7 in Wingspan 10 00 m 32 ft 10 in Height 3 10 m 10 ft 2 in Wing area 16 00 m2 172 2 sq ft Empty weight 615 kg 1 356 lb Gross weight 872 kg 1 922 lb Powerplant 1 de Havilland Gipsy Major I four cylinder inline piston engine 96 kW 130 hp Propellers 2 bladedPerformance Maximum speed 185 km h 115 mph 100 kn 210 km h at sea level Range 840 km 520 mi 450 nmi Service ceiling 4 000 m 13 000 ft Rate of climb 2 54 m s 500 ft min See also EditZmaj Fizir FN SIM VIII Rogozarski SIM VI Rogozarski R 100Notes Edit Petroviћ O 2004 Voјni aeroplani Kraљevine SHS Јugoslaviјe Deo II 1931 1941 Beograd MVЈ Let 3 Rogozharski Brucosh Janic Cedomir Rogozarski Brucos in Serbian Aeromagazin YU Beograd BB Soft ISSN 1450 6068 Petroviћ Ogњan M 3 2004 Voјni aeroplani Kraљevine SHS Јugoslaviјe Deo II 1931 1941 in Serbian Let Flight YU Beograd Muzeј јugoslovenskog vazduhoplovstva 3 60 ISSN 1450 684X References EditGrey C G 1972 Jane s All the World s Aircraft 1938 London David amp Charles ISBN 0 7153 5734 4 Gunston Bill 1989 World Encyclopaedia of Aero Engines 2 ed Wellingborough Patrick Stephens Ltd ISBN 1 85260 163 9 Janic Cedomir O Petrovic 2011 Short History of Aviation in Serbia Beograd Aerokomunikacije ISBN 978 86 913973 2 6 Petroviћ Ogњan M March 2004 Voјni aeroplani Kraљevine SHS Јugoslaviјe Deo II 1931 1941 Let Flight in Serbian YU Beograd Muzeј јugoslovenskog vazduhoplovstva 3 60 ISSN 1450 684X Stanoјeviћ Dragoљub Chedomir Јaniћ December 1982 Zhivotni put i delo јednog velikana nasheg vazduhoplovstva svetao primer i uzor narashtaјima Mashinstvo in Serbian YU Beograd Savez inzheњera i tehnichara Јugoslaviјe 31 1867 1876 Janic Cedomir Rogozarski Brucos Aeromagazin in Serbian YU Beograd BB Soft ISSN 1450 6068 External links Edit Wikimedia Commons has media related to Rogozarski Brucos www goldenyears ukf net www airwar ru in Russian Rogozarski Brucos Retrieved from https en wikipedia org w index php title Rogozarski Brucos amp oldid 1132190574, wikipedia, wiki, book, books, library,

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