Rogožarski SIM-XII-H

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Rogožarski SIM-XII-H
300px
Role Trainer floatplane
National origin Yugoslavia
Manufacturer Prva Srpska Fabrika Aeroplana Živojin Rogožarski AD.
Designer Sima Milutinović
First flight 7. February 1938
Introduction 1939
Retired 1941
Status inactive
Primary user Yugoslav Royal Air Force
Produced from 1939 to 1941
Number built 9[1]
Developed from Rogožarski SIM-X

The Rogožarski SIM-XII-H (Serbian Cyrillic:Рогожарски СИМ-XII-Х) was a Yugoslav trainer single-engine floatplane, with two floats designed in 1938. It was designed and built at the Rogožarski factory in Belgrade.

File:SIM-XII i SIM-XIV.JPG
Seaplanes Rogožarski SIM-XII-H (left) and SIM-XIV-H (right) (Kumbor 1938)
File:De Havilland Gipsy Six.jpg
Engine installed in aircraft Seaplanes Rogožarski SIM-XII-H

Design and development

The YRAF was unsuccessfully trying to choose the most appropriate seaplane for pilot training so they turned to the Rogožarski factory for help in 1937 and ordered the seaplane school project to be made that would fit in its characteristics to the school plane SIM-X. Since it was not possible to make a simple modification (adaptation of existing aircraft SIM-X) for installation of EDO floats, chief designed Sima Milutinović fitted the plane with a more powerful engine Walter Major 6 190 hp, leading to an increase in aircraft size. Thus, this new high-flying school plane with two floats represented an entirely new plane, designated SIM-XII-H. During 1937, the project went into realization stage, and as early as the end of the year the prototype was ready for testing.[2] The test flight was conducted on February 7, 1938, by test pilot Ivan Koroša in hydro-base Divulje. After the flight tests had achieved satisfactory results, the first batch of aircraft was ordered, which were delivered in mid-1939.[3]

Aircraft SIM-XII-H, a supported two-seat high-flying plane, with engine Walter Major 6 (190 hp), of predominantly wooden construction, with an elliptical cross-section of fuselage entirely made of wood and covered with plywood, wings as the supporting structure made of wood covered with fabric, with rounded ends. On each side, the wings are supported by a pair of inclined struts attached to the fuselage. The fuel tank was located in the central part between the wings, that is, at their junction. The first series of aircraft had two (a pair of) EDO floats installed (EDO Float Model 47).

Operational history

As for experience with the use of aircraft SIM-XII-H, which was called by pilots and technical staff of the aircraft "little SIM", were very positive and the navy command (Royal Maritime Navy) signed a contract with Rogožarski factory on July 15, 1940 for the second series of these plane (4 aircraft) with the difference that these seaplanes were equipped for instrument, or, "blind" flying. Rogožarski delivered these aircraft in five months but without floats as the delivery from Canada was delayed for several months. Upon the agreement reached between the Rogozarski factory an the Navy command, the design and development of domestic aircraft floats was launched, unfortunately this project did not reach completion due to the outbreak of April war . In the pre-war period two SIM-XII-H aircraft were in accidents both in Boka Kotorska in 1940. Both aircraft were designated for disposal, so the Navy Command requested approval to install the floats from these planes onto new aircraft ( onto the 2nd series of SIM-XII-H ) considering that these planes were equipped with instruments for instrumental ("blind") flying. When the approval was given, the floats were installed into new planes, so the aircraft in the second series were enabled for use before the war broke out.[4]

Operators

 Kingdom of Yugoslavia

Specifications

Data from Станојевић, Д.; Јанић, Ч; (12/1982.).[5]

General characteristics

  • Crew: 2
  • Length: 7.50 m (24 ft 7 in)
  • Wingspan: 11.00 m (36 ft 1 in)
  • Height: 2.96 m (9 ft 9 in)
  • Wing area: 2,050 m2 (22,100 sq ft)
  • Empty weight: 635 kg (1,400 lb)
  • Gross weight: 920 kg (2,028 lb)
  • Powerplant: 1 × Walter Major 6, 6-cylinder line,, 140 kW (190 hp)
  • Propellers: 2-bladed

Performance

  • Maximum speed: 208 km/h (129 mph; 112 kn) 212 at sea level
  • Range: 840 km (522 mi; 454 nmi)

See also

Aircraft of comparable role, configuration and era
Related lists

Notes

  1. ↑ Петровић, O. (2004). Војни аероплани Краљевине СХС/Југославије (Део II: 1931–1941.). Београд: МВЈ Лет 3.
  2. ↑ Станојевић, Драгољуб.; Чедомир Јанић (12/1982.). "Животни пут и дело једног великана нашег ваздухопловства - светао пример и узор нараштајима" (in (Serbian)). Машинство (YU-Београд: Савез инжењера и техничара Југославије) 31: 1867 - 1876.
  3. ↑ http://airserbia.com/vvkj/index.php?str=avioni&av=75
  4. ↑ Петровић, O. (2004). Војни аероплани Краљевине СХС/Југославије (Део II: 1931–1941.). Београд: МВЈ Лет 3
  5. ↑ "Животни пут и дело једног великана нашег ваздухопловства - светао пример и узор нараштајима" (in (Serbian)). Машинство (YU-Београд: Савез инжењера и техничара Југославије) 31: 1867 - 1876.

References

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External links

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