Lublin R-XX
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| Lublin R-XX | |
|---|---|
| Type | Torpedo bomber floatplane |
| Manufacturer | Plage i Laśkiewicz |
| Maiden flight | 8 April, 1935 |
| Retired | 1937 |
| Status | Prototype |
| Primary user | Polish Navy |
| Number built | 1 |
The Lublin R-XX was the Polish torpedo bomber floatplane, designed in the early 1930s in the Plage i Laśkiewicz factory in Lublin. It remained a prototype.
Contents |
[edit] Design and development
In 1930 the Polish Ministry of Defence announced a contest for a torpedo-bomber floatplane for the Polish Navy. Plage i Laśkiewicz works proposed first a floatplane variant F.VIIW of a licence-built bomber (developed from a passenger plane) Fokker F.VII, but it was not built. It also proposed a floatplane variant of single-engined Lublin R-VIII biplane bomber. In a course, three R-VIIIs were converted to floatplanes and given to the Navy, but they did not meet all demands, for they were obsolete, slow and could not carry torpedoes. Then Plage i Laśkiewicz proposed quite modern twin-engined plane Lublin R-XX, the main designer of which was Jerzy Rudlicki. The last design won the contest in 1932, besting PZL-18 and PWS-62 designs, and a prototype was ordered. It was initially planned to build a series of 9.
In 1934 the prototype was built and on 22 June transported to Puck - a base of the Naval Aviation Squadron (MDLot). It appeared there, that it was tail-heavy on water, and it demanded some modifications, like lengthening engine nacelles towards front. It first flew on 8 April 1935[1] (some sources: 10 April[2]). Initially the plane was kept in secret. The design was found satisfactory, but it had also faults, like moving of centre of gravity during flight and low fuselage rigidity. The prototype was modified then and returned from the factory for further trials on 30 October 1935.
In early 1935 an improved variant R-XXA was developed. It had more streamlined fuselage, covered machine gun turrets with 6 machine guns, smaller span of 23.65 m and stronger engines 750 hp Pegasus III. The Polish Navy ordered 6 production aircraft in the beginning of 1935, with planned deliveries by April 1937, and Plage i Laśkiewicz prepared to build the R-XXA prototype. However, the factory at that time was about to bankrupt (caused by a policy of Ministry of Defence, refusing to buy Lublin R-XIIIf planes), and on 23 November 1935 the Navy Headquarters broke off an order for R-XXA due to long development.
After nationalization of the bankrupt Plage i Laśkiewicz works in 1936, as the LWS, the R-XXA design was taken over as the LWS-1. However, its development was soon canceled in mid-1936, because the factory proposed a floatplane variant LWS-5 of slightly more modern LWS-6 Żubr bomber. This design was not completed as well, and the Polish Navy remained without torpedo bombers (there were finally ordered six CANT Z.506 in Italy, but only one unarmed was delivered by the outbreak of the war).
The only R-XX prototype was used in the MDLot with a number 806 until September 1937, when it was written off, then scrapped in 1938. It was planned to use floats for LWS-5 prototype.
There was also a preliminary design of a medium bomber R-XXB, from 1934-1935. It was to have a streamlined fuselage and covered gun turrets, similar to R-XXA. Main difference was a fixed conventional landing gear with wide covers and a single tailfin. It was to carry 600 kg bombs (some sources - 1500 kg)[1]. It was less modern, than LWS-6 Żubr (PZL.30) and PZL.37 Łoś and the plane, redesignated later as LWS-1/II, was not built.
[edit] Variants
- R-XX
- Prototype.
- R-XXA
- Improved version with streamlined fuselage, covered machine gun turrets, smaller span and stronger Pegasus III engines. Six were ordered, none built.
- R-XXB
- Preliminary design of a medium bomber.
[edit] Operators
[edit] Specifications (R-XX)
[edit] Description
Mixed construction low-wing cantilever monoplane, two-engine, conventional in layout. A fuselage was square in cross-section, made of a steel frame, canvas-covered (duralumin-covered in front). Wings of wooden construction, two-spar, plywood-covered. Twin strutted tail. Crew of five: in a glazed nose a bombardier-gunner, then two pilots, sitting side by side in an open cockpit. In mid-fuselage a radio operator and an upper gunner. Two Short metal floats. Four-blade wooden propellers, later three-blade metal ones. Two fuel tanks 1680 l in wings. Armament: four 7.9 mm Vickers F machine guns on ring mountings in fuselage nose and in a dorsal position. According to some sources, also one underbelly machine gun. Bomb load: up to 1000 kg[3] (other sources - 600 kg[2]) or 750 kg torpedo.
Data from Glass, A. (1977)
General characteristics
- Crew: 5
- Length: 15.9 m ()
- Wingspan: 25.4 m ()
- Height: 6.1 m ()
- Wing area: 75 m² (ft²)
- Empty weight: 4000 kg ()
- Loaded weight: 6000 kg ()
- Useful load: 2000 kg ()
- Powerplant: 2× PZL Bristol Pegasus IIL2 air-cooled 9-cylinder radial engines, 635 hp () each
Performance
- Maximum speed: 250 km/h
- Cruise speed: 210 km/h
- Stall speed: 80 km/h ()
- Range: 500 km ()
- Service ceiling 3500 m ()
- Rate of climb: 2.8 m/s [1]or 1.8 m/s[2] ()
- Wing loading: 80 kg/m² ()
Armament
- 5 movable 7.9 mm Vickers F machine guns
- 1000 kg bombs or a 750 kg torpedo
[edit] See also
Comparable aircraft
[edit] References
- ^ a b c Lublin R-XX (LWS-1) at Samoloty 1,5]
- ^ a b c Morgała, Andrzej: Samoloty w polskim lotnictwie morskim, WKiŁ, Warsaw, 1985, ISBN 83-206-0478-8
- ^ Glass, A. (1977)
- Andrzej Glass: "Polskie konstrukcje lotnicze 1893-1939" (Polish aviation constructions 1893-1939), WKiŁ, Warsaw 1977, p. 162-164 (Polish)
- Lublin R-XX (LWS-1) at Samoloty 1,5
[edit] External links
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