PZL P.11
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PZL P.11 | |
---|---|
PZL P.11c | |
Type | Fighter |
Manufacturer | PZL |
Designed by | Zygmunt Pulawski |
Maiden flight | August 1931 |
Retired | 1945 |
Primary users | Poland Romania |
Number built | 325 |
Developed from | PZL P.7 |
The PZL P.11 was a Polish fighter aircraft, designed in early 1930s by PZL in Warsaw. It was briefly considered to be the most advanced fighter design in the world. The PZL P.11 served as Poland's primary fighter defence in the Polish campaign but by that point was outdated due to rapid advances in aircraft design.
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[edit] Design and development
The history of the PZL P.11 started in 1929, when a talented designer, Zygmunt Pulawski, designed an all-metal, metal-covered monoplane fighter. While most of the world's forces were still using biplanes, the new P.1 used a high-mounted gull wing to give the pilot an excellent view. A second prototype, the P.6, was completed the next year. The design generated intense interest around the world, the layout becoming known as the "Polish wing" or "Pulawski wing". A further improvement, the PZL P.7, was built for the Polish Air Force in a series of 150.
After designing the P.7, Pulawski started further variants with larger engines, leading eventually to the P.11. The first prototype P.11 flew in August 1931, after Pulawski's death in an air crash. It was followed by two slightly modified prototypes. The first variant ordered by the Polish Air Force was the P.11a, considered an interim model and built in a series of 30. Otherwise similar to the P.7, it mounted the 575 hp (429 kW) Bristol Mercury IV S2 radial engine produced in Poland under licence.
The final variant for the Polish airforce, the P.11c had a new, refined fuselage, with the engine lowered in the nose to give the pilot a better view. The central part of wings was also modified. Production of the P.11c started in 1934 and 175 were produced. The first series of approximately 50 P.11c aircraft were fitted with Mercury V S2 of 600 hp (447 kW), the rest with Mercury VI S2 of 630 hp (470 kW).
Such limited production may appear irresponsible on the part of the Polish government, with the Red Army aviation reaching into thousands and Germany ramping up production at an unprecedented scale. Even without the new WP2 plant at Mielec, the PZL works could produce at least 10 fighters every month. However, the Lotnictwo Wojskowe (Military Aviation) command was still studying different concepts of the use of fighters and bombers, while the Polish design bureaus were developing very advanced designs. The untimely death of Zygmunt Pulawski also complicated the matter.
Apart from Poland, Romania showed interest in the new design. Even before the P.11a, 50 aircraft designated P.11b were produced for the Romanian Air Force and delivered in 1932. They were fitted with Gnome-Rhone 9Krsd Mistral 595 HP engines, otherwise they were similar to the P.11a. After the P.11c had been developed, the Romanians decided to buy a licence and produce the new model at IAR factory. As a result, from 1936 IAR built 70 aircraft as the IAR P.11f with the slightly updated 9Krse of 610 hp. The Romanians then produced another Polish fighter, the PZL P.24, developed from the P.11 exclusively for export. Some other countries were interested in buying the P.11, but finally Bulgaria, Greece and Turkey bought the P.24 instead.
When the P.11 entered service in 1934 it was arguably the most advanced fighter in the world. However, due to the quick progress in aircraft technology, they were obsolete by 1939, overtaken by cantilever designs with retractable landing gear such as the Soviet Polikarpov I-16 and Nazi German Bf-109. Unfortunately, they remained the only Polish fighters in service, totalling about 185, distributed within six air regiments and the aviation school in Deblin. Although they were aware that the P.11 was outdated, the Polish Air Force had pinned their hopes on the new PZL P.50 Jastrzab, which suffered extended delays. When it became apparent that the P.50 would not be in widespread service in time for a war that was clearly looming, consideration was given to producing an updated version with the 840 hp (626 kW) Mercury VIII and an enclosed cockpit, known as the P.11g Kobuz. Only the prototype of the P.11g with a maximum speed increase to a still-slow 390 km/h (~240 mph)was flown before the war, in August 1939.
[edit] Technical description
The aircraft was conventional in layout, with high wings, all-metal, metal-covered. The cockpit was open. An internal fuel tank in a hull could be dropped in case of fire emergency. The armament was two 7.92mm machineguns on hull sides, some 1/3 of P.11c had additional two machineguns in wings. P-11c could carry four small 12.5 kg bombs (P.11a could not). The radial engines used were: P-11a: Bristol Mercury IV S2 (normal: 525 hp, maximum: 575 hp); P-11b: Gnome-Rhone 9Krsd (550 hp, max: 595 hp), P.11c: Bristol Mercury V S2 (565 hp, max: 600 hp) or Mercury VI S2 (590 hp, max: 630 hp), P.11f: Gnome-Rhone 9Krse (560 hp, max: 610 hp).
[edit] Operational history
At the outbreak of the Second World War, on 1 September 1939, the Polish Air Force had 109 PZL P.11c and 20 P.11a (and 30 P.7a) in combat units. A further 43 P.11c aircraft were in reserve or undergoing repairs. Only a third of P.11c were armed with four machineguns, the rest had only two, even fewer had a radio. The P.11 were used in 12 squadrons, each with 10 aircraft (two squadrons constituted a group, in Polish: dywizjon). Two groups - four squadrons - were in the Pursuit Brigade deployed around Warsaw, the rest were assigned to Armies. All of them took part in defense during the Invasion of Poland. Apart from combat units, several P.11 aircraft, including a prototype P.11g, were used in improvised units at air bases.
By 1 September 1939, the fighter squadrons had been deployed to remote airfields, so they were not bombed by the Germans. During the Polish campaign, the P.11 fought against more modern German bombers and fighters. Not only were the German Messerschmitt Bf 109 and Bf 110 faster and better armed, but also most German bombers were faster. Since the P.11 fighters were intensively used, their maximum speed was even lower than the theoretical 375 km/h. The P.11a were in an even worse condition. Another serious deficiency was their small number which meant that missions involving groups larger than about 20 planes were rarely accomplished and reserve machines were practically unavailable.
On the other hand, the Polish planes had better manoeuvrability and because of their design, had much better vision from the cockpit than the German planes. The P.11 had a strong construction, good rate of climb and could operate from short fields, even rough ones. It was also of a very durable construction and could dive at up to 600 km/h without risk of the wings falling apart. Theoretically the only limit in manoeuvres was the pilot's ability to sustain high g forces. Despite the German superiority, the P.11 managed to shoot down a considerable number of German aircraft, including fighters, but suffered heavy losses as well. The exact numbers are not fully verified, but it appears that at least one German plane shot down for each P.11 lost (a figure of 141 German planes is often given as compared with 118 planes lost).
At dawn on 1 September, Capt. Mieczysław Medwecki flying a PZL P.11c was shot down by a German Ju 87, having the dubious honor of becoming the first aircraft shot down in the Second World War. The first Allied air victory was achieved 20 minutes later by Medwecki's wingman, Wladyslaw Gnys who shot down two Dornier Do 17s with his P.11c. The PZL P.11c was also the first airplane to successfully ram an enemy plane in the Second World War. The first large air battle of the Second World War took place in the early morning of 1 September over the city of Nieporet in North-Western Poland when a German bomber group of about 70 Heinkel He 111 and Dornier Do 17 was intercepted by some 20 P-11 and 10 P-7 fighters and had to abandon their mission to Warsaw.
Most of the P.11s were destroyed in 1939 while 36 were flown to Romania and taken over by the Romanian Air Force. Due to their obsolescence, these veteran aircraft were not used in combat; only a small number was used for training while the rest were dismantled for spare parts. Some aircraft were used by the Germans for training. Two PZL P.11s were captured by the Red Army and used for testing. One landed in Hungary (near the town of Hajdúböszörmény)and was used as a glider towing plane by the University of Technology in Budapest.
[edit] Survivors
The sole surviving plane is on display in the Polish Aviation Museum in Cracow.
[edit] Operators
- Hungary: One PZL P.11a evacuated in September 1939
- Poland
- Romania
- Latvia
- Soviet Union
[edit] Specifications (P-11c)
General characteristics
- Crew: 1
- Capacity: Fighter
- Length: 7.55 m (24 ft 9 in)
- Wingspan: 10.72 m (35 ft 2 in)
- Height: 2.85 m (9 ft 4 in)
- Wing area: 17.9 m² (167 ft²)
- Empty weight: 1,147 kg (2,529)
- Loaded weight: 1,650 kg (3,638 lb)
- Powerplant: 1× Bristol Mercury IV S2 or Mercury VI radial engine, 470 kW [1] (630 hp)
Performance
- Maximum speed: 375 km/h (233 mph)
- Range: 550 km (341 mi)
- Service ceiling: 8,000 m (26,246 ft)
- Rate of climb: 12.4 m/s (2,440 ft/min)
Armament
- Guns: 2-4× 7.92 mm (0.312 in) machine guns
- Bombs: 50 kg (110 lb)
[edit] References
- ^ Note: the horsepower data of engines differ in publications.
- Taylor, John W. R. "PZL P.11." Combat Aircraft of the World from 1909 to the present. New York: G.P. Putnam's Sons, 1969. ISBN 0-425-03633-2.
- Winchester, Jim. "PZL P.11." Aircraft of World War II: The Aviation Factfile. Kent, UK: Grange Books plc, 2004. ISBN 1-84013-639-1.
[edit] External link
- Recorded sound of the Bristol Mercury VI engine used in PZL P.11c (mp3 format)
- PZL P.11 "Walkaround" photos
[edit] Related content
Related development
Comparable aircraft
Dewoitine D.371 - Loire 46 - Ikarus IK-2 - Polikarpov I-15
Designation sequence
PZL-6 - PZL P.7 - PZL P.8 - PZL P.11 - PZL-12 - PZL-19
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