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PZL P.7

From Wikipedia, the free encyclopedia
Polish fighter aircraft
PZL P.7
PZL P.7
General information
TypeFighter
ManufacturerPZL
Statusretired
Primary userPoland
Number built149+2
History
Manufactured1932–1933
Introduction date1933
First flightOctober 1930
Developed fromPZL P.6

ThePZL P.7 was a Polishgull wing monoplanefighter aircraft designed in the early 1930s at thePZL factory inWarsaw. It was the main fighter of thePolish Air Force between 1933 and 1935. The PZL P.7 was replaced in Polish service by its follow-up design, thePZL P.11c. More than 30 PZL P.7 fighters remained in service during theInvasion of Poland, scoring several kills despite its obsolescence.

Design and development

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The history of the PZL P.7 began in 1928, when a talented designer namedZygmunt Puławski designed an all-metal, metal-covered monoplane fighter, thePZL P.1. It introduced a high gull wing whose design was called the "Polish wing" or "Pulawski wing." The P.1 was powered by aninline engine and developed a speed of 302 km/h (188 mph). But it remained a prototype because a decision was made to use a licence-producedradial engine in the Polish Air Force fighters. So the next model, thePZL P.6, flown in August 1930, was powered by theBristol Jupiter VI FH radial engine. Both aircraft were well received and it won the AmericanNational Air Races in August–September 1931.

The PZL P.6 did not enter production because a more advanced variant, thePZL P.7, was in development. The first prototype was basically a P.6 with a more powerful Bristol Jupiter VII.F engine. The addition of asupercharger improved performance at higher altitudes. The prototype P.7/I was first flown in October 1930 byBolesław Orliński.[1] Initially, engine cylinders had individual cylinder fairings. After numerous changes, most noticeably the addition of a wideTownend ring to the engine, and a higher aspect tail, the second prototype P.7/II which had been completed in autumn 1931, was accepted for production with the designationP.7a. The wing was redesigned with slightly increased span, taken from thePZL P.8, and shorterailerons were used, and structural changes eliminated external ribs from the wing upper surfaces.[1] P.7a production began in mid-1932 and the last of the 149 (plus two prototypes) were completed in 1933.[1] ThePolish Air Force received the P.7a in 1933.

Puławski continued to develop the basic design by adding more powerful engines, which resulted in thePZL P.11. Puławski preferred inline engines and also designed the slimmerP.8 and the related P.9 with inline engines but he died in an air accident in March 1931, and these were cancelled. The P.11 became the standard Polish fighter while thePZL P.24 was developed in parallel as an export variant in 1932.

Technical features

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The all-metal,duralumin metal-covered strut braced gull-wingmonoplane was conventional in layout, and used a conventional fixed undercarriage with a tail skid. The two-spar trapezoid wing was thinner by the fuselage and was covered with a ribbed Wibault type duralumin sheet (although the upper surfaces were smooth) and braced by two struts on each side. The fuselage was framed in a front section and semi-monocoque in mid- and tail sections, oval in cross-section. In keeping with the period, the pilot's cockpit was open with a windshield. Armament was two 7.92 mm (0.312 in) machine guns mounted on the fuselage sides which replaced the initially fitted 7.7 mm (0.303 in) Vickers E which were re-bored. The aircraft was powered by a 360 to 390 kW (480 to 520 hp)Bristol Jupiter VII F radial engine fitted with aTownend ring and two-blade propeller. A main 290 L (64 imp gal; 77 US gal) fuel tank in the fuselage, behind the engine could be dropped in case of a fire emergency. The second fuel tank was 7 L (1.5 imp gal; 1.8 US gal).

Operational history

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The PZL P.7a entered service in spring 1933, replacing PWS-A (a licence-builtAvia BH-33) andPWS-10 fighters. Consequently, thePolish Air Force became the first air force entirely equipped with all-metal monococque fighters.[1][2] When the P.7 entered service, it was comparable to contemporary designs, but due to rapid progress, it was obsolete by 1939. From 1935, thePZL P.11 replaced the P.7 in most combat units, but was only a slight improvement, while the P.7as were relegated to air schools.

At the outbreak ofWorld War II on 1 September 1939, the Polish Air Force still had 30 PZL P.7a fighters in combat units. A further 40 were with flying schools, and 35 were in reserve or undergoing repairs for a total of 106 aircraft. The P.7as were used by three squadrons, each equipped with 10 aircraft. ThePursuit Brigade's123rd Squadron was deployed nearWarsaw, while the151st and the162nd Squadrons were attached to Army units. Despite being obsolete, they engaged the German attackers during theinvasion of Poland. In addition to combat units, at least 18 P.7a fighters were used by improvised units from air bases inDęblin and Ułęż.

Although the P.7 was more manoeuvrable than their opponents and could operate from short or rough fields, almost all the German aircraft were faster, and worse, the Polish aircraft and their engines were worn out from intensive service use. Their two machine guns was also inadequate and jammed frequently while only some replaced the vintage Vickers with the betterPWU FK wz.33 [pl].[1] Pilots flying the P.7a claimed to have shot down seven German aircraft (twoHeinkel He 111s, twoDornier Do 17s, oneHenschel Hs 126 and twoMesserschmitt Bf 110s), against 22 losses.

Most were destroyed in 1939, in combat or on the ground, but around a dozen were withdrawn toRomania, but were not used in combat there. Some captured P.7s were used by the Germans for training. Several aircraft were captured by the Soviets and were also assigned to training units.

Variants

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P.6
precursor design prototypes with lower rated engine; two built.[3]
P.7/I
First prototype.
P.7/II
Second prototype equipped withTownend ring.
P.7a
Serial-built version.

Operators

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Germany
  • Luftwaffe operated few captured aircraft for training.
 Poland
 Romania
 Soviet Union

Specifications (PZL P.7a)

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Data from Polish Aircraft 1893–1939[3]

General characteristics

  • Crew: One
  • Length: 7.16 m (23 ft 6 in)
  • Wingspan: 10.3 m (33 ft 10 in)
  • Height: 2.75 m (9 ft 0 in)
  • Wing area: 17.2 m2 (185 sq ft)
  • Airfoil:root: IAW-72 (Bartel 37/IIa) (6.5%);tip: IAW-72 (Bartel 37/IIa (8%))[5]
  • Empty weight: 1,010 kg (2,227 lb)
  • Gross weight: 1,409 kg (3,106 lb)
  • Fuel capacity: 250 L (55 imp gal; 66 US gal) in a jettisonable fuselage tank
  • Powerplant: 1 ×Polish Skoda Works Jupiter VIIF 9-cylinder air-cooled radial piston engine, 393 kW (527 hp) for take-off
362 kW (485 hp) normal rating
  • Propellers: 2-bladed Szomański fixed-pitch wooden propeller

Performance

  • Maximum speed: 317 km/h (197 mph, 171 kn) at 4,000 m (13,000 ft)
308 km/h (191 mph) at 2,000 m (6,600 ft)
276 km/h (171 mph) at sea level
  • Stall speed: 102 km/h (63 mph, 55 kn)
  • Range: 560 km (350 mi, 300 nmi)
  • Service ceiling: 8,275 m (27,149 ft)
  • Time to altitude: 1,000 m (3,300 ft) in 1 minute 38 seconds
3,000 m (9,800 ft) in 5 minute 3 seconds
  • Wing loading: 81.8 kg/m2 (16.8 lb/sq ft)
  • Power/mass: 0.2652 kW/kg (0.1613 hp/lb)

Armament

See also

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Related development

Aircraft of comparable role, configuration, and era

References

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Wikimedia Commons has media related toPZL P.7.

Notes

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  1. ^abcdeMorgała, Andrzej (2003):Samoloty wojskowe w Polsce 1924–1939. Warszawa: Bellona.ISBN 8311093199, pp. 48–54 (in Polish)
  2. ^Murphy and McNiece 2009,pp. 18–19.
  3. ^abCynk, Jerzy B. (1971).Polish Aircraft 1893–1939. London: Putnam. pp. 147-154.ISBN 978-0-370-00085-5.
  4. ^Kotelnikov, Vladimir. "Lotnictwo w wojnie polsko-sowieckiej we wrześniu 1939 r.(in Polish)"Lotnictwo Wojskowe, May 1999.
  5. ^Lednicer, David."The Incomplete Guide to Airfoil Usage".m-selig.ae.illinois.edu. Retrieved16 April 2019.

Bibliography

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  • Cynk, Jerzy B.History of the Polish Air Force 1918–1968. Reading, Berkshire, UK: Osprey Publishing Ltd., 1972.
  • Cynk, Jerzy B.Polish Aircraft, 1893–1939. London: Putnam & Company Ltd., 1971.ISBN 0-370-00085-4.
  • Eberspacher, Warren A. and Jan P. Koniarek.PZL Fighters Part One - P.1 through P.8. (International Squadron Monograph 2). St. Paul, MN: Phalanx Publishing Co., Ltd., 1995.ISBN 1-883809-12-6.
  • Glass, Andrzej.Polskie konstrukcje lotnicze 1893–1939 (in Polish: "Polish aviation constructions 1893–1939"). Warszawa, Poland: WKiŁ, 1977. no ISBN.
  • Glass, Andrzej.PZL P.7: Cz.1. Gdańsk, Poland: AJ Press, 2000.ISBN 83-7237-080-X.
  • Kopański, Tomasz J.PZL P.7: Cz.2. Gdańsk, Poland: AJ Press, 2001.ISBN 83-7237-081-8.
  • Murphy, Justin D. and Matthew A. McNiece.Military Aircraft, 1919–1945: An Illustrated History of their Impact. Santa Barbara, California: ABC-CLIO, 2009.ISBN 1-85109-498-9.
PZL aircraft
PZL - up to 1939
(Państwowe Zakłady Lotnicze)
PZL:
CSS / WSK-Okęcie
/ PZL Warszawa-Okęcie
PZL:
Other:
WSK-Mielec / WSK PZL-Mielec
/ PZL Mielec
(Polskie Zakłady Lotnicze)
PZL:
Other:
WSK-Świdnik / WSK PZL-Świdnik / PZL-Świdnik
PZL:
Other:
WSK PZL-Krosno
Szybowcowy Zakład Doświadczalny
/ PZL Bielsko-Biała / Allstar PZL Glider
Authority control databases: NationalEdit this at Wikidata
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