PZL.46 Sum

infobox Aircraft
name = PZL.46 Sum
type = Light bomber and reconnaissance aircraft
manufacturer =Państwowe Zakłady Lotnicze


caption =
designer =
first flight = August 1938
introduced =
retired =
status = Prototype
primary user = Polish Air Force
produced = 1939
number built = 2 prototypes
unit cost =
variants with their own articles =

PZL.46 Sum was a projected light bomber of the Polish Air Force before World War II, that remained a prototype.

Design and development

The PZL.46 Sum ("wels catfish") was designed by Stanisław Prauss in the PZL works as a successor to standard Polish light bomber and reconnaissance plane, the PZL.23 Karaś, also of Prauss' design. First sketches were made in 1936. In order to test new features, like double tail fins and retractable underbelly bombardier gondola, a single modified PZL.23, designated PZL.42 was built and tested in 1936.

The first prototype of PZL.46 Sum flew in August 1938. It shared only a general composition with Karaś, its fuselage was much more aerodynamically refined and wings had thinner profile. Initially it was intended to use retractable landing gear, but since the Polish industry did not produce proper landing gear, a fixed one was used. In November-December 1938 the prototype was shown at the Paris Air Show. In May 1939 the second similar prototype was flown (PZL.46/II).

Tests proved, that Sum was a successful design, with much better performance, than Karaś. The only major faults were with a mechanism of retracting of the underbelly gondola (the gondola for a bombardier, with a machine gun at the rear, was a feature copied from Karaś, where it was a fixed one. It was rare feature in light bombers' construction and its usefulness was questionable, as it reduced performance).

In March 1939 the PZL.46 was ordered for a serial production. The Polish Air Force planned to buy 160 aircraft in a variant PZL.46A. First were to be delivered in early 1940. Only some parts were produced by the German invasion of Poland in September 1939.

The third prototype was in construction in the summer of 1939, it was to be an export variant PZL.46B, powered with Gnome-Rhône 14N21 engine. Bulgaria, using PZL.43 Karaś bombers, showed an interest in the new design and made a preliminary order for 12 aircraft, uncompleted due to war.

Stanisław Prauss made also a preliminary design of smaller development variant PZL Łosoś, which was to be a two-seater dive bomber with 1600 hp Hispano-Suiza 12Z inline engine and retractable landing gear, without underbelly gondola.

Operational history

During World War II, the first prototype was left in Warsaw, because of a landing gear damage. On 5 September 1939 the second prototype was evacuated from Warsaw to Lwów, then on 17 September to Bucharest in Romania, where it was interned. On 26 September 1939, under pretext of delivering the plane to IAR factory in Brasov, it was flown by Riess with other three crewmen (including Witold Urbanowicz) from Romania to besieged Warsaw. The crew delivered orders from the Polish C-in-C Edward Rydz-Śmigły for the commander of Warsaw defence Juliusz Rómmel. On 27 September 1939, with most of the Polish territory occupied by Germans or Soviets, it flew to Kaunas in Lithuania. The plane was interned and left there and later captured there and tested by the Soviets.

Operators

;POL
* Polish Air Force

Specifications

Technical design

The aircraft was conventional in layout, mid-wing all-metal cantilver monoplane, metal-covered. A fuselage was semi-monocoque, oval in cross-section. Double tail fins. The crew consisted of three: pilot, observer/bombardier and a rear gunner. A combat station of bombardier was in a gondola underneath a fuselage, where he also operated an underbelly machine gun. The gondola could be retracted into a fuselage to decrease drag. The fixed undercarriage had aerodynamic teardrop covers. Radial engine, PZL-built 840 hp Bristol Pegasus (PZL Pegaz) XXB (maximum power 940 hp), under NACA cover. Three-blade metal propeller Hamilton Standard. Fuel tanks: 750 l in a central wing section.

aircraft specification
jet or prop?=prop
plane or copter?=plane

crew=3
capacity=
length main=10.5 m
length alt=34.4 ft
span main=14.6 m
span alt=48.9 ft
height main=3.3 m
height alt=10 ft 10 in
area main=31.5 m²
area alt=103.3 ft²
empty weight main=1,995 kg
empty weight alt=4,398 lb
loaded weight main=3,550 kg
loaded weight alt=7,826 lb
useful load main=1,555 kg
useful load alt=3,428 lb
max takeoff weight main=
max takeoff weight alt=

engine (prop)= PZL-Bristol Pegasus XXB;
type of prop=9-cylinder radial engine
number of props= 1
power main= 940 hp
power alt=

max speed main= 425 km/h
max speed alt=264 mp/h
cruise speed main=
cruise speed alt=
never exceed speed main=
never exceed speed alt=
stall speed main=110 km/h
stall speed alt=68 mph
range main=1,300 km
range alt=807 miles
ceiling main=7,700 m
ceiling alt=25,262 ft
climb rate main=6 m/s
climb rate alt=19.6 ft/s
loading main=112 kg/m²
loading alt=
thrust/weight=
power/mass main=
power/mass alt=

armament=
*6 x machine guns:
**2 x 7.92 mm FK wz.36 fixed in nose with synchronising gear;
**2 x 7.92 mm FK wz.36 fixed in wings;
**1 x 7.92 mm karabin maszynowy obserwatora wz.37 in rear upper station (serial planes were to have 2)
**1 x 7.92 mm karabin maszynowy obserwatora wz.37 in rear underbelly station;
*600 kg bombs under wings.

References

* Andrzej Glass: "Polskie konstrukcje lotnicze 1893-1939" ("Polish aviation constructions 1893-1939"), WKiŁ, Warsaw 1977 (Polish language, no ISBN)

External links

* [http://translate.google.com/translate?hl=en&sl=ru&u=http://www.airwar.ru/enc/bww2/pzl46.html&sa=X&oi=translate&resnum=8&ct=result&prev=/search%3Fq%3DPZL.23%2BKaras%26start%3D80%26hl%3Den%26ie%3DUTF-8%26sa%3DN PZL-46 Sum with photos and drawings] (translated page from Ugolok Neba)

ee also

aircontent
related=
PZL.23 Karaś

similar aircraft=
Heinkel He 70 -
Fairey Battle -
A-35 Vengeance -
Mitsubishi Ki-30 -
DAR-10

sequence=
PZL.42 -
PZL.43 -
PZL.44 -
PZL.45 -PZL.46 -
PZL.48 -
PZL.50 -
PZL.54

lists=

* List of bomber aircraft