Maximální vzletová hmotnost: Maximum Take-off Weight:
11500 kg
25353 lb
Rozpětí: Wingspan:
18,20 m
59ft 8,53in
Délka: Length:
14,40 m
47ft 2,92in
Výška: Height:
4,80 m
15ft 8,97in
Plocha křídla: Wing Area:
53,00 m2
570.49 ft2
Plošné zatížení: Wing Loading:
? kg/m2
? lb/ft2
Pohon: Propulsion:
Kategorie: Category:
pístový
piston
Počet motorů: Number of Engines:
2
Typ: Type:
PZL Hercules o výkonu 1030 kW/1400 k nebo Gnôme-Rhône 14N 50/51 o výkonu 1030 kW/1400 k třílistá stavitelná vrtule
PZL Hercules, power 1381 hp, or Gnôme-Rhône 14N 50/51, power 1381 hp three-bladed variable-pitch propeller
Objem palivových nádrží: Fuel Tank Capacity:
?
?
Výkony: Performance:
Maximální rychlost: Maximum Speed:
520 km/h v ? m
323.1 mph in ? ft
Cestovní rychlost: Cruise Speed:
? km/h v ? m
? mph in ? ft
Rychlost stoupání: Climb Rate:
? m/s
? ft/min
Čas výstupu na výšku: Time to Climb to:
? min do ? m
? min to ? ft
Operační dostup: Service Ceiling:
? m
? ft
Dolet: Range:
2000 km
1242.7 mi
Maximální dolet: Maximum Range:
3000 km
1864.1 mi
Výzbroj: Armament:
1x kanon Hispano-Suiza ráže 20 mm, Oerlikon ráže 37 mm nebo 4 kulomety ve hřbetní věži 1x pohyblivý kulomet ve výsuvném břišním střelišti 2x pohyblivý kulomet v přídi
~3000 kg pum
1x 20 mm Hispano-Suiza or 37 mm Oerlikon cannon or four machine guns in the dorsal turret 1x flexible machine gun in the retractable ventral position 2x flexible machine gun in the nose
~6600 lb of bombs
Uživatelské státy: User States:
-
-
Poznámka: Note:
-
-
Zdroje: Sources:
Morgala, Andrzej. Samoloty wojskowe w Polsce 1924-1939. Dom Wydawniczy Bellona, Warszawa 2003. ISBN 83-11-09319-9. www.samolotypolskie.pl
It was a five-seater, twin-engine, single-plane heavy bomber with a fully retractable stern-type landing gear and a double SOP.
It was planned as a successor to the Loś type. It was generally characterized by higher performance. These were to help him mainly more powerful power units with an output of about 1350 hp (Loś - 918 hp). The planned top speed of around 520 km/h was 75 km/h higher than its predecessor and it was expected that the climb and access would increase. A larger supply of fuel was to extend its range up to 3,000 km.
This aircraft was also planned for the then relatively large main armament. This was primarily to consist of one movable 20 mm cannon, located in a rotating tower on the back of the fuselage. Two designs of turret were considered. The first was to be two-thirds retractable with a convex ceiling and the second fully retractable with a ceiling shaped according to the cross-section of the fuselage. In the second case, it would not protrude above the contour of the butt at all when retracted, which would be a more advantageous solution from the aerodynamic point of view. Another armament was to consist of four movable machine guns. One shooting position was located in the glass bow. Another shooting post was to be located at the bottom of the fuselage, approximately below the upper turret. It is not known whether they should have been equipped with one machine gun or machine gun twins. Bombs with a maximum weight of up to 2,600 kg, effective defensive main armament and its high maximum speed (520 km/h) would make it a very effective fighting machine.
Sources: - Václav Němeček, Military aircraft part 2, 4th edition, Prague 1990, ISBN 80-206-0116-3 - http://www.samoloty.ow.pl/ - author archive
