Focke-Wulf Fw 190 A-0

     
Název:
Name:
Focke-Wulf Fw 190 A-0 Focke-Wulf Fw 190 A-0
Originální název:
Original Name:
Focke-Wulf Fw 190 A-0
Kategorie:
Category:
stíhací letoun fighter aeroplane
Výrobce:
Producer:
DD.11.1940-DD.12.1940 Focke-Wulf Flugzeugbau AG, Bremen /
Období výroby:
Production Period:
DD.11.1940-DD.12.1940
Vyrobeno kusů:
Number of Produced:
28 (W.Nr.: 0008-0035)
První vzlet:
Maiden Flight:
01.06.1939 (prototyp / prototype Fw 190 V1)
Osádka:
Crew:
1
Základní charakteristika:
Basic Characteristics:
 
Vzlet a přistání:
Take-off and Landing:
CTOL - konvenční vzlet a přistání CTOL - conventional take-off and landing
Uspořádání křídla:
Arrangement of Wing:
jednoplošník monoplane
Uspořádání letounu:
Aircraft Concept:
klasické conventional
Podvozek:
Undercarriage:
zatahovací retractable
Přistávací zařízení:
Landing Gear:
kola wheels
Technické údaje:
Technical Data:
 
Hmotnost prázdného letounu:
Empty Weight:
2500 kg 5512 lb
Vzletová hmotnost:
Take-off Weight:
3489 kg 7692 lb
Maximální vzletová hmotnost:
Maximum Take-off Weight:
? kg ? lb
Rozpětí:
Wingspan:
10,51 m 34ft 5,77in
Délka:
Length:
8,80 m 28ft 10,45in
Výška:
Height:
3,95 m 12ft 11,5in
Plocha křídla:
Wing Area:
14,901) m2 196.981) ft2
Plošné zatížení:
Wing Loading:
? kg/m2 ? lb/ft2
Pohon:
Propulsion:
 
Kategorie:
Category:
pístový piston
Počet motorů:
Number of Engines:
1
Typ:
Type:
BMW 801 C-0
- dvouhvězdicový
- počet válců: 14
- vzletový výkon: 1147 kW (1560 PS)
BMW 801 C-0
- two-row radial
- number of cylinders: 14
- take-off power output: 1539 hp
Objem palivových nádrží:
Fuel Tank Capacity:
524 l 115 Imp gal / 138 US gal
Výkony:
Performance:
 
Maximální rychlost:
Maximum Speed:
630 km/h v 6100 m 392 mph in 20013 ft
Cestovní rychlost:
Cruise Speed:
? km/h v ? m ? mph in ? ft
Rychlost stoupání:
Climb Rate:
14 m/s 2756 ft/min
Čas výstupu na výšku:
Time to Climb to:
? min do ? m ? min to ? ft
Operační dostup:
Service Ceiling:
9600 m 31496 ft
Dolet:
Range:
810 km 503 mi
Maximální dolet:
Maximum Range:
? km ? mi
Výzbroj:
Armament:
2x 7,92mm kulomet MG 17 (v trupu)
2x 7,92mm kulomet MG 17 (v kořeni křídla)
2x 20mm kanón MG FF/M (v křídle)
2x 7,92mm MG 17 machine-gun (in the fuselage)
2x 7,92mm MG 17 machine-gun (in the wing root)
2x 20mm MG FF/M cannon (in the outboard wing)
Uživatelské státy:
User States:
- -
Poznámka:
Note:
1) letouny W.Nr.: 0008-0014, letouny 0015-0035: 18,30 m2 1) aircraft W.Nr.: 0008-0014, aircraft 0015-0035: 196.98 ft2
Zdroje:
Sources:
Rodeike, P.: Jagdflugzeug Focke-Wulf Fw 190 A, Fw 190 „Dora“, Ta 152 H, Struve- Druck, 1998
Griehl, M.: Focke-Wulf Fw 190, Flugzeug Profile 9
Scheibert, H., Campbell, J. L., Greer, D.: Focke Wulf Fw 190, Podzun-Verlag, 1976
Skupierski, A.: Fw 190 A/F/G, cz. 2, AJ-Press, 1994
Janowicz, K.: Focke Wulf Fw 190 vol. I, Kagero, 2003
URL : https://www.valka.cz/Focke-Wulf-Fw-190-A-0-t54912#386010 Version : 0
Fighter aircraft Focke-Wulf Fw 190 A-0 represents the first pre-series group of Fw-190 designed for field testing and involving a total of 28 aircraft (26 passed for testing, two used for ground static breaking tests) including prototypes V6 and V7. Aircraft were equipped with engines BMW 801 C-0 (the first 10 aircraft, including prototypes), and then also BMW 801 C-1 (gradually them outside of the newly built aircraft were in April 1941, covered the aircraft with the engines BMW 801 C-0) and their armament was made up of four machine guns the MG 17 the caliber of 7.62 mm (two machine guns above the engine, two in the wing roots).

The planes were for the purposes of the field tests passed in February 1941 in the arsenal of the Eprobungsstaffel 190 placed in the Gap. There were tested not only the test pilots of the company Focke-Wulf but also which the field airmen, who had a new aircraft to assess in terms of the possible frontline deployment. These tests have shown very good agility and maneuverability of the airplane but at the same time has demonstrated a number of shortcomings. The most heavily criticised has become the imperfect design of the radiator, which in the long-term stress causes very rapid heating of the engine (this defect has been fixed up in the version of A-3 when he was between the radiator and spinner mounted bladed fan tightly coupled to the propeller shaft) and the inability to jettison the canopy at speeds above 400 km/h (covered with was in the marginalization of the need to use the pan in the upper part slightly bend to make the copy of the guide rails, at speeds over 400 km/h normally the air pressure in the cabin to prevent it bending, pushed and dump). In particular, the second defect was not initially paid attention but after one of the pilots with this defect died (6.made aircraft, may 1941, exceeding the limit angles of attack) was to the entire mechanism mounted small pyropatrona, which the whole covered up samočině dropped.

Tests aircraft within the Eprobungsstaffel 190 were completed in June 1941 and produced aircraft were handed back to the factory, where planes were converted to standard Fw 190 a-1.


Sources:
www.topsid.com
www.wikipedia.org
Archives of the author.
URL : https://www.valka.cz/Focke-Wulf-Fw-190-A-0-t54912#202655 Version : 0

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Fw 190 A-0/U4 (W.Nr. 0022 a 0023) při zkouškách s podvěšenou pumovou výzbrojí.


Zdroj: viz výše
Focke-Wulf Fw 190 A-0 -


URL : https://www.valka.cz/Focke-Wulf-Fw-190-A-0-t54912#387079 Version : 0

This post has not been translated to English yet. Please use the TRANSLATE button above to see machine translation of this post.

Fw 190 A-0 (W.Nr. 0024, SB+ID) po opuštění výrobní linky.


Zdroj: viz výše
Focke-Wulf Fw 190 A-0 -


URL : https://www.valka.cz/Focke-Wulf-Fw-190-A-0-t54912#387081 Version : 0
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