Breda Ba.201

infobox Aircraft
name = Ba.201
type = Dive bomber
manufacturer = Breda


caption =
designer =
first flight = 3 July 1941
introduction =
retired =
status =
primary user =
more users =
produced =
number built = 2
unit cost =
developed from =
variants with their own articles =

The Breda Ba.201 was a Italian dive bomber designed during World War II, that never entered production.

Development

The struggle of Regia Aeronautica to develop an effective bomber force was surprising for everyone, as in the pre-war period the Italian air force was highly rated and performed well during the Spanish Civil War and the Second Italo-Abyssinian War. But its performance in the first months of WWII was poor, even failing to reduce Malta with 1,000 bombers based less than 100 km (62 mi) away. One of the reasons was the lack of dive bombers and effective ground attack aircraft; the Breda Ba.88 was a failure, and the Caproni Ca.310 was so ineffective that was replaced by the Fiat CR.32 fighter-bomber. Another failure was the Savoia-Marchetti SM.85 dive bomber, phased out and replaced by the Junkers Ju 87 even before the evaluation of its successor the Savoia-Marchetti SM.86 was complete.

In 1939 a new contest for a dive bomber was called, requiring a single-engined aircraft with a maximum speed of 500 km/h (310 mph), or 450 km/h if twin-engined, capable of carrying 500 kg (1,100 lb) bombs, with an endurance of 1,200 km (745 mi) with a single engine, or 2,400 km (twin-engined). There was only one twin-engine proposal, the Piaggio P.122, which despite its all-metal construction, dorsal-wing airbrakes, two Piaggio P.XI RC40 engines giving a total of 2,000 hp, and the lack of competitors, was considered unfit for service. Single-engined types included the Caproni Ca.335 and the Breda Ba.201.

Design

The Ba.201 was a single-engined dive-bomber, all-metal in construction with a retractable undercarriage. It had a long fuselage, quite slim, with a high tail. The cockpit was set as far forward as possible. The wings had a distinct polyhedral "W" shape, like the Junkers Ju 87 "Stuka". The dive capabilities were found to be satisfactory, and the air brakes were highly effective, perhaps too effective - with the risk of slowing the aircraft down so much it became too easy a target. It was capable of carrying a single 500 kg bomb and was armed with two 12.7 mm Breda-SAFAT machine guns fixed in the wings. After such engines as the 1,200 hp Fiat A.38, the 960 hp Isotta-Fraschini IF L.121, and the powerful 1,125 hp Isotta-Fraschini Zetra, were evaluated, the Daimler-Benz DB 601 engine was chosen, because it was compact, and allowed free dives thanks to its direct injection system.

The prototype first flew on 3 July 1941, and was then sent to Guidonia for official testing. The aircraft showed that it had enough agility, once freed of its bombload, to hold its own against other Italian fighters. However speed was disappointing, only 460 km/h - slower than the requested for 500 km/h - and slightly slower than older first line fighters. The aircraft was barely capable of defending itself against enemy fighters, and then only after releasing its bomb. It had very good forward visibility, but rear visibility was poor.

In comparison the Junkers Ju-87D had a top speed of only 410 km/h, but was armed with two new MG 81z machine guns, with 3,200 rpm instead of 1,050. The Junkers rear-gunner gave it a greater defensive capability, while the Ba.201 pilot relied on himself alone. The Reggiane Re.2001 fighter-bomber fitted with the same DB 601 engine was able to reach almost 550 km/h, and carry 640 kg bombs.

The first prototype "MM.451" was followed by only one other before the programme was cancelled.

pecifications (Ba.201)

aircraft specifications
plane or copter?= plane
jet or prop?= prop
ref=
crew=One, pilot
capacity=
payload main=
payload alt=
length main= 11.09 m
length alt= 36 ft 5 in
span main= 13.00 m
span alt= 42 ft 8 in
height main= 3.10 m
height alt= 10 ft 2 in
area main=24.84 m²
area alt= 267.28 ft²
airfoil=
empty weight main= 2380 kg
empty weight alt= 5,236 lb
loaded weight main=
loaded weight alt=
useful load main=
useful load alt=
max takeoff weight main= 3650 kg
max takeoff weight alt= 8,030 lb
more general=
engine (prop)=Daimler-Benz DB 601
type of prop=liquid-cooled V12 engine
number of props=1
power main=
power alt=
power original=
max speed main= 460 km/h
max speed alt= 248 knots, 286 mph
max speed more= at 4,000 m
cruise speed main=
cruise speed alt=
never exceed speed main=
never exceed speed alt=
stall speed main=
stall speed alt=
range main= 1,200 km
range alt= 648 nm, 745 mi
ceiling main=
ceiling alt=
climb rate main=
climb rate alt=
loading main=
loading alt=
power/mass main=
power/mass alt=
more performance=
armament=
* 2 × 12.7 mm Breda-SAFAT machine guns
* 1 × 500 kg (1,100 lb) bomb
avionics=

References

*Lembo, Daniele "I tuffatori della Regia Aereonautica" Aerei nella Storia n.8. it icon

External links

* [http://1000aircraftphotos.com/Contributions/KleinBernhard/6555.htm 1000 Aircraft Photos]
* [http://www.tgplanes.com/Public/snitz/topic.asp?TOPIC_ID=1669 Great Planes forum]
* [http://www.airwar.ru/enc/bww2/ba201.html Ba.201] ru icon
* [http://italie1935-45.aceboard.fr/97185-3171-6967-0-Breda.htm Ba.201] fr icon

ee also

aircontent
related=

similar aircraft=
* Junkers Ju 87
sequence=

lists=
* List of aircraft of Italy, World War II
see also=