Miloch
January 24th 18, 02:02 PM
https://en.wikipedia.org/wiki/Sukhoi_Su-2
The Sukhoi Su-2 (Russian: ????? ??-2) was a Soviet reconnaissance and light
bomber aircraft used in the early stages of World War II. It was the first
airplane designed by Pavel Sukhoi. The basic design received an engine and
armament upgrade (Su-4) and was modified for the ground-attack role (ShB).
In 1936, Joseph Stalin released a requirement for a multipurpose combat
aircraft. Codenamed Ivanov, the airplane had to be capable of performing
reconnaissance and then attacking the targets it located. P. O. Sukhoi was
working in the Tupolev OKB at the time and designed (copied the aircraft from a
Lithuanian Antanas Gustaitis; the main aircraft was ANBO-8) the "Ivanov"
aircraft under the tutelage of Andrei Tupolev. The resulting ANT-51 flew on 25
August 1937 with M. M. Gromov at the controls. Powered by a 610 kW (820 hp)
Shvetsov M-62 air-cooled radial engine,the ANT-51 reached 403 km/h (220 kn, 250
mph) at 4,700 m (15,420 ft). This was considered insufficient but since the
basic design was sound, it was decided to re-test it with a more powerful
engine. Equipped with a 746 kW (1,000 hp) Tumansky M-87 engine, the ANT-51
reached 468 km/h (255 kn, 290 mph) at 5,600 m (18,370 ft) and was accepted into
production as BB-1 (Blizhniy Bombardirovschik; Russian: ??????? ?????????????? —
"short-range bomber"). In 1940, the aircraft was renamed Su-2 and the unreliable
M-87 engine was replaced with a Tumansky M-88. This lightened version with an
M-88B engine reached 512 km/h (275 kn, 320 mph) in testing.
The Su-2 was of mixed construction. The fuselage was semi-monocoque with wood
spars and a plywood skin. The wings were of duralumin and steel construction
with fabric-covered rod-actuated control surfaces. The pilot and gunner were
protected with 9 mm (0.35 in) of armor. The taildragger landing gear was
retractable, including the tailwheel.
Role
Reconnaissance aircraft and light bomber
National origin
Soviet Union
Manufacturer
Sukhoi
Designer
Pavel Sukhoi
Andrei Tupolev
First flight
25 August 1937
Introduction
December 1939
Retired
1944
Primary user
Soviet Air Forces
Number built
910
Although 910 Su-2s were built by the time production was discontinued in 1942,
the aircraft was obsolete and underarmed by the start of the Great Patriotic
War. In combat, the Su-2 ground attack aircraft squadrons suffered heavy losses
against the Germans, with some 222 aircraft destroyed. From 1942, the Su-2 was
withdrawn from the frontline and replaced by Ilyushin Il-2, Petlyakov Pe-2 and
Tupolev Tu-2 bombers. The Su-2 was relegated to a training and reconnaissance
role. However, due to a critical shortage of aircraft in early World War II,
some Su-2s were used as emergency fighters.
Specifications (Su-2 with M-82)
General characteristics
Crew: 2
Length: 10.46 m (34 ft 4 in)
Wingspan: 14.3 m (46 ft 11 in)
Height: 3.75 m (12 ft 3 in)
Wing area: 29 m² (312 ft²)
Empty weight: 3,220 kg (7,100 lb)
Loaded weight: 4,700 kg (10,360 lb)
Fuel capacity: 1,240 l (270 imp gal; 330 US gal)
Powerplant: 1 × Shvetsov M-82 radial engine, 1,044 kW (1,400 hp)
Performance
Maximum speed: 485 km/h (300 mph, 260 kn) at altitude
Range: 1,100 km (685 mi; 595 nmi)
Service ceiling: 8,400 m (27,560 ft)
Rate of climb: 9.8 minutes to 5,000 m (16,405 ft)
Armament
6 × 7.62 mm ShKAS machine guns (4 in the wings, 1 in rear turret, 1 in the hatch
in the floor)
10 × RS-82 rockets
8 × RS-132 rockets
Up to 600 kg (1,320 lb) of bombs in the internal bomb bay and underwing
hardpoints
*
The Sukhoi Su-2 (Russian: ????? ??-2) was a Soviet reconnaissance and light
bomber aircraft used in the early stages of World War II. It was the first
airplane designed by Pavel Sukhoi. The basic design received an engine and
armament upgrade (Su-4) and was modified for the ground-attack role (ShB).
In 1936, Joseph Stalin released a requirement for a multipurpose combat
aircraft. Codenamed Ivanov, the airplane had to be capable of performing
reconnaissance and then attacking the targets it located. P. O. Sukhoi was
working in the Tupolev OKB at the time and designed (copied the aircraft from a
Lithuanian Antanas Gustaitis; the main aircraft was ANBO-8) the "Ivanov"
aircraft under the tutelage of Andrei Tupolev. The resulting ANT-51 flew on 25
August 1937 with M. M. Gromov at the controls. Powered by a 610 kW (820 hp)
Shvetsov M-62 air-cooled radial engine,the ANT-51 reached 403 km/h (220 kn, 250
mph) at 4,700 m (15,420 ft). This was considered insufficient but since the
basic design was sound, it was decided to re-test it with a more powerful
engine. Equipped with a 746 kW (1,000 hp) Tumansky M-87 engine, the ANT-51
reached 468 km/h (255 kn, 290 mph) at 5,600 m (18,370 ft) and was accepted into
production as BB-1 (Blizhniy Bombardirovschik; Russian: ??????? ?????????????? —
"short-range bomber"). In 1940, the aircraft was renamed Su-2 and the unreliable
M-87 engine was replaced with a Tumansky M-88. This lightened version with an
M-88B engine reached 512 km/h (275 kn, 320 mph) in testing.
The Su-2 was of mixed construction. The fuselage was semi-monocoque with wood
spars and a plywood skin. The wings were of duralumin and steel construction
with fabric-covered rod-actuated control surfaces. The pilot and gunner were
protected with 9 mm (0.35 in) of armor. The taildragger landing gear was
retractable, including the tailwheel.
Role
Reconnaissance aircraft and light bomber
National origin
Soviet Union
Manufacturer
Sukhoi
Designer
Pavel Sukhoi
Andrei Tupolev
First flight
25 August 1937
Introduction
December 1939
Retired
1944
Primary user
Soviet Air Forces
Number built
910
Although 910 Su-2s were built by the time production was discontinued in 1942,
the aircraft was obsolete and underarmed by the start of the Great Patriotic
War. In combat, the Su-2 ground attack aircraft squadrons suffered heavy losses
against the Germans, with some 222 aircraft destroyed. From 1942, the Su-2 was
withdrawn from the frontline and replaced by Ilyushin Il-2, Petlyakov Pe-2 and
Tupolev Tu-2 bombers. The Su-2 was relegated to a training and reconnaissance
role. However, due to a critical shortage of aircraft in early World War II,
some Su-2s were used as emergency fighters.
Specifications (Su-2 with M-82)
General characteristics
Crew: 2
Length: 10.46 m (34 ft 4 in)
Wingspan: 14.3 m (46 ft 11 in)
Height: 3.75 m (12 ft 3 in)
Wing area: 29 m² (312 ft²)
Empty weight: 3,220 kg (7,100 lb)
Loaded weight: 4,700 kg (10,360 lb)
Fuel capacity: 1,240 l (270 imp gal; 330 US gal)
Powerplant: 1 × Shvetsov M-82 radial engine, 1,044 kW (1,400 hp)
Performance
Maximum speed: 485 km/h (300 mph, 260 kn) at altitude
Range: 1,100 km (685 mi; 595 nmi)
Service ceiling: 8,400 m (27,560 ft)
Rate of climb: 9.8 minutes to 5,000 m (16,405 ft)
Armament
6 × 7.62 mm ShKAS machine guns (4 in the wings, 1 in rear turret, 1 in the hatch
in the floor)
10 × RS-82 rockets
8 × RS-132 rockets
Up to 600 kg (1,320 lb) of bombs in the internal bomb bay and underwing
hardpoints
*