
Avia B-33 | |
|---|---|
| Zemlja | Иehoslovaиka |
| Ulogu | Avioni za kopneni napad |
| Prvi let | 18 April 1944 |
| Izgradio | 6166 |
Čaj Ilyushin Il-10 was a Soviet ground attack aircraft developed at the end of World War II by the Ilyushin construction bureau. It was also license-built in Czechoslovakia by Avia as the Avia B-33.
Izvor: Avia B-33 na Wikipediji
| Avia B-33 Walk Around | |
|---|---|
| Fotograf | Unknow |
| Lokalizacija | Nepoznato |
| Fotografije | 36 |
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General Characteristics
The Avia B-33 was the Czechoslovak-built, licensed version of the Soviet Ilyushin Il-10 “Beast,” a heavily armored, single-engine ground attack aircraft developed at the end of World War II. Produced by Avia in the early Cold War era, the B-33 served as a primary close air support platform for Czechoslovakia and was also exported to other Eastern Bloc nations.
| Property | Typical Value (Based on Il-10/B-33) |
|---|---|
| Ulogu | Ground Attack / Close Air Support |
| Proizvođača | Avia (Czechoslovakia) |
| First Flight (Il-10) | April 18, 1944 |
| First Flight (B-33) | December 26, 1951 |
| Posada | 2 (Pilot and Rear Gunner) |
| Dužina | 11.20 m (36 ft 9 in) |
| Raspon krila | 13.40 m (43 ft 11 in) |
| Max Takeoff Weight | 6,700 kg (14,771 lb) |
Design and Powerplant
- Engine: One Mikulin M-42 12-cylinder, liquid-cooled V-12 piston engine (produced under license in Czechoslovakia).
- Power Output: Approximately 1,470 kW (1,970 hp).
- Armor: The aircraft was heavily armored, with a “bathtub” shell of armor plates (4 to 8 mm thick) protecting the engine and crew compartment, making it highly survivable against ground fire.
- Construction: Low-wing monoplane with a metal-covered frame.
- Landing Gear: Fully retractable main undercarriage, folding rearward.
Performance and Armament
- Maximum Speed: Up to 551 km/h (342 mph, 298 knots) at altitude.
- Cruise Speed: Approximately 310 km/h (190 mph, 170 knots).
- Service Ceiling: 5,500 m (18,000 ft).
- Range: Approximately 800 km (500 mi, 430 nmi).
- Fixed Armament (B-33/Post-War Il-10):
- Forward: Four 23 mm NS-23 or NS-23RM cannons in the wings.
- Rear: One 20 mm B-20E cannon in a flexible rear turret for the gunner.
- Ordnance Load: Normal bomb load of 400 kg (880 lb), maximum of 600 kg (1,300 lb), including:
- General-purpose bombs (up to 250 kg).
- Anti-tank HEAT bombs (PTAB-2.5-1.5).
- Unguided Rockets (RS-82 or RS-132) on underwing rails.
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