Alekseyev I-21
I-21 | |
---|---|
Role | Jet fighter
|
National origin | Soviet Union |
Manufacturer | Alekseyev OKB-21 |
Designer | Semyon Alekseyev |
First flight | Late 1947 |
Retired | 1947 after test flight. |
Status | Prototype |
Number built | 3 |
Variants | Alekseyev I-212 |
The Alekseyev I-21 was a Soviet
Development
After working as
The I-21 was a twin-engined, all-metal,
Design work on the I-210 (I-21 version 0) was concurrent with the I-21, probably as a fall back for any lack of availability of the latter's TR-2 engines. The only significant difference was the substitution of 800 kgf (7.8 kN; 1,800 lbf) BMW 003 engines (or the reverse-engineered RD-20), but the ex-German engine's significantly inferior thrust rating meant that it would never meet the I-21's speed requirement. Even replacing the BMW 003 with the slightly more powerful (900 kgf (8.8 kN; 2,000 lbf)) Jumo 004 would not allow the I-210 to meet the speed requirement and the project was cancelled before any metal was cut.[3]
Construction of the first two airframes, designated as the I-211 (I-21 version 1), began at the end of 1946, under extreme pressure by the Ministry of Aircraft Production to complete initial flight testing by 1 August 1947, to enable the aircraft to take part in the Aviation Day Flypast at
Flight testing started in late 1947, but only six test flights had been carried out before the I-211 struck a
A second I-215 was built to an order from
Variants
- I-210 - The initial version with BMW 003 or Tumanskii RD-20 engines, project only.[3]
- I-211 - The first flyable example completed as the I-211 with Lyul'ka TR-1 engines, rebuilt as the I-215.[7]
- I-211S - I-211 with swept wing and unswept tail, project only.[7]
- I-215 - The re-built I-211 with Rolls-Royce Derwent V engines and other minor modifications.[8]
- I-215D - Bicycle-undercarriage I-215 built to order of OKB-1.[6]
Specifications (I-211 as tested)
Data from Early Soviet Jet Fighters[9]
General characteristics
- Crew: 1
- Length: 11.54 m (37 ft 10 in)
- Wingspan: 12.25 m (40 ft 2 in)
- Wing area: 25 m2 (270 sq ft)
- Airfoil: I-S10-11
- Empty weight: 6,890 kg (15,190 lb)
- Gross weight: 7,400 kg (16,314 lb)
- Fuel capacity: 2,000 kg (4,400 lb) (internal), 2,500 kg (5,500 lb) (with drop tanks)
- Powerplant: 2 × Lyul'ka TR-1axial-flow turbojet, 12.8 kN (2,870 lbf) thrust each
Performance
- Maximum speed: 950 km/h (590 mph, 510 kn) at sea level
- Ferry range: 1,550 km (960 mi, 840 nmi)
- Service ceiling: 13,600 m (44,600 ft)
- Rate of climb: 27.78 m/s (5,469 ft/min)
- Time to altitude: 5,000 m (16,000 ft) in 3 minutes
Armament
- Guns: 2 × 23 mm (0.91 in) Nudelman-Suranov NS-23 autocannon with 75 rounds per gun
See also
Aircraft of comparable role, configuration, and era
Related lists
References
- ^ a b Gordon & Kommissarov 2014, pp. 405–06
- ^ Gordon & Kommissarov 2014, p. 415
- ^ a b Gordon & Kommissarov 2014, pp. 406–07
- ^ Gordon & Kommissarov 2014, p. 410
- ^ Gordon & Kommissarov 2014, pp. 410–11, 414–16, 422
- ^ a b Gordon & Kommissarov 2014, p. 422
- ^ a b Gunston 1995, pp. 16–17
- ^ Gordon & Kommissarov 2014, pp. 416–18, 422
- ^ Gordon & Kommissarov 2014, pp. 405–06, 415
Bibliography
- Gordon, Yefim & Kommissarov, Dmitry. Early Soviet Jet Fighters. Manchester, UK: Hikoki Publications, 2014. ISBN 978-1-902109-35-0.
- ISBN 1-85532-405-9.
Further reading
- Green, William & Swanborough, Gordon. "The Complete Book of Fighters". London: Salamander Books. 1994. ISBN 1-85833-777-1
External links
- I-215 at Ugolok Neba site (in Russian)