• Source: Ikarus 451

The Ikarus 451 is a family of research aircraft designs built in Yugoslavia in the 1950s, all sharing the same basic airframe, but differing in powerplants and cockpit arrangements. One member of the family Ikarus 451M became the first domestically-built jet aircraft to fly in Yugoslavia, on 25 October 1952.




Design and development


To research prone pilot cockpit arrangements and controls, the Government Aircraft Factories developed the Ikarus 232 Pionir, a small twin-engined low-wing monoplane, powered by 2x 48 kW (65 hp) Walter Mikron III piston engines. An enlarged version of the Pionir was developed as the Type 451, powered by 2x 120 kW (160 hp) Walter Minor 6-III piston engines.
The first aircraft built under this designation was a propeller-driven aircraft that also accommodated the pilot in prone position. It was an otherwise conventional low-wing monoplane with retractable tailwheel undercarriage, the main units of which retracted backwards into the engine nacelles mounted below the wings. This flew in 1952, and by the end of the year was followed by the 451M (Mlazni – "Jet") which had conventional seating for the pilot and in place of the two Walter Minor 6-III inline engines of the original Ikarus 451 (which has two inverted Walter six-cylinder piston engines of 120 kW (160 hp) each, 6.7 m (22 ft) wingspan, a maximum speed of 335 km/h (182 knots) and a ceiling of 4750m (15,570 ft).) was fitted with Turbomeca Palas turbojets. In this version, the undercarriage retracted inwards. Provision was made to carry one 20 mm Hispano Suiza 404A cannon under the fuselage, plus six RS rockets under the wings. Further developments were aimed at developing a viable military aircraft from this basic design.
The S-451M Zolja ("Wasp") that flew in 1954 featured a stretched fuselage, folding wings, and redesigned engine nacelles, now in the same plane as the wing rather than being hung under them. In 1960 a S-451M Zolja set a speed record for aircraft with a takeoff weight from 1,000 kg (2,200 lb) to 1,750 kg (3,860 lb), flying at 500.2 km/hour. It then served as the basis for the development of an armed version, the J-451MM Stršljen ("Hornet") intended for the close-support (Jurisnik) role. This differed from preceding designs in having a tricycle undercarriage, as well as Turbomeca Marbore engines with over twice the thrust of those used on earlier aircraft, and armament increased to two HS.404 cannon carried under the fuselage. This configuration then formed the basis for the S-451MM Matica ("Queen bee") two-seat trainer that set an airspeed record for aircraft weighing between 1,750 kg (3,860 lb) and 3,000 kg (6,600 lb), achieving 750.34 km/hour (466.24 mph) in 1957. It was also developed into the T-451MM Stršljen II single-seat acrobatic trainer.
No member of the family was produced in any number. The 451, 451M, and J-451MM are all preserved at the Museum of Aviation in Belgrade.




Variants


232 Pionir
A small twin-engined prone-pilot research aircraft, powered by 2x 48 kW (65 hp) Walter Mikron III piston engines. (1 built)
S-451
A larger, more powerful version of the Pionir, powered by 2x 120 kW (160 hp) Walter Minor 6-III piston engines and also incorporating a prone pilot cockpit. (1 built)
S-451M
(Mlazni – Jet) Derived directly from the S-451 airframe, the S-451M substituted Turbomeca Palas turbojet engines for the piston engines, in underslung nacelles at the same positions on the wing and conventional cockpit.
S-451M Zolja
(Zolja – Wasp) Flown in 1954, the S-451M Zolja featured a stretched fuselage, folding wings, and engine nacelles centred on the wing chordline. Powered by 2x 1.57 kN (353 lbf) Turbomeca Palas 056A turbojet engines, the S-451M was used to set a world speed record in its class in 1960.

J-451MM Stršljen
(J – Jurisnik – close support) (Stršljen – Hornet)The intended production close support version with tricycle undercarriage, Turbomeca Marbore engines and cannon armament. (1 built).
S-451MM Matica
(Matica – Queen bee) Two-seat trainer version, used for a world speed record in 1957.
T-451MM Stršljen II
A single seat aerobatic trainer, fitted with more ammunition and maximum ordnance weight was slightly increased.




Specifications (451M)



General characteristics

Crew: One pilot
Length: 7.45 m (24 ft 5 in)
Wingspan: 6.78 m (22 ft 3 in)
Height: 2.32 m (7 ft 7 in)
Wing area: 8.0 m2 (86 sq ft)
Empty weight: 897 kg (1,977 lb)
Gross weight: 1,350 kg (2,980 lb)
Powerplant: 2 × Turbomeca Palas 056A , 1.5 kN (330 lbf) thrust each
Performance

Maximum speed: 470 km/h (290 mph, 250 kn)
Range: 300 km (190 mi, 170 nmi)
Service ceiling: 8,500 m (27,900 ft)




See also



Ikarus 452




References



Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 430.




External links



Ikarus S-451M (Specifications, photos, scheme...)
Ikarus T-451M Stršljen ("Hornet") photo
Ikarus S-451, 451M & S-451MM Matica ("Queen bee") photos
Ikarus T-451M Stršljen ("Hornet") & T-451MM Stršljen II ("Hornet II") photos

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• Aeronautical Museum Belgrade