Nikitin IS-1

The IS-1 (Istrebitel Skladnoi or folding fighter) was conceived by Nikitin’s Test pilot Vladimir V Shevchenko and designed in collaboration with Vasili V Nikitin. Polymorphic in concept, it could translate from biplane to monoplane configuration and back again in the air. He created the IS-1 by modifying an I-153. He added a retractable lover wing that was pneumatically of hydraulically raised into the upper wing. Control was provided through means of a three-position switch with first raise the landing gear, then raise the wing.

The IS-1 was intended to take-off as an unequal-span biplane, subsequently retracting its main wheels pneumatically into the lower wing and then folding this wing (again pneumatically), the centre section into recesses in the fuselage sides and the outer panels into shallow depressions in the upper wing. Theoretically, the lower wing could be extended during combat to increase manoeuvrability.

The IS-1 was powered by a 1,100hp Shvetsov M-63 nine-cylinder radial and carried an armament of four 7.62mm ShKAS machine guns. Construction was all metal and the prototype was flown for the first time on 6 November 1940, the lower wing being successfully retracted and extended within 7-10 seconds during subsequent trials. Refinement of the basic design for series production had meanwhile resulted in the IS-2, only one prototype of the IS-1 being completed.

Engine: 1,100hp Shvetsov M-63
Wingspan: 8.60 m / 28 ft 3 in
Length: 6.79 m / 22 ft 3 in
Wing area: 13.0-20.8 sq.m / 139.93 – 223.89 sq ft
Take-off weight: 2300 kg / 5071 lb
Empty weight: 1400 kg / 3086 lb
Max. speed: 453 km/h / 281 mph
Range: 600 km / 373 miles
Armament: 7.62mm ShKAS machine guns

Nieuport 29

Nieuport 29V

The 1924 Beaumont Cup race was won by Sadi Lecointe on the Nieuport 29, equipped with Hispano’s 450-horsepower V-engine. The Sadi-Lekuanta aircraft covered a distance of 300 kilometers in 57 minutes 50 seconds with an average speed of 312.39 km / h. Thus, a prize of 75,000 francs was awarded by Société Nieuport-Astra.

The Nieuport 29V set two world records in 1929.

Nieuport 28

Nieuport 28C

By 1917 the single-spar wing had reached the limit of development so Nieuport designed to two-spar Nieuport 28 around the new 160 hp Gnome engine.

Flying the Nieuport 28C-1 – Frank Tallman

A single bay biplane, the two-spar wooden wings have plywood on the leading edges and fabric covering aft of the front spar. The wooden fuselage has plywood covering as far as the cockpit and fabric on the rear fuselage. Conventional controls were fitted, with ailerons on the lower wings only.

Nieuport 28C-1

Only a few were used by the French Air Force but the Americans bought 297 to equip their Expeditionary Force.

They did have a habit of shedding fabric from its wings in a dive. Before this was fixed, the Nieuport 28 had been replaced in the US squadrons by Spad 13’s.

Ultralight replica:
Airdrome Airplanes Nieuport 28

28C
Engine: Gnome, 160 hp or Clerget, 160 hp
Wingspan: 26 ft 9 in
Length: 20 ft 3 in
Height: 7 ft
Max speed: 140 mph at SL
Endurance: 2 hr
Armament: 1 or 2 Vickers mg
Crew: 1

Nieuport N 28 C 1 Bébé
Engine: Gnôme-et-Rhône 9 N Monosoupape, 160 hp
Length: 21 ft 9 in / 6.4 m
Height: 8 ft 1 in / 2.5 m
Wingspan: 26 ft 9 in / 8.16 m
Wing area: 172.224 sqft / 16.0 sq.m
Max take-off weight: 1540 lb
Weight empty: 960 lb / 435.0 kg
Max. weight carried: 507.2 lb / 230.0 kg
Fuel capacity: 33 Imp.Gal
Max. speed: 128 mph / 111 kts / 206 km/h at SL
Initial climb rate: 1181.10 ft/min / 6.00 m/s
Service ceiling: 20,000 ft / 6100 m
Wing load: 8.61 lb/sq.ft / 42.00 kg/sq.m
Range: 130 nm / 240 km
Endurance: 2 h
Crew: 1
Armament: 2 x Vickers mg

Nieuport 27

Nieuport 27.C1

The Nieuport 27 saw comparatively little com¬bat and the AEF appear to have made the greatest use of it. Over 180 are thought to have been purchased, most being used as ‘pursuit trainers’.

The genuine Nieuport 27.Cl had the plain tailskid. The central, vertical, bracing wire to the mid point of the spreader bar where the two half axles were pivoted, and the simplified skid, distinguished the Nie 27 from the Nie 24.

Ultralight replica: Airdrome Airplanes Nieuport 27

Nieuport 24

Nieuport 24.C1

The Nieuport 24bis strongly resembled previous Nieuport designs but was lighter and had more power than the 17. It was aerodynamically cleaner through the use of fuselage side stringers.

Type 24bis

The Nieuport 24 and 27 were fitted with a round tail similar to the later type 28, whereas the type 24bis used the angular type 17 empennage.

As with all “Vee” strut Nieuport designs the 24bis possessed an inherent weakness of the lower wing. The sesquiplane configuration caused the wing to twist during prolonged high speed dives or abnormally violent maneuvers.

Shortly after its inception the 24bis was cancelled out as a first line fighter and many found their way to the rear as advanced trainers.

Gallery

Replica: Redfern Nieuport 24

Ultralight replica:
Airdrome Airplanes Nieuport 24
Circa Reproductions Nieuport 24

24bis
Engine: Bentley, 130 hp
Weight: 782 lb
Max speed: 116 mph