ISF Mistral / Mistral Flugzeugbau Mistral

ISF Model 2 Mistral-C

Developed from the original Mistral, which first flew in 1975, the ISF Model 2 Mistral-C single-seat Club Class sailplane is a product of the German firm Ingenieur/Buro Dipling Strauber – Frommhold GmbH & Co KG. Design work on the Mistral-C, which was intended to conform with the new FAI Club regulations, started in October 1974 and the prototype made its first flight in October 1976; 20 examples of this glassfibre T-tailed sailplane had been completed by the beginning of 1979. The type took 3rd place out of 33 contestants in the first Club class international competition held in Sweden in 1979.

The Mistral-C is a cantilever shoulder wing monoplane with 1° forward sweep at the quarterchord line; the wings and tail unit are of glassfibre reinforced plastic/foam/Conticell CC60 sandwich construction, the ailerons being of glassfibre reinforced plastic (GRP). There are Schempp-Hirth aluminium air brakes in the wing upper surfaces.

The fuselage is a GRP monocoque structure, and the landing gear consists of a non-retractable monowheel with a brake, and a tailskid. The tailplane is a fixed incidence one with spring trim, and the pilot sits under a large flush-fitting one-piece canopy that opens sideways. There is a towing hook on the centre of gravity, and a nose-mounted hook is optional.

In 1980 Mistral Flugzeugbau was formed to continue production of the Mistral-C at Hassfurt/Main; it had previously been built at Bensheim.

Mistral-C
Span: 15.0 m / 49 ft 2.5 in
Length: 6.73 m / 22 ft 1 in
Height: 1.45 m / 4 ft 9 in
Wing area: 10.9 sq.m / 116.8 sqft
Aspect ratio: 20.7
Wing section: Wortmann FX-61-163
Empty weight: 230 kg / 510 lb
Max weight: 350 kg / 77 1 lb
Water ballast: None
Max speed: 155 mph 135 kt / 250 km/h (in smooth air)
Max aero-tow speed: 105 mph
Stalling speed: 33 kt / 62 km/h
Min sinking speed: 2.17 ft/sec at 43.5 mph
Min sinking speed: 0.60 m/sec / 1.96 ft/sec at 35 kt / 65 km/h
Best glide ratio: 35: 1 at 55.5 mph
Best glide ratio: 35 at 49 kt / 90 km/h

Isaacs Spitfire

Construction of the 60% replica of the World War 2 Spitfire was begun by John Isaacs in 1969 at Southampton. Wood and fabric construction. Powered by a Rolls-Royce/Continental O-200-A engine, the prototype, c/n.2, later registered G-BBJI PFA.27-10055, first flew in early 1975.

Gallery

Engine: Continental O-200, 100 hp.
Height: 5.6 ft.
Length: 19.3 ft.
Wing span: 22.1 ft.
Wing area: 87 sq.ft.
Weight empty: 805 lbs.
Gross: 1100 lbs.
Fuel cap: 13 USG.
Speed max: 150 mph.
Cruise: 130 mph.
Range: 200 sm.
Stall: 47 mph.
ROC: 1100 fpm.
Take-off dist: 600 ft.
Landing dist: 450 ft.
Service ceiling: 15,000 ft.
Seats: 1.
Landing gear: tail wheel.

Isaacs Fury / PFA Isaac Fury

Fury II

Designed by John Isaacs, the Fury is a 7/10 scale, single seat wooden replica of the famous Hawker Fury biplane of the 1930’s. The Isaacs Fury Mk 1 prototype G-ASCM first flew in 1963 powered by a 65 hp Mikron III engine. In 1967 the prototype was modified to Mk 2 standard by installing a 125 hp Lycoming O-290 engine. This aircraft is stressed to 9g for aerobatics. Normal load limits are +5 and -1G.

Fury II

The fuselage is a spruce structure of rectangular cross-section, with a curved turtlede eking and plywood covered. The wing is made up of solid spruce, warren girder ribs, internal diagonal wooden bracing and fabric covering. Ailerons are on the top wing only. No flaps are fitted. N type cabane and interplane struts support the wings which have conventional external wire bracing. The airfoil section is RAF 28. The empennage is a wooden structure utilising solid spars, girder ribs and fabric covering. The tailplane is strut braced. The fixed landing gear incorporates rubber cord shock-absorption and 3.25 x 14” wheels. A 10 Imperial gallon fuel tank is located aft of the firewall. A luggage locker is provided behind the cockpit.

It is only offered as a scratch built project with plans from John Isaacs. It is also an approved type of aircraft by the PFA in the UK.

John Isaac had sold 200 sets of plans (revised in 1994) by 1998. The plans were then marketed by the Popular Flying Association.

Gallery

Engine: Lycoming
Wing span: 6.4 m
Wing area: 11.4 sq.m
MAUW: 454 kg
Empty weight: 333 kg
Fuel capacity: 68 lt
Max speed: 185 kph
Cruise speed: 160 kph
Minimum speed: 72 kph
Climb rate: 8 m/s
Seats: 1
Fuel consumption: 25 lt/hr
Plan price (1998): $120

Engine: Lycoming 0-290, 125 hp.
Span, upper wing: 2l ft 0 in.
Lower wing: 18 ft 2 in.
Length: 19 ft 3 in.
Wing Area: 123.8 sq.ft.
Wing Loading: 8.1 lb/sq.ft.
Fuel cap: 18 USG.
MAUW: 1000 lbs.
Weight Empty: 730 lb.
Stall Speed: 38 mph.
Cruise: 100 mph.
Vne: 135 mph.
Top speed: 115 mph
Range: 200 sm.
Take-off dist: 400 ft.
Vne: 160 mph.
ROC: 1600 fpm.
Ultimate Loading: +9/-4.5g.

Engine: Lycoming 0-235-C, 115 hp.
Range 160km (100 miles).
MTOW: 1000 lbs.
Empty wt: 675 lbs.
Wing span: 21 ft.
Stall: 30 kts.
ROC: 1400 fpm.
Load limits: +9 / -4.5G.

Engine: Lycoming 0-235 C2A, 125hp.
Prop: Henry 428 72in dia/44in pitch
Cruise 85kt @2400rpm
ROC: 1500fpm
Fuel burn @ cruise: 26 lt/hr
Load: +9/-5.

Isaac, A.C.T.

Mr A.C.T. Isaac, of London, later of Hillmorton, near Rugby, Warwickshire, in the UK, built a two-seat primary gliders. The first, in 1923 had trials off Parliament Hill,in North London, resulted in the gliders either breaking up and injuring the pilot, or in requests from the police to ‘take them away’.

1923 glider

A two seat primary type with 9.29 sq.m / 100 sq.ft wing area with a slotted section.

It was left overnight in dead-calm conditions. The following morning it was not to be seen, and was presumed stolen.

A second machine was built in 1929 to Zogling-like specification but this too was a failure. The flexible structure was abandoned as impracticable. The empty was 45.35 kg / 100 lb.

1929 glider

A biplane glider of 7.32m / 24 ft 0 in span was later built and test flown at Chingford, London.

Irwin Meteorplane M-T-2 / SP-1

After the First World War the company built an improved version of the M-T, the M-T-2, powered by a 20 hp Meteor engine. The 1926 M-T-2, or SP-1, was of plywood construction and sold for $1,165.

By Irwin’s estimate about 40 were sold, including N2616, plus an unrecorded number sold as kits for $350, including N579M, N3685, and N7788, less motor (the Meteormotor went for $625). One of the world’s first successful small, personal airplanes.

Engine: Irwin Meteormotor, 25hp
Wing span: 14’0″
Length: 12’0″
Useful load: 175 lb
Max speed: 85 mph
Cruise speed: 75 mph
Stall: 24 mph
Range: 200 mi
Seats: 1

Irvine Aerocycloid

The photograph shows a quarter-size model of the Irvine Aerocycloid of 1908/1909 which was able to lift the weight of ninety pounds. The San Francisco based John C. Irvine (president of the Pacific Aero Club) had worked three years on the machine, which was driven by a 3 hp electrical engine, that could lift 30 pounds for each hp. Records do not show that the full-sized model was ever built, probably due to problems with financing of the project. The specialty of the machine was of course the two upright wheel construction, driven by cables, which carried four “propellers” which pivoted between the wheel and furnished the lifting power. With the propellers in the proper position the force would be upright, lifting the machine vertically. Pivoting the propellers at an angle would obtain a forward motion.

Irkut MC-21

A project of Russian civil aviation was the new-generation narrow-body mid-range airliner MC-21-300. United Aircraft Corporation continued to work on the new civilian aircraft from the very beginning of the COVID-19 pandemic.

IT solutions have made it possible to transfer employees of engineering and corporate centres to remote workstations. The factories also did not stop, shift work was organised to support continuous production processes, on which the implementation of the SDO and MTC programs depended. Strict control over the health status of employees has been introduced, disinfection of territories and premises of UAC enterprises was carried out.

Due to the COVID-19 pandemic, there was a short break, but work resumed. As part of the certification program according to Russian and European standards MC-21-300, a large complex of ground, flight, bench tests was underway.

The MC-21-300 airliner is being created in a wide cooperation of Rostec enterprises. More than half of avionics was developed by the holdings of the State Corporation, and titanium and composite parts are supplied. The first MC-21-300 aircraft is under construction at the Irkutsk Aviation Plant, which will undergo flight tests with PD-14 engines developed by the United Engine Corporation.

Test flights of the MC-21-300 continued. The program involves four experimental aircraft. Two of them are equipped with passenger cabins. In the case, modifications are being checked with a two-class layout for 163 seats and an ultra-dense layout for 211 seats. Flights are performed by crews of the Irkut Corporation and joint crews: pilots of the corporation and representatives of certification centres. The pace of flight tests is increasing. Often, two aircraft are simultaneously in flight.

During flights, the testing equipment allows recording of about 40 thousand parameters. By 2021 the MC-21-300 was tested for resistance to flutter and at extreme angles of attack. The main engines and auxiliary power unit were tested, including during take-off and landing with a failed engine. The minimum separation speed of the aircraft is determined. The operability of the instrumental landing system and equipment for flying in the dark was confirmed.

The production of MC-21-300 aircraft for delivery to customers had begun by 2021. The start of mass production was allowed by the positive results of flight and ground tests, which proved the correctness of the basic design and technological solutions.

Irkut

Founded on 28 March 1932 and commissioned on 24 August 1934, as GAZ 125 (becoming GAZ 39 in 1941), Irkut has built some 6,500 aircraft of 16 types from Antonov, Ilyushin, MiG, Petlyakov, Sukhoi, Tupolev and Yakovlev bureaux and supplied them to 21 countries. In recent years, it has manufactured MiG-23UB trainers (1970-85); 165 kits for Indian-assembled MiG-27MLs; Su-27UB trainers (from 1986); and was responsible for producing the Su-30 fighter (since 1991) and Beriev Be-200 amphibian. Su-30 customers include China and India; offers Su-27UBM and Su-30KN upgrades to older aircraft. Series manufacture of the Yak-112 lightplane has been abandoned, although company has been allocated prospective manufacture of the Ilyushin/HAL IL-214 twin-jet transport. Also undertakes Su-30 upgrades.
Irkut is a member of AVPK Sukhoi. Known from April 1989 until 2002 as IAPO (Irkutsk Aviation Industrial Association), having become a joint stock company in October 1992, but on 19 December 2002: shareholders approved a company change of name to Irkut NPK, IAPO becoming a subsidiary.