Mikoyan-Gurevich

Mikhail Iosifovich Gurevich and Artem Ivanovich Mikoyan with a model of the MiG-3 fighter

A. Mikoyan and G. Gurevich design bureau established December 1939; still operating in 1990 as MAPO “MiG” as part of MIG “MAPO-M” organization, although Gurevich retired in early 1960s and Mikoyan died December 9,1970.

MiG-1 fighters with AM-35 engine produced 1940-1941; developed MiG-3 produced until 1942. First jet aircraft built in quantity was MiG-9 with twin RD-20 (BMW 003A) engines, flown 24 April 1946. Swept-wing MiG-15 with Russian copy of Rolls-Royce Nene introduced 1947, built under license in Czechoslovakia and Poland. Followed by approximately 9,000 of derived MiG-17, with redesigned wing, manufactured 1950-1957. Twin Mikulin AM-5-powered MiG-19 flown September 1953, built under license in Czechoslovakia, Poland, and China. Superseded by delta-winged MiG-21, in service in the USSR from 1959 and, when built in India, was first Russian aircraft manufactured in non-communist country.

Col-Gen Mikoyan died in 1970.

As ANPK “MiG” named after A.I. Mikoyan Aviation Scientific- Production Complex, produced MiG-23 (4,278 constructed 1969-1985; also built in India) and MiG-27 (over 900 between 1973 and 1983) related variable-geometry fighter and ground-attack aircraft, MiG-25 Mach 2.8+ reconnaissance aircraft and interceptor (some 1,200 built up to 1985), and MiG-31 long-range interceptor (about 400, operational from 1983).

MAPO ‘MiG’ produced MiG-21 upgrade as MiG-21 -93, MiG-29 Fulcrum lightweight close-air-combat fighter (first flown October 1977 and over 1,500 built, serving since 1983), improved MiG-29M (first flown April 1986) and MiG-33 export version, MiG-29K shipborne fighter prototype (first flown July 1988, first landing on aircraft carrier Admiral KuznetsovNovember 1989, and development restarted in 1996 after earlier program halt), MiG-35 multirole fighter (first flight 1999?), MiG 1-44 uniquely configured newgeneration combat aircraft (first seen February 1999), and MiG-AT/UTS/AC series of advanced and combat trainers. MiG-301/321 are reported hypersonic reconnaissance aircraft, thought to be under development. Also developing MiG-110 light multipurpose transport and MiG-115 and MiG-125 transports.

Migavia – the first national aircraft manufacturer in Russia aircraft corporations. RAC “MiG” is integrated company in which all technologies of design, production and improvement of aircraft are collected together in one legal frame. Corporation Migavia holds the shares of other corporations which are included into the complex of firms developing and producing the aircraft engines.

Mike Adams Balloon Loft A55

Persons: 4
Diameter: 55 ft
Height: 67 ft
Volume: 75,000 cu.ft
Weight: 629 lb
Payload: 1500 lb
Burner: 8.8 Million BTU/hr
Fuel capacity: 10-40 USG
Cost: (1972): US$ 6920
FAI AX-7

A55-S
Persons: 4
Diameter: 55 ft
Height: 70 ft
Volume: 83,000 cu.ft
Weight: 639 lb
Payload: 1500 lb
Burner: 8.8 Million BTU/hr
Fuel capacity: 10-440 USG
Cost: (1972): US$ 7560
FAI AX-8

Mike Adams Balloon Loft A50

Persons: 3
Diameter: 50 ft
Height: 61 ft
Volume: 55,000 cu.ft
Weight: 604 lb
Payload: 1050 lb
Burner: 8.8 Million BTU/hr
Fuel capacity: 10-40 USG
Cost: (1972): US$ 5760
FAI AX-6

A50 – S
Persons: 3
Diameter: 50 ft
Height: 64 ft
Volume: 62,000 cu.ft
Weight: 614 lb
Payload: 1250 lb
Burner: 8.8 Million BTU/hr
Fuel capacity: 10-40 USG
Cost: (1972): US$ 6240
FAI AX-7

Mike Adams Balloon Loft

1982: Mike Adams Balloon Loft, DeKalb Peachtree Airport, Atlanta, Georgia 30341, USA.

PO Box 12168
Atlanta
Georgia 30355
USA

Adams offers seven models of balloons, all of which can be fitted with options such as an additional fuel tank with vapor takeoff or an electric digital py¬rometer. Envelope volumes range from 27,000 .to 83,000 cubic feet. Price, quoted on request, includes complete leather trimmed basket and all FAA required instruments.

Mijelson-Morschikhin U-4

The MU-4 (Russian: Михельсон/Никитин МУ-4) amphibious flying boat was designed and built by NG Mijelson at Leningrad Factory No.23. The initials MU correspond to Morskaya Uchebnaya or Marine Trainer.

The MU-4 was designed as a flying-boat with a single hull and amphibious capacity. The hull was made entirely of wood and was made up of five watertight departments.

The wing configuration was sesquiplanar with the wing box braced by V-shaped struts made of duralumin. The wooden wing featured a double spar structure with a slim profile and constant chord. The covering was fabric. The lower plane was inserted into the fuselage, while the upper one was located high above the cabin, from where the engine supports started. The drop-shaped stabilization floats were located in the lower wing.

For operations on land, the MU-4 had a conventional landing gear with oleo-pneumatic shock absorbers and a tail skid. The main units retracted forward on the sides of the hull by means of a manual drive system. To allow winter operations the wheels could be replaced by skis.

The MU-4 tested with skis in the winter of 1937 – 1938.

The tail unit was of the conventional monoplane type with the stabilizers located high on the empennage and fixed by parallel struts in its lower part.

The MG-11F engine was installed on the upper wing in a tractor configuration protected by a Townend ring hood and moving a two-blade propeller. For winter, a special “winter” cowl was designed.

The MU-4 could carry two people, seated side by side in an enclosed, dual-control, glazed cabin.

The first prototype was finished in August 1937. Tests showed that the plane had good flight characteristics and could perform aerobatics. During the manufacturing tests this example was destroyed due to a construction defect. The engine fixing brackets to the gunwales were glued with a poor quality glue that ended up coming off. A short time later Mijelson would be imprisoned so the responsibility for further development passed to VV Nikitin.

Mijelson MU-4/2 at Factory No.23.

The second prototype was submitted for testing in May 1938. Model tests were carried out at the NII GVF hydrostation located in Konstantinovska Bay in Sevastopol. The flights were carried out by test pilot GI Sergueyev. The MU-4 was presented as a simple plane to fly and capable of taking off and landing in small aquatic spaces.

MU-4/2 during factory tests in 1938.

It was proposed to build a series of 30 examples at Factory No.23, but after Mijelson ‘s conviction this decision was reversed. The Shavrov Sh-2 was produced in series, covering the same needs.

MU-4
Powerplant: 1 x 190 hp MG-11F
Wingspan of upper plane: 12.00 m
Wingspan of lower plane: 9.00 m
Wing area: 33.00 m²
Length: 8.70m
Height: 3.70m
Empty weight: 989 kg
Normal takeoff weight: 1255 kg
Wing loading: 36.4 kg/m²
Power load: 4.2 kg/hp
Fuel + lubricant capacity: 80 + 20 kg
Top speed: 173km/h
Cruising speed: 154 km/h
Service ceiling: 3400 m
Accommodation: 2

Mijelson-Morschijin U-3

In the mid 1930’s Leningrad Factory No.23 was producing versions of the Polikarpov U-2 trainer. In parallel with the development of the serial versions U-2, AP and others, NG Mijelson and AI Morschijin proposed in 1934 the development of a version with a similar layout, but with larger dimensions and a more powerful M-48 engine of 200hp. The objective of this model was to obtain a medium training aircraft in which the students could continue after finishing the initial classes with the U-2.

Construction of the U-3 (Russian: Михельсон/Морщихин У-3) included a number of bolted duralumin aggregates. These aggregates were generally lighter. This, together with some decrease in the reserves of structural resistance, lightened the model. Other minor modifications were introduced with a view to improving performance.

The M-48 engine was protected by a hexagonal-shaped Townend cowling constructed of “Enerzh-6” stainless steel.

The U-3 was tested in 1935 but the results obtained were not much higher than those of the U-2, and the M-48 engine was not produced in series.

Mijelson PT/PSN Valk / Nikitin PT/PSN Valk

PT

Starting in 1933, a series of projects began to be developed in the USSR under the common name of PSN, acronym for P laner S petsialnovo N aznachenya or Gliders for Special Missions. Among these projects was SF Valk’s idea of using a glider with a torpedo and an infrared or radio guidance system to attack surface ships and naval bases.

This idea had its development in a series of projects known as:
LTDD – Letayushaya Torpeda Dalnevo Dieztvya (Long Range Flying Torpedo);
DPT – Dalni Planerni Torpedo (Long Range Glider Torpedo);
BMP – Bozduzhni Minni Planer (Airborne Mine Glider);

As a development of this conception, Mijelson would receive the task of building an experimental manned hydrofoil glider capable of carrying a torpedo and intended primarily to test remote flight control systems. This glider, called PT, was followed by a small series of copies that received the name PSN (Russian: Михельсон / Никитин ПСН).

The PSN was designed as a small single-seater hydrofoil glider with stabilization floats located approximately halfway across the wingspan of each half plane. The entire construction was made of wood.

The wings presented high implantation with a trapezoidal shape in the plane. Louvered ailerons and flaps were included as control surfaces. The tail unit featured the outriggers braced by double struts high on the keel.

The pilot was located in a glass cockpit in front of the wing leading edge. At the bottom of the glider was fixed a torpedo.

The PSN was carried by a Túpolev TB-3 or TB-7 mother bomber and was released at a pre-calculated height and distances between 30 and 50 km from the target. After launching its torpedo, the glider would land on the water.

A PSN hydrofoil glider with a torpedo under the wing of the Túpolev TB-3 mother plane.

In 1934 the first PT copies and their equipment were built and tested. The first 4 units were built in 1935 at factory No. 23 in Leningrad. In this case, it was a piloted glider version designed to evaluate the infrared guidance piloting system known as Kvant (Quanto). This project was developed under the direction of Mijelson and Nikitin was in charge of the production.

Two PT gliders during the water tests.

From June until October of August of 1936 at the Naval base Krechevits the first fixation tests PT were performed under a bomber Tupolev TB-3. During these tests the PT was piloted by N N. Ivanov.

Between 1937 and 1938 the construction of a small series of PT without a pilot was requested, which received the name PSN (or PSN-1 in some literature).

In general, 10 copies of the PSN-1 were built, which were used in different tests of the Kvant guidance system and an autopilot system developed at that time.

In March 1938, after the arrest of Mijelson, the works were interrupted. All produced copies of the PSN were destroyed.

PSN
Wingspan: 8 m
Wing area: 13.2 sq.m
Length: 8.9 m
Height: 2.11 m
Empty weight: 970 kg
Loaded weight: 1970 kg
Speed: 150 – 350 km / h
Dive speed: 500 km / h
Range: 30 – 35 km
Accommodation: 1

Mijelson, Nikolai Gustavovich

Nikolai Gustavovich Mijelson (in Russian: Николай Густавович Михельсон) was born in 1895 in Bielovostok, Grodnienski governor.

The first references to Mijelson appear after joining the construction bureau “Gamayún” in Saint Petersburg, directed by Schetinin and specialized in the design and construction of hydrofoils. Starting in 1912, after the incorporation of DP Grigorovich to the factory as technical director, Mijelson became his main collaborator, participating in the creation of all his designs during the pre-revolutionary period. Mijelson’s participation was decisive in the development of the famous M-5, M-9 and M-11 hydrofoils, participants in the First World War.

During the events of October 1917 Mijelson was in Krasnoyarsk where he met MM Shishmariov, Grigorovich’s former assistant. Together in 1920 and not without running into great dangers, he managed to move to Taganrog, as they had heard that the “Lieved” factory run by B. Levediev had been created there. The years of civil war ran and the friends were forced to avoid the white and red troops in combat.

The following year, together with Shishmariov and the engineer of the “Liebed” factory, formerly a naval pilot of the Denikin troops, VL Korvin-Kerber, he won a competition promoted by the VVS leadership for the project of a single-seater naval fighter with a Hispano-Suiza 200 hp engine. Construction of the prototype began in Taganrog. The new fighter, called MK-1 “Ribka” (Fish), was designed as a biplane with a monocoque structure that completely hid the engine. This structure used four plywood stringers and frames with holes to lighten the weight. The radiator was located in the center plane of the upper wing.

For the spring of 1922 the VVS made the decision to continue the construction of the experimental MK-1 “Ribka” in Petrograd, at the “Krasni Liotchik” factory. As a result, Mijelson headed there with the details and built components of the new fighter. The other co-authors were sent to Moscow to make themselves available to DP Grigorovich.

In Petrograd Mijelson completed the construction of the plane, but during the tests the prototype refused to take off from the water. The floats were too heavy for the low power of the engine. Measures to lighten the plane did not bring positive results either. Only when Mijelson removed the floats and replaced them with a train of wheels did pilot LI Giks manage to lift it up into the air. The aircraft proved to be well designed, but the low power of its engine did not allow it to go into series production. While waiting for a new engine, the plane was stored in a hangar at the small airfield on Kretovski Island where it was destroyed during a flood in 1924.

Mijelson continued to work at the “Krasni Liotchik” factory until the Department of Experimental Shipbuilding (OMOS) led by DP Grigorovich was transferred there from Moscow. From that moment on, Mijelson joined the group led by his former boss. During this period, he participated in the development of all OMOS works, including the SUVP passenger plane, the MRL-1 naval reconnaissance plane, the I-2bis fighter, the ROM-1 and ROM-2 open sea explorers. and the MUR-1 training scout. Many of these designs were unsuccessful, which was reflected in the collective’s psychological climate. For this reason, when it was decided to return Grigorovich with his collective to Moscow, Mijelson and another group of collaborators made the decision to remain in the “Krasni Liotchik” . Mijelson was in charge of the drawing department.

In 1929 Mijelson was arrested. This happened unexpectedly and was a continuation of the process that began with the arrest of DP Grigorovich and involved a significant number of OMOS workers. For a whole year Mijelson had been summoned to answer as a witness in the trials of DP Grigorovich, AN Sidielnikov, VL Korvin-Kerber and other colleagues, until his time finally came. Judged by article 58, Mijelson was sent to the first Sháraga TsKB-39 of the OGPU, where builders of the Grigorovich and Polikarpov collectives were already working. This collective in a very short time and under a strict supervision system managed to develop the I-5 fighter, the IZ gun fighter and the TB-5 bomber. In all these works Mijelson had an active participation.

In 1931 Mijelson was released and returned to Leningrad. Here at Factory No.23 (new designation of “Krasni Liotchik”) he began working as director of the construction department. In 1935 with the help of IV Chasovikov he created the PV-23 light seaplane and later devoted himself to improving the Polikarpov U-2 by creating the U-3 and U-4 trainers with improved aerodynamics.

Soon after, Mijelson would work on the MU-4, MU-5 and MU-6 training amphibians. The projects looked very promising, which was confirmed during testing of the second MU-4 prototype in Sevastopol. Almost parapelled Mijelson developed a lightweight torpedo boat named MP and was designed to be transported to the attack area under the wings of a TB-3 bomber. Once the torpedo was released, this aircraft was able to return by its own means to its base and land there.

These designs Mijelson could not finish. At the end of 1937 he was arrested again. Mijelson was charged under article 58 and on January 17, 1938, he was sentenced to the maximum penalty. The next 12 days were torture awaiting the announced end. Nikolai Mijelson was shot on January 29, 1938. His remains rest in an unidentified grave in Leningrad, presumably in the NKVD special cemetery “Levashovskaya Pustosh”.

The continuation of these projects was originally assigned to VL Korvin-Kerber and later to the young architect VV Nikitin, but soon they all ended up being closed. In the opinion of the NKVD an “enemy of the people” could not build anything good.

Mignet HM 1100 Cordouan

Avions Henri Mignet HM.1100 Cordouan first flew in 1998.

The type was not intended to be sold as a kit, but it meets the French ULM or ultralight category, having a maximum take-off weight under 1000 lb.

The fuselage is steel tube framed with a composite shell, and it seats two, side by side. It has a nose wheel undercarriage and although retaining the tandem wings (which traditionally do away with the need for ailerons) Mignet has incorporated ailerons on the rear wing, giving a classic three-axis control via rudder pedals and a single central control stick. If requested a two control model can be made.

Fitted with a Rotax 912, the prototype maximum speed is 117 mph and normal cruise 93 mph. It won’t stall, and it can take off fully loaded from a 260 ft grass strip, and land even shorter. Rate of climb is about 900 fpm.

The Cordouan’s forward wing is entirely free of pitch, control being effected through aerodynamic compensator. The ailerons are on the trailing edge of the rear wing. The fuselage is moulded in composite.

Mignet Aviation HM 1100 Cordouan
Engine: Rotax 912, 80 hp
Wing span: 7.30 m
Wing area: 18.50 sq.m
MAUW: 450 kg
Empty weight: 260 kg
Fuel capacity: 50 lt
Max speed: 190 kph
Cruise speed: 160 kph
Minimum speed: 65 kph
Climb rate: 5 m/s
Seats: 2
Fuel consumption: 14 lt/hr
Price (1998): 260 000 Fht