Conceived to make use of new high-strength steels obtainable from Germany in the late 1920s, the ANT-13 was a small unequal-span staggered biplane single-seat fighter. Utilising steel for the wing spars and the welded truss fuselage – the remainder of the structure being dural – the ANT-13 was fabric covered and powered by a 600hp Curtiss V-1570 Conqueror 12-cylinder water-cooled engine. Armament consisted of twin 7.62mm synchronised guns.
Construction of the prototype, designated I-8, was threatened with cancellation in 1929 through the pressures of higher priority projects at the AGOS, but each worker donated 70 hours to completing the I-8, which was flown on 28 October 1930. Dubbed unofficially the Zhokei (Jockey), the fighter was the first aircraft to exceed 300km/h in the Soviet Union, but the decision not to licence manufacture the Conqueror engine worked against series production of the ANT-13.
Engine: 600hp Curtiss V-1570 Conqueror 12-cylinder water-cooled Max take-off weight: 1424 kg / 3139 lb Empty weight: 960 kg / 2116 lb Wingspan: 9.00 m / 30 ft 6 in Max. speed: 313 km/h / 194 mph Range: 440 km / 273 miles Armament: 2 x 7.62mm synchronised machine guns
Under the military designation R-7, a single ANT-10 was built as a possible alternative to Polikarpov’s R-5, which first flew in 1928 and went on to have a production run of 4,995 in the 1930s.
Tupolev’s project was an all-metal sesquiplane. The shortage of metal was one of the factors which worked in favour of the simple wooden airframe chosen by Polikarpov. For both aircraft the BMW-VI engine was specified, due to its planned Soviet production as the Mikulin M-17.
TsAGI began design work on the R-7 in 1928, when the R-5 was already flying. Its first flight was made on 30 January 1930, flown by Mikhail Gromov. As it was not appreciably better than the R-5, the programme was discontinued six months later.
Engine: 1 x BMW VI, 500hp Max take-off weight: 2920 kg / 6438 lb Empty weight: 1720 kg / 3792 lb Wingspan: 15.2 m / 50 ft 10 in Length: 10.9 m / 36 ft 9 in Height: 3.6 m / 12 ft 10 in Wing area: 49 sq.m / 527.43 sq ft Max. speed: 235 km/h / 146 mph Ceiling: 5500 m / 18050 ft
The ANT-9 was created in AGOS TsAGI (the first was called the Tupolev Design Bureau however, in reality, this machine was originally created at the initiative of the military. The very idea of designing a large (by the then standards) passenger aircraft originated in the mid-1927 within the walls of the Office of Air Forces RKKA (Red Army UWS).
The military was aware that the CAF – Air Force Reserve provided additional development of the aviation industry and related industries, the airfield network, and trained cadres of pilots and ground staff. In the event of war, civilian aircraft would join the military transport aviation. Moreover, in wartime, a passenger plane could turn into a battle plane. The question fot the Scientific and Technical Committee (STC) at UWS was whether it will be a bomber with the ability to transport passengers, or an airliner capable of carrying bombs and machine guns.
On October 27th, 1927 TsAGI specified the basic characteristics of the aircraft speed of at least 190-195 km / h, ceiling 4,500-5,000 meters, payload of 750 kg and a crew of three. The first task was to build a passenger ship used as a military transport plane, the second is the creation on its base bomber modification.
Tupolev found a compromise that allowed a fast and relatively cheap build. He proposed to build a passenger aircraft at the military base. On April 9 1928 at a meeting of the STC, Tupolev reported on the conceptual design of the new aircraft, named ANT-9. It was a three-engine all-metal monoplane with the wing overhead.
Tupolev prepared three options for the project with different engines. The first three engines would be the Gnome-Rhone “Titan”, the second and third – a combination of the two American “Wright” J4 and one French Gnome-Rhone “Jupiter.” The number of passenger seats variants differed in total payload, gross weight, as well as range and speed. The plane with the three Titans of 230 hp provided a small gain in speed and range. Tupolev emphasized the use in the project of components and assemblies of other aircraft that were created in the TsAGI – ANT-3 (R-3), ANT-7 (R-6) and ANT-8. Most borrowed from R-6. From it they took wing and tail.
Evaluation of the project considered the aircraft of modern western standard of the same weight carrying capacity. Tupolev was told that the fuselage was overly broad and could be narrowed to 10-15 cm, however, in general opinion was favorable.
A little later, the Commission on the organization of passenger aircraft, established by order of the UWS June 12, 1928 including representatives from the Air Force, TsAGI, Aviatresta, Osoaviahima and airlines’ Dobrolet. ” Chairman was appointed as deputy head of the UWS Ya.I.Alksnisa. Work on the ANT-9, and labor agreement were decided. Total allocated for the design was 100 thousand rubles. Half of this amount allocated Air Force, and others equally “Dobrolet” and Osoaviakhim. According to the agreement concluded with the TsAGI prototype ANT-9 was required to be presented on May 1, 1929
For the first machine of the three chosen engines were 230 hp Gnome-Rhône Titan. This five-cylinder radial air-cooled engine was developed in England by Bristol, while France produced them under license.
The lead engineer was A.A.Arhangelsky, who also designed the fuselage. Wing was engaged in VM Петляков, шасси – А.Н. Petlyakov, chassis – AN Путилов, оперением – Н.С.Некрасов, силовой установкой – братья Е.И. Putilov, feathers – N.S.Nekrasov, propulsion – the brothers E. и И.И.Погосские. and I.I.Pogosskie. September 24 completed the drawing of the general form.
In fact, re-done with the center fuselage, were landing gear and engines. The fuselage had a cross-section, close to rectangular, and made entirely of kolchugalyuminiya – the German equivalent of the Soviet duralumin. Corrugated sheathing was performed, and the closer to the tail, it took over some loads. Increased rigidity of the fuselage diagonal bands. In the nose housed the central engine. The cabin held two pilots and flight engineer. Inside, was a partition passenger compartment, two rows of the left and right of passage, with nine passenger seats. In the interior there were clothes, luggage room and two toilets (in the documents of that time wrote simply – “toilet”).
The center section was manufactured separately from the fuselage and was attached to its upper longitudinal members with four nodes. The fuselage was made entirely of imported special steel.
The engines frames had rubber bumpers to absorb vibration. Gasoline was placed in the wing tanks. The Titans had wooden fixed-pitch two blade props, specially designed to TsAGI. By November the building of the fuselage and wing of the prototype began. In March, proceeded to the strength tests.
Much of the new machine was bought abroad. From Germany, the entire lighting system, batteries, glass cockpit, fabric and artificial leather for the trim, even the mats. Tupolev liked the wicker chairs of “Merkur” from Dornier. Instruments were to be German and American.
Delays in imports is seriously hampered the assembly. The engines arrived late by three months, with no mufflers. The wheels were brought from France in time though, but smaller in diameter – in Paris trade mission members had mixed the size.
On March 27, the Commission agreed that delays should no longer be tolerated, wanting domestic materials and not waiting foreign arrivals. On April 30th, a day ahead of time, the prototype was ready. In appearance the aircraft had woven reed chairs made a small factory near Moscow. For ventilation all the passenger cabin windows opened, as for heating, there was none.
May 1, 1929 saw the ANT-9 in the middle of Red Square, demonstrating the new Soviet aircraft. A huge cart slowly moved the plane to toward Khodynka, Central Airport, at night.
When at the entrance to the airfield the procession began to cross the tram tracks but from the morning mist suddenly popped a tram. The driver did not have time to brake and the car crashed into a plane. Bending the console and completely blew the roof off the tram, the wing is almost not affected.
Tupolev ANT-9 (URSS-309) was first flown by M.M. Gromov on May 7 (some sources say 5th), 1929 at Khodynka. Originally it had no registration and was painted in natural metal colors. In May 1929, it was registered as URSS-309.
Just a few days was spent piloted by Gromov for factory testing . The plane was very successful. After the first flight Tupolev brought to the airfield his family, and literally forced the pilots to carry the unplanned passengers.
May 16, 1929 started the state tests in the Air Force Institute. The aircraft was piloted by the same Gromov and Stoman for an engineer. The tests were until 28 May and it was noted that the aircraft is stable, the control force small, with no tendency to stall or spontaneously reverse.
Although the ANT- 9 did not meet the requirements to climb above 1,500 m, the practical ceiling and takeoff distance , an overall assessment of the Research Institute of the report was: ” the ANT -9 is a very good passenger aircraft and some quality is undoubted advantage over the best foreign similar power planes.”
Observations made in the Institute concerned secondary issues and were easy to handle : seizing vent in the cockpit, a high level of noise in the cabin. An important point was insufficient deflection angle of the stabilizer. In addition, employees of the Research Institute clearly seized n the process of refueling with gasoline. From a barrel with bucket into the filler neck. To prepare the machine to fly in such a way it took half a day .
Tests were completed by a small flight Moscow- Serpukhov – Kashira -Moscow . Already on June 6 Gromov, co-pilot Mikheev , Spirin navigator and mechanics Rusakov and Monakhov flew the ANT- 9 to Odessa. It was a kind of rehearsal before the tour on the capitals of Europe, scheduled for July. The appearance of the ANT- 9 in Odessa included a courtesy visit to a group of Italian pilots who arrived in flying boats S.55. Chief of Staff of the Italian Air Force de Pinedo even a little fly on the Soviet machine.
On June 6, 1929 the aircraft left for Odessa. On July 10, 1929, with Tupolev on board taking a vacation in Odessa, with a group of his chief of staff and UWS PI Baranov, and Gromov, heading for Kiev. Approaching to the Dnieper, the plane entered rain. Suddenly the speed of the machine began to fall. When she approached the stall speed, they had to make an emergency landing. Swollen blisters on the props had reduced thrust. Remains of fabric were cut off with penknives. Since the area was too small to take off, a portion of gasoline was sent on foot to a nearby village with passengers. With Tupolev on the plane, Gromov took off safely.
On July 10 the aircraft went on an overseas tour. At this time the crew consisted only of Gromov and the mechanic Rusakov. ANT-9 was carrying a group of pilots and journalists. During the month of the “Wings of the Soviets’ they visited Warsaw, Berlin, Paris, Rome, Marseilles and London. The aircraft behaved perfectly. On the Moscow-Berlin Gromov flew 10:00 against a strong wind. Returning on August 8.
The only unpleasant incident occurred over southern France. ANT-9 suddenly went into a dive, and then began to tremble. The pilot immediately landed on a small meadow. After inspecting the aircraft, he said quietly: “Well, I thought – a coffin.” Buffeting arose from the opened hatch on the center from a burst of vibration of a broken engine mount tube. The tube is welded by a local garage mechanics, and ANT-9 flew on.
The fact that the ANT-9 launch into production, was determined in advance. The plane actually did not exist, and it had entered into a five-year plan for development of civil aviation. In the first option plan, prepared in July 1928, three airlines, then existing in our country – “Dobrolet”, “Ukrvozduhput” and “Derulyuft” gathered over five years to put a total of 148 vehicles of this type into service.
Few had the desire to acquire the new aircraft. The aircraft factories Aviatrest was so overwhelmed with orders and flatly refused to release the ANT-9. At the beginning of 1929 Alksnis even appealed to the President of “Dobrolet” V.N.Ksandrovu with a proposal to build the plant themselves in Voronezh. But even if “Dobrolet” would agree to this, the construction would take a long time, and the ANT-9 were needed now.
Aviatrestu began to “twist arms” at all levels. As a result, its leaders surrendered in April and ordered to start commercial production at the plant 22 in Fili – the only one who has had experience in producing all-metal machines. During the summer of 1929 TsAGI had sent drawings to the plant.
Initially it was assumed that the production ANT-9 would also receive ” Titans”. A large batch was ordered from France, but the fall of 1929 in the U.S. a representative went to a Soviet delegation headed by the Chief UWS PI Baranov. There she was negotiating with “Curtiss-Wright” the corporation on the three types of air-cooled engines; the 165, 225 and 320 hp. The last of them, “Wright” J5, was proposed for use of the ANT-9 instead of “Titans.”
December 28, 1929 meeting of the UWS approved the decision to abandon the French engine and put the U.S. engines in all production machines.
The calculations showed that the more powerful, 320 hp Wright J6 would increase the speed and capacity, albeit at the expense of a decrease in range – the same amount of tanks, more “hungry” engines. Firm “Gnome and Rhonw” was sent a formal notice of termination of the contract. Baranov, in January 1930 ordered a small batch of Wrights.
As a prototype decided to use the prototype ANT-9, replacing motors on it. This operation was enacted to implement by 20 February 1930, but actually did not carry out adaptations. Experienced ANT-9 passed the “Dobrolet” with “Titans.” September 15, 1930 returned to TsAGI. January 29, 1931 is registered as a Soviet-L101, transferred to Aeroflot.
But the entire series of 10 planes, planted at the beginning of 1930 the plant ╧ 22, has already had to get the Wright. Half of the machines designed for the Air Force, the other – for civilian pilots. The first six ANT-9 planned to deliver by July 1. Thus, the “unplanned” trehmotornik went into a series of one year earlier than the P-6, on the basis of which it did.
By the summer of several ANT-9 have already collected, but the motors from the United States do not have time. Since the plant was to carry out the plan, and the supply of engines lay on the responsibility of the customers had to start a “conditional” acceptance cars without engines. One such aircraft was in June and two more – in July. “”Wright” also began to mount in August.
Externally, the ANT-9, “Wright” differed from the prototype only in the absence cooks on the screws and partial nosing engines. The screws have others – U.S. Steel bought the firm, “Steel Propeller Corporation.” By eliminating the shortcomings of the prototype, the course of the stabilizer increased. Empty weight increased slightly, mainly due to motoustanovki.
The three 172kW Gnome-Rhone Titan radials were replaced in series machines by domestic M-26s, which proved to be underpowered and were in turn replaced by imported Wright Whirlwinds of 224kW each. After the first batch of some 12 aircraft the design was revised to twin-engined configuration, with two 507kW M-17 engines raising maximum speed from 205km/h to 215km/h; this version was known usually as the PS-9, and about 70 were built.
PS-9
The three-engined ANT-9s served with the Soviet-German airline Deruluft on the Moscow-Berlin service. Some were also operated by the VVS as troop or VIP transports.
The PS-9 was flown widely on passenger services, the most famous being the propaganda aircraft Krokodil, with a suitably decorated plywood nose complete with a set of sharp teeth.
Engines: 3 x 172kW Gnome-Rhone Titan radial Max take-off weight: 6200 kg / 13669 lb Empty weight: 3353 kg / 7392 lb Wingspan: 23.7 m / 78 ft 9 in Length: 16.8 m / 55 ft 1 in Wing area: 84.0 sq.m / 904.17 sq ft Max. speed: 210 km/h / 130 mph Cruise speed: 195 km/h / 121 mph Ceiling: 3750 m / 12300 ft Range: 1800 km / 1118 miles Range w/max.payload: 1000 km / 621 miles Crew: 2 Passengers: 9
Engines: 3 x M-26
Engines: 3 x Wright Whirlwind, 224kW / 365 hp Maximum speed: 205 kph
PS-9 Engines: 2 x M-17, 507kW Maximum speed: 215km/h
Although Tupolev and the TsAGI had been requested to construct a flying boat in 1925, higher priority had been given to his long-range bomber projects and little work was done. But in 1930, with Ivan Pogosski as head, work began in earnest on the ANT-8, which was given the military designation of MDR-2 (MDR = Morskoi Dalnii Razvedchik = Naval Long-Range Reconnaissance).
The designation ANT-8 indicated how long the TsAGI had held back this project, for shortly after its first flight, the ANT-14 flew. The flying boat’s wings and tailplane were derived from the ANT-9, and again an all-metal construction was chosen. The fuselage was given a lot of attention by the design team, and the opportunity was taken to make the floats part of the load bearing structure as well as surface balancing devices. Power was provided by two BMW-VI pusher engines mounted on struts over the wings. It was piloted by S. Riballschuk on its first flight which took place on 30 January 1931. Armament was two DA-2 machine-guns, and it could carry an underwing bomb load of 900kg.
Tupolev regarded the ANT-8 as a proof of concept machine for further development, particularly of hulls. In fact, it turned out to be a worthwhile design in its own right, although the Soviet Navy decided not to proceed with it as it considered the design already dated and unlikely to meet its developing needs.
Only the prototype ANT-8 was built; although several modifications were made to its hull, it remained essentially a one-off experimental aircraft.
Engine: 2 x BMW-VI, 500hp Max take-off weight: 8160 kg / 17990 lb Empty weight: 4560 kg / 10053 lb Wingspan: 23.7 m / 78 ft 9 in Length: 17.03 m / 56 ft 10 in Height: 5.67 m / 19 ft 7 in Wing area: 84.00 sq.m / 904.17 sq ft Max. speed: 166 km/h / 103 mph Ceiling: 3350 m / 11000 ft Range: 1062 km / 660 miles Crew: 5
The Tupolev ANT-7 prototype was a scaled-down version of the ANT-4. First flown on 11 September 1929, it was powered by two 544kW BMW VI engines. Production began in summer 1930 as the multi-purpose R-6 for the air force, with a total of 435 built by June 1934. The KR-6 version was a long-range reconnaissance aircraft with increased fuel capacity and no bombload, and the MR-6 was a naval floatplane variant. Many late production aircraft were delivered for civil use under the designation PS-7 or P-6; modifications were minimal, including a strengthened freight floor and elimination of gunners’ positions. The MP-6 was the civil floatplane version, and many P-/MP-6s and PS-7s had enclosed cockpits for Arctic use. The specially built R-6L was a one-off ‘limousine’ version incorporating a nine-passenger cabin.
R-6 Engine: 2 x M-17 Max take-off weight: 6470 kg / 14264 lb Empty weight: 3855 kg / 8499 lb Wingspan: 23.2 m / 76 ft 1 in Length: 15.1 m / 50 ft 6 in Height: 6.1 m / 20 ft 0 in Wing area: 80.0 sq.m / 861.11 sq ft Max. speed: 230 km/h / 143 mph Ceiling: 4900 m / 16100 ft Range: 800 km / 497 miles Armament: 3 x 7.62mm machine-guns, 500kg of bombs Crew: 3-5
The Tupolev TB-3 all-metal cantilever monoplane was the most advanced four-engined heavy bomber in service in the world in the early 1930s. First flown by M M Gromov on 22 December 1930, it was Tupolev’s first stake to the claim of having built the world’s largest landplane.
The first TB 3s closely resembled the TB 1, and carried the same bomb load, but were more powerful and more heavily armed. The 1936 version, powered by M 34FRN engines, established a number of weight lifting records for the USSR in that year, and in May 1937 four unarmed TB 3s airlifted the Schmidt Polar Expedition to the North Pole.
Production began at the end of 1931, continuing through many modifications until early 1937 when a total of 818 had been built.
Tupolev TB-3 (ANT-6)
For many years the TB-3 was the backbone of the VVS (Soviet air forces) heavy bomber units. A number retained the bureau designation ANT-6 and were used for transport. As the first four engine cantilever monoplane production bomber; it carried 4,410 pounds of bombs and became famous as the carrier craft in the world’s first mass paratroop exercises.
In 1938-39 TB-3s were used operationally against the Japanese, but by the time Germany invaded the Soviet Union in 1941 most had been converted as paratroop or freight transports under the designation G-2. A squadron of six TB 3s, each carrying two fighter bombers, was used against the advancing Germans in 1941.
TB-3 August 1941
Other uses then consisted of night bombing and transport work of all kinds, including the carriage of vehicles or tanks between landing gear legs, and glider towing.
Experiments started with two I 16 fighters, and slowly worked up to five, four of which were rolled up ramps on to cradles fixed to the bomber’s wings, while a fifth joined up in flight, hooking on to yet another version of the trapeze gear used in British and American experiments. To help get this heavy formation airborne the engines of the wing mounted fighters were run up at take off, and once up, the TB 3 could just maintain altitude under its own power.
Use in parasite fighter experiments led in 1941 to Black Sea Fleet TB-3s being used to launch two Polikarpov SPB dive-bomber versions of the I-16 fighter, for raids on pinpoint targets in the Ukraine and Romania.
Variation Grojovski G-52 Flying Battery
TB-3 Engines: 4 x M-17F Max take-off weight: 17047 kg / 37582 lb Wingspan: 39.5 m / 130 ft 7 in Length: 24.4 m / 80 ft 1 in Height: 8.5 m / 28 ft 11 in Wing area: 230.0 sq.m / 2475.70 sq ft Max. speed: 182 km/h / 113 mph Ceiling: 3600 m / 11800 ft Range: 2200 km / 1367 miles Armament: 4 x 7.62 mm machine-guns, 3000kg of bombs Crew: 8
ANT-6 Engines: 4 x AM-34, 830 hp Wingspan: 132 ft 10.5 in Max speed: 155 mph
Designed by Pavel O Sukhoi when a brigade leader of Andrei N Tupolev’s AGOS (Aviatsiya, Gidroaviatsiya i Opytnoye Stroityelstvo – Aviation, Hydro-aviation and Experimental Construction) collective within the TsAGI (Tsentralnyi Aero-gidrodinamicheskii Institut -Central Aero and Hydro-dynamic Institute), the ANT-5 was the first Soviet all-metal fighter. A single-seat sesquiplane powered by a nine-cylinder Gnome-Rhone Jupiter radial of 420hp, the first prototype performed factory testing between 10 August and 25 September 1927. A second prototype, or dubler, with a 480hp Gnome-Rhone Jupiter 9ASB, was flown in July 1928, and underwent state testing between 1 December 1928 and 4 April 1929, series production of the type having meanwhile been initiated as the I-4. The first series I-4 underwent state testing between 15 October and 26 November 1929, subsequent aircraft having the 480hp M-22 engine, a licence-built version of the G-R Jupiter 9ASB, and an armament of twin 7.62mm guns. Second series aircraft had the 4.00sq.m lower wing removed, controllable slats occupying 44.5% of the remaining wing’s leading edge, and a Townend ring-type engine cowling incorporating cylinder helmets. Designated I-4bis in this form, the prototype was tested by the NIl VVS, the Air Force’s Scientific Research Institute, between 11 and 23 September 1931. No further development of the I-4bis was undertaken.
Three I-4s were fitted with very much smaller lower wings for aerial launch and retrieval trials from 31 December 1931 by Vladimir S Vakhmistrov utilising a TB-1 bomber as an Aviamatka, or “mother aircraft”. Devised by V S Vakh¬mistrov to extend the radius of action of fighter aircraft, two I 4 (ANT 5) single seat fighters were to be carried into action on the wings of a TB 1 mother plane. The Zveno 1, as it was known, was successfully tested.
In December 1931, one I-4 was tested with a 76mm Kurchevski recoilless cannon mounted beneath each upper wing half. A total of 369 I-4s was built to January 1934, these equipping 18 eskadrii at their service peak; the type remaining in first-line service through 1933 and for tuitional tasks until 1937.
I-4 Max take-off weight: 1430 kg / 3153 lb Empty weight: 978 kg / 2156 lb Wingspan: 11.40 m / 37 ft 5 in Length: 7.28 m / 24 ft 11 in Wing area: 23.80 sq.m / 256.18 sq ft Max. speed: 231 km/h / 144 mph Ceiling: 7500 m / 24600 ft Range: 840 km / 522 miles
Design work on Tupolev’s first large air¬craft, the twin engined ANT 4, began before the first flight of the ANT 3. It owed much to the three engined Junkers G 23 transport, and was built on the second floor of a former Moscow merchant’s house which formed part of the TsAGI premises. The walls had to be knocked down and the components taken to the Central Aerodrome for assembly before the seven minute first flight on 26 Novem¬ber 1925.
A cantilever low-wing monoplane powered by two 336kW Napier Lion engines, the prototype TB-1 or Tupolev ANT-4 made its maiden flight on ski landing gear on 26 November 1925. Intended mainly for the heavy bomber role, the ANT-4 was of all-metal construction with corrugated metal sheet covering and a glazed nose section.
The second aircraft was the true TB-1 bomber prototype; flown initially in July 1928 it had a redesigned nose section with ‘balcony’-type gunner’s cockpit and a crew of five including three gunners, and was powered by two 544kW BMW VI engines. A third prototype, designated ANT-4bis, had revised engine nacelles and increased armament.
The first series machine was completed as a propaganda aircraft; named Strana Sovietov (Land of the Soviets) it was equipped for a staged flight across Siberia and on to New York but was soon damaged severely in a forced landing. A second aircraft was prepared and completed the journey, using wheels or floats as appropriate, and this second Strana Sovietov (URSS 300) covered 21242km between leaving Moscow on 23 August 1929 and arriving in New York on 1 November.
In its production form, as the TB 1 heavy bomber, the ANT 4 was armed with three pairs of 7.62 mm DA machine guns, in the nose and two dorsal positions. Two hun¬dred and sixteen were produced at the former Junkers concessionary factory at Fili, Moscow, which had been taken over by the Soviet authorities in July 1926.
Production of the TB-1 continued until August 1932, a total of 152 being delivered plus 66 TB-1P twin-float bomber/torpedo seaplanes.
The TB 1 was used for a number of duties (torpedo bomber, freight plane) and was the first Tupolev component of the ‘Zveno’ series of composite aircraft, devised by V S Vakh¬mistrov to extend the radius of action of fighter aircraft. Two I 4 (ANT 5) single seat fighters were to be carried into action on the wings of a TB 1 mother plane. The Zveno 1, as it was known, was first and successfully tested on 3 December 1931.
Pavel Grokhovsky proposed hanging special container under the wings of TB-1 aircraft, capable of transporting paratroopers. Officially these structures were called “Red Soldier Automatic Launchers” (“автоматическими выбрасывателями красноармейцев”). In each container there was a soldier with his parachute. In the landing area, the pilot released the containers, which, pivoting on their attachment to the wing, released their contents. The parachute was opened automatically by a rope attached to the structure. Members of the collective jokingly called the contenders “coffins.”
Parachute launchers under the wings of Túpolev TB-1 bombers.
In the first tests it was Grokhovsky, and later his wife, Lidia Alexseyevna, who were launched from a container under the wing of a TB-1 bomber on July 14, 1931.
In the USSR the first flight with solid fuel accelerators (TTU for the acronym of Tviordo-Toplivnie Uskaritieli) took place in May 1931 and was carried out in a U-1 suitably modified by the engineers of the GAZ No.3 VI Dudakov and VA Konstantinov. The results obtained suggested the possibility of using the method on Tupolev TB-1 heavy bombers. In 1933, 6 accelerators were installed in a TB-1, three on each side of the fuselage, at the junction with the centroplane. Two aircraft were modified. In the first one (No.614) the six accelerators were located above the wing, in the second (No.726) one accelerator was located above the wing and two below. The tests, which concluded in October 1933, showed that with the use of the gunpowder accelerators the takeoff run of the bomber was reduced by 4 times.
The ANT-4s were front-line equipment for a number of years before being relegated to the transport role with the revised designation G-1. Many were used as freighters by Aeroflot and by the Soviet Arctic Aviation Authority (Aviaarktika), final examples of the type being grounded in 1945. The TB-1 was also used in a number of experiments, including autopilot and drone trials, inflight refuelling of other aircraft, rocket-assisted take-offs, and cargo parachute drops. It was the first twin-engined all-metal cantilever monoplane to enter production in the world.
TB-1 Engine: 2 x M-17 Max take-off weight: 6712 kg / 14798 lb Empty weight: 4420 kg / 9744 lb Wingspan: 28.7 m / 94 ft 2 in Length: 18.0 m / 59 ft 1 in Wing area: 121.5 sq.m / 1307.81 sq ft Max. speed: 200 km/h / 124 mph Ceiling: 4800 m / 15750 ft Range: 1000 km / 621 miles Armament: 3 x 7.62mm machine-guns, 700 kg of bombs Crew: 5
The first production aircraft designed and built by Tupolev at TsAGI was the ANT 3 two seat biplane, which made propaganda flights abroad in 1926 and 1927 and was used by the air force for reconnaissance until about 1932.
The prototype flew for the first time in August 1925. An unequal-span biplane, intended for reconnaissance duties, it was of all-metal construction with corrugated sheet covering.
The original 298kW Liberty engine was replaced by a 336kW Napier Lion, the aircraft then being redesignated R-3NL The first 12 series aircraft had Liberty engines but the next 18 had the Soviet development of this powerplant, which was designated M-5. The final 79 aircraft with the 336kW Lorraine Dietrich engine were designated R-3LD, and one ANT-3 was tested with a 507kW BMW VI. Most R-3s saw military service, but a few retaining the ANT-3 designation were flown as mailplanes or used for liaison and for propaganda flights. The R-3LD version had a maximum speed of 205km/h, was armed with three 7.7mm machine-guns and could carry 10 10kg bombs on external racks. Plans for a Shturmovik version with 400kg of armour protection came to nothing.
ANT-3 Engine: 1 x M-5 Max take-off weight: 2103 kg / 4636 lb Empty weight: 1351 kg / 2978 lb Wingspan: 13.0 m / 43 ft 8 in Length: 9.9 m / 33 ft 6 in Height: 3.9 m / 13 ft 10 in Wing area: 36.0 sq.m / 387.50 sq ft Max. speed: 204 km/h / 127 mph Ceiling: 4600 m / 15100 ft Range: 750 km / 466 miles Armament: 3 x 7.62mm machine-guns Crew: 2
The ANT 2, completed in 1923, was a single engined, three seat monoplane, with cabin accommodation for two pas¬sengers. It had a thick multi spar wing, triangular section fuselage and thin cor¬rugated duralumin covering, called Kol¬chugalumin after the village where it was produced. The overall design was not un¬like that of the Junkers K 16 of 1922, and indeed a close study of Junkers design and practice had been made at TsAGI since the first Junkers C.1 was captured during the civil war. Tu¬polev’s ANT 2 represented an advance over the Junkers concept of the all¬-metal (corrugated aluminum alloy), cantilever low wing monoplane. First flew on May 26, 1924.
ANT-2 Engine: 1 x Bristol Jupiter Max take-off weight: 836 kg / 1843 lb Wingspan: 10.5 m / 34 ft 5 in Length: 7.6 m / 25 ft 11 in Height: 2.1 m / 7 ft 11 in Max. speed: 170 km/h / 106 mph Ceiling: 3000 m / 9850 ft Crew: 1 Passengers: 2
All Aero 