Ginga variants and projects

The Yokosuka P1Y1 was designed in 1940, following a specification of the IJN clearly inspired by the Junkers Ju 88. The P1Y1 turned out to be a complex and difficult to maintain aircraft that only came into service when the war was lost for Japan.

Forced by circumstances to make long journeys over the sea with some unreliable engines, all missions of the Frances had some suicidal quality. These bombers were so valuable to the IJN that the decision to carry out a conventional or suicidal attack was left up to each pilot, depending on the circumstances of each combat. The first Tokko attack was made by a Frances in flames that had been reached by the AA, against the destroyer USS Ammen (DD-527) in Leyte Gulf, on November 11, 1944. On the 15th of the same month, the first Reppu suicide unit was formed, with aircraft from the 763rd Kokutai.

On the 25th, six airplanes of the Shippu and Kyofu units made the first suicide attack on an Allied Task Force, 15 nm off Manila. Several Frances were shot down by the Hellcats of the aircraft carriers USS Ticonderoga and USS Essex, but an aircraft of the Kyofu-Tai, loaded with two bombs of 507 kg, impacted the aircraft carrier USS Intrepid (CV-11) east of Lamon Bay. On March 11, 24 P1Y1 bombers of the Azusa Special Attack Unit, from the 762nd Kokutai, were guided by a Kawanishi Emily flying boat, flying during 12 hours, heavily loaded with two detachable fuel tanks of 600 lt and a bomb of 807.5 kg, in order to attack the US naval base at Ulithi Atoll.

Most of these aircraft were forced to abort the attack because of engine problems and adverse winds. Only two of them reached Ulithi and one impacted the aircraft carrier USS Randolph (CV-15) damaging the flying deck. On March 18, ten aircraft of the Ginga Unit again damaged the USS Intrepid, east of Kyushu. On May 7, another nineteen Frances of the 4th Mitate Tokubetsu Kogekitai were forced to abort Operation Tan No. 3 that was to be a second attack against Ulithi, again due to engine failures. On the 25th, three aircraft of the Ginga Unit No. 10 managed to sink the destroyer USS Bates (DE-68), 2 nm south of Le Shima.

Between November 14, 1944 and May 25, 1945, no less than 218 Frances of the suicide units Reppu, Shippu, Kyofu, Doto, Gufu, Kusanagi, Mitate, Ginga, Azusa, Yubu and 501st Special Attack Squadron, carried out attacks against Allied ships and airfields in Lamon Bay, Kossol Roads, Leyte, Sulu Sea, Davao, Okinawa, Leyushu, Ryukyu Islands, Kikai Islands, Ulithi Atoll and Taiwan.

In the summer of 1944, a certain number of aircraft of the P1Y2-S Kyokko type entered service with the 302nd Kokutai. They had been specially modified as night fighters to operate against the B-29s, but the experiment was a failure because the Kyokko lacked the ceiling to reach the Superfortress due to the poor performance of its new engines Kasei 25a. The slightly different version P1Y1 Byokko that was manufactured by Nakajima, was also not very successful and the IJN ordered all night fighters were retrofitted to the bomber role.

In July 1945, the first flight tests of the Mukade were conducted in the Arsenal of Yokosuka. The Mukade was a modification of the Frances specialized in long range strafing role against the US bases of B-29s. The project was inspired by the ventral armament of the Irving and consisted of twelve 20 mm cannons angled at 30 degree downwards and fired from an altitude of 200 m over the rows of refuelled and bombed-up B-29s. It was hoped that a fireball effect would take place with entire ranks of Superfortress blowing each other up.

The Mukade tactics were part of the Operation Ken-Go consisting of attempting an attack against the USAAF base at Iwo Jima using thirty six Frances of the Mitate Unit No. 6, thirty six Mukade and thirty G4M bombers that had been modified for transporting suicide commands. There was also the project of the P1Y3 Mod.33, a Frances with enlarged fuselage and extended wingspan specially modified as a mother ship for the Ohka Mod.22 jet bomber.



-Night Fighters

Yokosuka Ginga, Kawanishi Kyokko, Nakajima Byakko and Kugisho Tenga

The Yokosuka P1Y1 Ginga was designed in 1940, following a specification of the IJN (clearly inspired by the Junkers Ju 88) requiring a fast bomber that would be suitable for dive-bombing and low-altitude torpedo attack.

On March 1945 some units of the P1Y1 Model 11 of the 762nd Kokutai were equipped with an H-6 ASV radar to perform nigh attacks against U.S. Navy ships. The P1Y was tested in alternative roles.

Early in 1944 the Kawanishi Company was instructed by the Kaigun Koku Hombu to produce a night fighter variant under the designation P1Y2-S Kyokko Model 26. The new planes would be powered by two 1,850 hp Mitsubishi MK4T-A Kasei 25a radial engines, that were considered safer than the Homare 12 del Ginga, and armed with a

Type 5, 30 mm cannon angled at 35 degree in Schräge Musik configuration. The prototype flew in June 1944 and Kawanishi modified a total of 96 Ginga airframes.

Between March and November of 1944, a certain number of Kyokko entered into service with the Kokutais Nos. 302 and 321, but they were not successful against the B-29s. The low speed of 523 kph and the service ceiling of 9,400 m only proved disappointing. The plan was to install the FD-2 AI radar in the series version.

Kakajima also built the P1Y1-S Byakko night fighter, a Ginga armed with two Type 99-2, 20 mm cannons, angled at 30 degree in Schräge Musik configuration. In the summer of 1945, the P1Y1-S performed operational tests with the 302nd Kokutai basedo in Atsugi. Byakko performed better than Kyokko but also did not enter service. At least one P1Y1-S was equipped with a H-5/FD-1 AI radar, an experimental version of the H-6 ASV with Yagi antenna, that had been specially designed to generate less drag in the nose.

In July 1945, the first flight tests of the Mukade conversion were conducted in the Arsenal of Yokosuka. The Mukade was a modification of the Ginga specialized in long range strafing role against the US bases of B-29s. The project was inspired by the ventral armament of the Gekko and consisted of twelve 20 mm cannons angled at 30 degree downwards and fired from an altitude of 200 m over the rows of refuelled and bombed-up B-29s. It was hoped that a fireball effect would take place with entire ranks of Superfortress blowing each other up.

The Mukade tactics were part of the Operation Ken-Go consisting of attempting an attack against the USAAF base at Iwo Jima using thirty-six Gingas of the Mitate Unit No.6, thirty-six Mukade and thirty G4M bombers that had been modified for transporting suicide commands. There was also the project of the P1Y3 Mod.33, a Ginga with enlarged fuselage and extended wingspan specially modified as a mother ship for the Ohka Mod.22 jet bomber. The Model 33 did not go beyond the drawing board.

After the Battle of the Coral Sea in May 1942 the IJN admitted the need to have a ground based fast reconnaissance airplane. Little afterwards, the Naval Air Arsenal at Yokosuka received the specification 17 Shi to design an aircraft that could fly at 666 kph at an altitude of 6,000 m. Under the project name Y-30, it was assigned to two teams that would study the different possibilities of a single or a twin-engine airplane.

The R1Y1 Seiun would have had a classic airframe and been propelled by a Mitsubishi 24-cylinder, liquid cooled, 2,500 hp experimental engine. The R1Y2 Gyoun would be an evolution from the Ginga with two Mitsubishi Mk10A (Ha-214) 2,400 hp radial engines. The Seiun engine did not prove to be acceptable on the medium term and the estimated performance of the Gyoun showed that it did not comply with the requirements of the 17 Shi. Dr. Masao Yamana, of Kugisho, suggested the use of German inline engines, paired inside the fuselage, to build the R2Y1 Keiun with a single nose propeller and long power shaft. The formula did not work and the team of Kugisho proposed to the IJN its transformation into a suicide fast bomber with two Ne-30 turbojets.

The opportunity to have these new engines reactivated the Gyoun, using a Yokosuka P1Y1 Ginga as a prototype, propelled by the two turbojets under the wing nacelles. The final model was known as Tenga and would have probably been propelled by two Ne-130 turbojets with a power equivalent to that of a German Jumo 004. The most important modifications, compared to the Ginga series, included the adoption of a solid nose cone and the installation of the main undercarriage legs between the engines and the fuselage.

Tenga speculative technical data

Wingspan: 20 m, length: 15 m, height: 4.30 m, wing area: 55 sq.m, max weight: 10,500 kg, estimated max speed: 700-750 kph, estimated service ceiling: over 10,000 m, engines: two Ne-30 centrifugal turbojets with 850 kgf peak thrust or two Ne-130 axial turbojets with 900 kgf peak thrust.
 

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Mukade bibliography
-Arawasi May 2006, Issue 4
-Famous Aircraft of the World Special Ginga, Burindo , 2000
-Rikko to Ginga, by Yasuho Izawa, Asahi, Sonorama, 1995.
-Famous Aircraft of the World Nº. 50, Hiryu, Burindo, 1974
-Saraba Kuchu Senkan FUGAKU, by Yoshiro Ikari, Kojinsha, 2002.
-Fugaku by Maema Takanori, Kodansha, 1991
-Japanese Military Aircraft Ilustrated, Vol.2, Bombers, Burindo, 1982.
 
Excellent information as usual my brilliant Justo-san!!:)
 

Japanese website discussing development process of P1Y. I was using it to find performance estimates for the P1Y5, but as I had to rely on a translator, I'm fairly certain a lot of information was lost. Otherwise, a good article with lots of information and pictures.

Might have to start learning Japanese...
 
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It seems Plexiglass was used to some extent on the Ginga. How come acrylic wasn't used to form bubble canopies on the fighters, like the P-47D?
 
So the Tenga was not armed then? Or are there not enough documents to determine this?
 
So the Tenga was not armed then? Or are there not enough documents to determine this?

After the Battle of the Coral Sea in May 1942 the IJN admitted the need to have a ground based fast reconnaissance airplane. Little afterwards, the Naval Air Arsenal at Yokosuka received the specification 17 Shi to design an aircraft that could fly at 666 kph at an altitude of 6,000 m. Under the project name Y-30, it was assigned to two teams that would study the different possibilities of a single or a twin engine airplane.

The R1Y1 Seiun would have had a classic airframe and been propelled by a Mitsubishi 24 cylinder, liquid cooled, 2,500 hp experimental engine. The R1Y2 Gyoun would be an evolution from the Ginga with two Mitsubishi Mk10A (Ha-214) 2,400 hp radial engines.

The Seiun engine did not prove to be acceptable on the medium term and the estimated performance of the Gyoun showed that it did not comply with the conditions of the 17 Shi. Dr. Masao Yamana, of Kugisho, suggested the use of German technology inline engines, paired inside of the fuselage, to build the R2Y1 Keiun with a single nose propeller and long power shaft. The formula did not work and the team of Kugisho proposed to the IJN its transformation into a suicide fast bomber with two Ne-30 turbojets.

The opportunity to have these new engines reactivated the Gyoun, using a Ginga as a prototype, propelled by the two turbojets in under wing nacelles position. The final model was known as Tenga and would have probably been propelled by two Ne-130 turbojets with a power equivalent to that of a German Jumo 004. The Tenga could have just been built as suicide bomber within the Kokoku Heiki No.2 programme, carrying an anti ship bomb inside. The most important modifications compared to the Ginga series included the adoption of a solid nose cone and the installation of the main undercarriage legs between the engines and the fuselage. This single seat aircraft also included the usual Kokoku Heiki complements of machine guns in the nose and rockets launchers under the wings.


Technical data

Type suicide bomber

Airframe light alloy and steel

Wingspan 20 m

Length 15 m.

Height 4.30 m

Wing area 55 sq.m

Maximum weight 10,500 Kg

Engines two Ne-30 centrifugal turbojets with 850 kgf peak thrust or two Ne-130 axial turbojets with 900 kgf peak thrust

Estimated maximum speed 700 to 750 kph

Estimated service ceiling over 10,000 m

Crew one

Armament two type 3 machine guns of 13 mm in the nose, four under wing I.S.R. 12 cm decoy rocket launchers, one number 30 Model 2, 807.5 kg anti-ship bomb.
 
I find it somewhat strange that there were turbojet-powered suicide aircraft, especially those using the better engines (Ne-130, Ne-20, etc.), considering the costly manufacture of these turbojets, and the fact that there were other cheaper suicide aircraft in production or on the drawing board, such as the Shinryu and Ohka
 
I find it somewhat strange that there were turbojet-powered suicide aircraft, especially those using the better engines (Ne-130, Ne-20, etc.), considering the costly manufacture of these turbojets, and the fact that there were other cheaper suicide aircraft in production or on the drawing board, such as the Shinryu and Ohka

I would guess that three factors applied:

* The high value of the targets--capital ships, particularly carriers and large amphibious assault ships--offset the cost of the aircraft.

* To be effective, the suicide aircraft had to evade radar pickets, penetrate high- and low-level fighter screens, evade destroyer-fired, proximity fused shells, and penetrate short-range AA, all of which were getting more effective in 1945.

* German and, presumably, Japanese-built versions of German jet engines had extremely short working lives no matter how they were used--more like contemporary cruise missile engines than modern aircraft engines.
 
I find it somewhat strange that there were turbojet-powered suicide aircraft, especially those using the better engines (Ne-130, Ne-20, etc.), considering the costly manufacture of these turbojets, and the fact that there were other cheaper suicide aircraft in production or on the drawing board, such as the Shinryu and Ohka




Kugisho MXY7 Ohka

Fortunately for the Allies, the piloted missile Kugisho MXY7 Ohka proved to have some flaws in the design when entered combat at the last stages of the WWII. As it happened with the German V-1, the Ohka could be intercepted by Allied fighters. This was actually the fact that saved the U.S. NAVY from retiring from the Philippine Sea with large losses of men and ships in March 1945.
The MXY7 Ohka Model 11was a small mid-wing monoplane with a fuselage of duralumin and wings and tailfins of wood. It has been designed by a transport pilot of the 405th Kokutai, Mitsuo Ohta, in August 1944. He inspired himself on the radio guided German bombs Hs 293 and Fritz-X that were launched from an aircraft flying almost on the vertical of the target.
The initial sketch, or Marudai Project, was presented to the Ichigisho design team, First Naval Air Technical Arsenal at Yokosuka. The team, responsible for building the prototypes and performing the flying tests, was integrated by engineers Tadao Mitsugi, Rokuro Hattori and Masao Yamana. Mass production of the 855 units was made in the Kugisho workshops, First Naval Air Arsenal at Katsumigaura, while the manufacturing of components was distributed between Fuji Hikoki and Nippon Hikoki.
The operational procedures established that the Ohka should be launched from between 16 and 37 km of distance to the target and at between 6,000 and 8,200 m of altitude. Following its flying profile, the Mitsubishi G4M2e Model 24J bombers that carried them were usually detected by the radars of the Allies from a distance of 130 km. Once detected, the fighters on CAP missions over the fleet could intercept the Bettys 111 km from the target. The powerful anti-aircraft defence deployed by the Allies warships in 1945 made almost impossible that a conventional bomber could fly with impunity over one of its Task Groups.
During its first combat on March 21, 1945 the 18 Bettys of the 721st Kokutai were shot down by Hellcat fighters when they were more than 90 km to the target. All Ohka units fell to the sea, without their pilots, well before the launch point. The Betty could just fly at 240 kph if loaded with an Ohka of 2,140 kg. Its only surviving possibility was reaching the launch point by surprise.
In the Okinawa Area, 69 Bettys escorted by 150 Zeros made ten attacks against the invasion fleet between March 21 and June 22, 1945. They launched 66 Ohkas of the Jinrai Corps (Oka Special Attack Group), sank the DD-733 Mannert L. Abele destroyer and damaged the BB-48 West Virginia battleship, the DD-478 Stanly and DD-774 Hugh W. Hadley destroyers, the DM-30 Shea minelayer, the DMS-27 Jeffers minesweeper, the APA-47 Alpine Attack Transport and the YMS-327 light minesweeper.
Previous to launch, the Betty initiated a shallow dive until reaching the take off speed of between 280 and 325 kph. The Ohka flight began as a shallow, unpowered dive, on a 5º 35’ gliding angle, reaching a cruise speed of between 370 and 450 kph. Some of the machines of the Model 11 last series carried a couple of Toku-Ro.1 Type 1 rockets under the wing roots that generated 300 kg of thrust during 10 seconds with the purpose of increasing its speed and range.
At a distance of between 3,000 and 8,000 m from the target, the pilot pressed the button on the top of the control stick to start the electric ignition of the three Toku-Ro.1 Type 2 rockets at the rear section of the fuselage. Each rocket had a length of 179 cm and a diameter of 25 cm, weighted 115 kg and contained 44 kg of solid fuel capable of generating 600 kg of thrust during 30 seconds. After the ignition, the pilot initiated the final 50º dive on the target reaching a terminal speed of 933 kph.
The Ohka could not be intercepted by the fighters at this stage and its course could only be altered by a direct impact from the heavy AA, due to the inertial momentum of the heavy warhead. Not even the pilot could alter its course as the pressure exercised by the air on the tail surfaces in transonic flight was superior to any muscular work applied to the flight controls.
The warhead had been designed for the destruction of major warships. It had a hardened steel warhead to pierce any armour deck and contained 512 kg of Trinitroanisol explosive. It had a length of 180.6 cm (without the nose priming plug) and a diameter of 60 cm and a weight of 1267 kg, including the three rear bolts. It had a wind air-armed fuse in the nosecone that automatically unblocked itself when the Ohka was released by the launch airplane. There were also four impact fuses at the rear of the warhead, activated by means of a T-handle located to the front right of the cockpit. The pilot carried a parachute for those cases when the bomb fell to the sea before reaching the target. The communication with the launch airplane was made by lights on the instrument panel and a one-way Gosport system of rubber tubing.
Trying to solve some of the operational shortcomings of the Ohka Model 11, the Model 21 was designed as a smaller version that could be carried by the fastest bomber available, the Yokosuka P1Y1 Ginga Model 11. The wingspan was reduced from 5.1 to 4.12 m. due to the smaller space available between the undercarriage legs of the Ginga. The warhead was also reduced to 600 kg. The Model 21 kept the three accelerator rockets of 30 seconds located at the rear section, while the 10 seconds rockets located under the wing roots were replaced by Type 3 rockets of 20 seconds. A one-third reduction in wing area meant that the handling characteristics of the Model 21 were far worse than those of the Model 11 and its range was inferior in spite of using five rockets. In July 1945, during the flight tests of the only prototype built, one of the rockets located under the wings did not ignite and the Ohka went completely out of control. The machine was destroyed and the pilot died.
It was decided to do without the rockets and replace them with the Tsu-11 thermo jet developed by the Kugisho engineers in 1944, based on the Italian technology on the Campini compressor. Originally designed to drive the Yokosuka MXY-9 Shuka, the school version of the rocket interceptor J8M1 Sushui, the Tsu-11 consisted of a conventional reciprocating engine, a single stage compressor wheel and a combustion chamber containing an annular fuel injection system and two igniters plugs that burned the air-fuel mixing creating a thrust of 250 kg.
The reciprocating engine was a 4-cylinder inverted, in line Hitachi Ha 11 Hatsukaze II of 105 hp (Japanese version of the German Hirth HM 504-A2). The Tsu-11 had a length of 220 cm, a diameter of 64 cm and a weight of 200 kg. At full throttle the reciprocating engine reached 3000 rpm and the compressor 9000 rpm. It was flight tested under the bomb bay of a Ginga by the end of 1944.
The version equipped with a Tsu-11 was named Ohka Model 22 and was built in a number of fifty units at the factories of Ichigisho, Aichi Kokuki, Fuji Hikoki, Miguro Hikoki and Murakami Hikoki, although only three of them were actually finished with the Tsu-11 for flying test. To transport the Ohka Model 22, a modified version of the Ginga P1Y3 Model 33 was designed following the model of the Junkers Ju 88 H-1 long range bomber. Its fuselage was enlarged 4 m and its wingspan increased to 22 m.
The operational procedure of the Model 22 established that the Ha 11 should be started by ground crews before take off, using the fuel provided by the Ginga during the flight, until launch. Compared to the system used in the Betty, the Ginga did not have enough room in its bomb-bay for the Ohka pilot to have access to it from the launch airplane. Therefore, he should stay within the Ohka at take off and communicate with the crew in the Ginga using a Gosport system.
Model 22 carried the same warhead of 600 kg than the previous design. A fuel tank of 225 litres was installed between the warhead and the main spar, another of 65 litres between the pilot seat and the engine and a third one of oil, of 10 litres, housed in a dorsal fairing behind the teardrop canopy. The new design had a range of 130 km that allowed the Ginga to reach safety before the fighters arrived. However, its cruise speed was just of 443 kph at full rpm, which made it an easy prey for the Hellcats and Corsairs that surpassed 600 kph. To accelerate during the final plunge, a Toku-Ro.1 Type 3 single rocket with 600 kg of thrust peak during 20 seconds, was suspended under the fuselage, equipped with front and rear cowling to reduce the air drag of the underpowered airplane. The rocket could be detached by a T-handle located on the floor in front of the pilot. Handling at high speed was improved by replacing the control cables from the Model 11 by a system of traction-resistant articulated bars.
To amend the low speed issue of the Model 22, the Tsu-11 was replaced by a Ne-12 B turbojet with a four stage compressor that had been originally developed by Ichigisho to propel the new jet fighter Nakajima J8N1 Kikka. The Ne-12B was a variant of the Ne-12, a centrifugal turbojet based on the German designs Heinkel-Hirth HeS 8 and HeS 8a , that was lighted up to 350 kg. It had 180 cm of length and a diameter of 74 cm producing 319 kg of thrust at 15,000 rpm.
When the technical information on the more powerful BMW 003 A axial turbojet, with a smaller diameter than the Ne-12 B, was received from Germany by mid July 1944, it was decided to improve its performance. This was actually made by increasing the compressor stages, to reduce the rpm, and adopting a combustion chamber of smaller diameter, similar to the one in the BMW 003A. The new design was named Ne-20, measured 275 cm of length and 62 cm of diameter, weighted 450 kg and produced 475-500 kp of thrust. Its mass production was decided as power plant for the Kikka.
Most of the 40 units of Ne-12 B that have already been built could then be assigned to propel the new series of Ohka designated as Model 33. This model had the same wings and tail surfaces than Model 11, although a little longer fuselage and a warhead of either 800 kg containing 315.2 kg of TNT+PETN or of 900 kg containing 415 kg of RDX explosive. It measured 133 cm of length (without the nose priming plug) and 55 cm. of diameter. The Ohka Model 33 carried one single fuel tank of 250 litres located between the warhead and the main spar. It had a range of 213 km, much wider than the Model 22, and a speed of 643 kph, a little faster than the Hellcat and equivalent to the Corsair speed. The launch airplane should have been the four engine bomber Nakajima G8N1 Renzan that could carry an Ohka suspended under the bomb bay in long range missions or two Ohkas suspended under the wings in medium range missions.
There was a plan to convert part of the production of the Ohka Model 11 to the Model 33 by the end of the war. Considering the limited number of available Ne-12 B engines and Renzan airplanes, the mass production would have not been above thirty units. The Model 33 did not use auxiliary rockets. The possibility of having some of the new Ne-20 turbojet engines by mid 1945, to drive missiles and Tokko airplanes, led the Aichi Kokuki engineers to design the Ohka 43 series. However, the nearly 3 m of length of the engine forced them to adopt a longer fuselage and the lack of the right launch airplanes and the new power of 500 kp available with the Ne-20, advised the creation of an airplane able to take off by itself, fitted with wooden wings and tail planes of a considerable size. The wingspan was widened from 5 to 8.972 m affecting the maximum speed that decreased to values below 600 kph and therefore left it exposed to interception.
The proposal was to build two variants designated Ohka 43-Ko and Ohka 43-Otsu at the Aichi-Gifu and Aichi-Oyaki factories. The first one was a replacement of the Aichi M6A1 Seiran that would be carried and launched from the new Sen Toku submarines of the I-400 series. Its watertight deck hangar had 31 m of length and 3.5 m of diameter and could house either four Ohkas or three Seirans or two Saiuns or four Baikas.
The Ohka, with backward foldable wings, moved over rails along the hangar, fixed to launching cars of 700 kg that could adjust their height and slope to several types of airplanes. With the submarine on the surface, the launch sequence was made with the help of two teams of four and six men respectively and went through a defined procedure. First, manual unblock and opening of the hangar door by means of an hydraulic mechanism; then, connection of the hangar rails with those in the launch ramp using two detachable rails. The Ohka was then pulled over its launch cart up to the start of the ramp (of 24 m of length and 3º 30' of slope) and the whole combination was fixed to the hook of the submarine steam catapult. The hangar door was then closed and secured, the wings unfolded and blocked and starter of the Ne-20 connected to an external wall socket. The Ne-20 was then started and the wall socket disconnected. The pilot gets in the cockpit and tests the telephonic connection with the bridge, the control surfaces, the throttle and the compass. The submarine now sails facing the wind at its maximum speed of18.7 km and the pilot selects ‘full throttle’ at 11,000 rpm. The crew takes refuge in the conning tower before the catapult is fired, the Ohka takes off and the cart falls to the sea.
In case of individual missions the submarine dives to reach a new launch position. For multiple launches, the well trained crew may launch the four Ohkas in 12-15 minutes. The pilots were equipped with parachutes but did not need radio equipment or oxygen to fulfil their mission. Their assignments might be either to attack the Allies fleets located in Ulithi and Pearl Harbour or vital centres located in the west coast of USA, or to destroy the Gatun and Miraflores floodgates of the Panama Canal, the task for which the Seiran had been designed.
The Ohka 43-Ko carried the same warhead (version of 800 kg) than the Ohka Model 33 but without the nose priming plug. Its fuel tank capacity was of 400 litres and it was located between the warhead and the main spar. The oil tank of 16 litres was between the pilot seat and the turbojet. It could reach targets placed 278 km from the launch point.
The ‘Ko’ version did not use auxiliary dive rockets. It released the folding wingtips by means of electrically activated explosive bolts, during the terminal dive to increase its speed. It was expected that it could surpass the 900 kph when reducing its wingspan to just 2.6 m. At this stage control was obtained by using the tail surfaces that could move in differential mode to act as ailerons. In normal configuration, the Model 43 had 13 sqm of wing surface, 4º 30' of dihedral angle and 2º 30' of tail plane incidence.
The ‘Otsu’ version was designed to take off from a 110 m length straight railway section and hide in the railway tunnels with its wings folded. Developed to avoid the use of conventional aerodromes in a situation of complete aerial superiority of the enemy, it was inspired by the launch procedure of the Messerschmitt P.1079 (July 3, 1942). The idea was to use it in a long range coastal artillery role to counteract the invasion of southern Kyushu, or ‘Olympic Operation’, which was expected to happen on November 1, 1945.
The Model 43-Otsu used a launch cart for take off similar to one used by the naval version but propelled by two Toku-Ro.1 Type 2 rocket engines with 600 kg thrust each and 30 seconds of life and by the power of its own Ne-20 turbojet. At the end of its run the cart was detached and braked by a cable and a counterweight system. At that moment, a third Toku-Ro.1 Type 3 rocket with 600 kg peak thrust and 20 seconds endurance automatically ignited. This was fixed to the fuselage centreline and its nozzle had an 8º 45' slope to make the thrust axis and the gravity centres of the Ohka converge, thus providing maximum lift.
The land version used the same warhead than the naval one but it was armed with two Type 3 machine guns of 13 mm with a rate of fire of 800 rpm located between the warhead and the fuel tank, which capacity had been reduced to 300 lt, and a combat range to 200 km. The guns configuration was inspired by the German air to air rocket bomber Sombold So 344 project and its objective was that the Ohka could break its way towards the Allies Task Forces fighting against the defensive fighters to which it was equal in speed. The ‘Otsu’ kept the mechanism to detach the wingtips of the naval version but was not considered a requirement to equip it with accelerator rockets for the terminal dive. It was expected that it would be able to surpass the 900 kph in a 50º dive with the Ne-20 at full throttle.
All the combat versions of the Ohka were protected from the rear against 12.7 mm ammunition of the Browning M2 machine guns used by the U.S. NAVY interceptors. The pilot seat was armoured and 15 mm steel plates were installed behind his head and shoulders and in the cabin floor under his legs. Frontal armour was considered impossible as the state of technology at the time could not produce armoured glass able to stop the 40 mm projectiles of the naval AA.
Two version of training were built to make the pilots familiar with the Ohka weapons system. The K-1 was an unpowered aircraft with landing skid and warhead replaced by water ballast. It was then succeeded by its refined version K-1-KAI Wakarazuka, derived from the Ohka 43. It was a two seat airplane with double flying controls and one Type 4 Mk I Model 10 rocket for ignition testing. A training rocket catapult with a 100 m long ramp was built in Takeyama, to the west of Yokohama, over a hill of 600 m of altitude located 3,000 m from the airfield where the Ohka gliders should land. Forty five Ohka K-1 and two K-1-KAI were manufactured before Japan surrendered to the Allies.
The Ohka Model 11 that took part in the first combats was overall painted in bright blue. Afterwards a paint scheme was adopted with pale green upper surfaces and pale grey under surfaces. The known units of the Model 22 were overall light grey. The training version units were painted in bright orange at the manufacturing plant, then receiving a dark green coating in the upper surfaces only. In all piloted versions the cockpit interior was factory applied dark green.



Technical Data Model 11 (Model 21) ((Model 22))

Wingspan 5.1 m (4.12 m) ((4.12 m))

Length 6.07 m (5.62m) ((6.88m))

Height 1.16 m (1.16 m) ((1.15 m))

Wing area 6 sqm (4 sqm) ((4 sqm))

Max weight 2140 Kg ((1450 kg))

Max Speed 648 Kph ((443 kph))

Max diving speed 926 kph

Warhead 1267 kg (600 kg) ((600 kg))

Fuel ((290 litres))

Oil ((10 litres))

Range 36 km ((130 km))

Engine 3 rockets (5 rockets) ((one TSu-11))

Launch G4M2e (P1Y1) ((P1Y3))



Technical Data - Model 33 (Model 43A) ((Model 43B))

Wingspan 5m (8.97m) ((8.97m))

Length 7.2 m (8.16 m) ((8.16 m))

Height 1.15 m (1.3) ((1.3))

Wing area 6 sq.m (13 sq.m) ((13 sq.m))

Max weight 2120 kg (2270 kg) ((2260kg))

Max speed 643 kph (596 kph) ((596 kph))

Warhead 900 kg (800 kg) ((790Kg))

Fuel 250 litres (400 litres) ((300 litres))

Oil 10 litres (16 litres) ((16 litres))

Range 213 km (278 km) ((200 km))

Engine one Ne-12B (one Ne-20) ((one Ne-20))

Launch G8N1 (Submarine I-400 Class) ((Railway))
 

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Incredible amount of information, and thank you for the insightful reply to my question
 
The Tenga is a jet fighter bomber planned by the Imperial Japanese Navy.

The aircraft was being developed as a successor to the land bomber galaxy by the Navy Aviation Technical Arsenal (Air Engineering Arsenal). Development was started in 1943 (Showa 18), and in 1944 (Showa 19). The plan continued even when the prototype models were sorted out, but the end of the war is still at the planning stage.

The engine that was planned to be installed is the axial flow turbojet engine "Ne 30" (ground static thrust: 850 kg) that was developed by Aircraft Factory, and the test was conducted with an experimental aircraft that mounted the ne 30 on the galaxy. Later, the Tianhe prototype was scheduled to be built. The first machine of Ne 30 was completed in October 1944, but it was not fully tested by the end of the war.

Ne 30

Source : Japanese blog
 
The Tenga is a jet fighter bomber planned by the Imperial Japanese Navy.

The aircraft was being developed as a successor to the land bomber galaxy by the Navy Aviation Technical Arsenal (Air Engineering Arsenal). Development was started in 1943 (Showa 18), and in 1944 (Showa 19). The plan continued even when the prototype models were sorted out, but the end of the war is still at the planning stage.

The engine that was planned to be installed is the axial flow turbojet engine "Ne 30" (ground static thrust: 850 kg) that was developed by Aircraft Factory, and the test was conducted with an experimental aircraft that mounted the ne 30 on the galaxy. Later, the Tianhe prototype was scheduled to be built. The first machine of Ne 30 was completed in October 1944, but it was not fully tested by the end of the war.

Ne 30

Source : Japanese blog
Galaxy= Ginga:)
 
Hi! Ginga with two torpedo plan and with multi cannons.
Source : Kugishi(海軍航空技術廠), ISBN978-4-05-605289-3
 

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Hi! Ginga with two torpedo plan and with multi cannons.
Source : Kugishi(海軍航空技術廠), ISBN978-4-05-605289-3
I suppose the first could be Ginga Model 33 long range bomber , the second photo seems be multicannon night fighter variant.
 
The Gyoun was a reconnaissance aircraft planned by the Imperial Japan Navy. The prototype name is "17 Experimental Land Reconnaissance Aircraft", the abbreviation code is "R1Y", and the prototype number (actual number) is "Y-30".

development
The basic design has been underway since around 1939 (Showa 14), and the high-altitude recording machine "Y-30" aimed at breaking the world record, as the predecessor, aiming for a land reconnaissance aircraft with excellent speed and cruising performance that exceeds the Army's Type 100 command reconnaissance aircraft, and in December 1941 (Showa 16), the Naval Aviation Arsenal (Air Engineering Arsenal) started planning. Full-scale design began in the summer of 1942 (Showa 17) with Technical Major Shio Otsuki as the chief designer, and the first prototype was scheduled to be completed around the end of 1943 (Showa 18).

However, due to the fact that the design value was below the required performance, and the situation in the Battle of the Solomon Islands worsened, it became necessary for reconnaissance aircraft to have a high-altitude flight capability and a smaller size than the cruising range, so in March 1943 the design drawing work was completed to about 85% and wind tunnel tests using models were carried out. Subsequently, based on an alternative proposal submitted by Technical Major Masao Yamana during development, the development of a new 18-test land reconnaissance aircraft (later "Keium") was started.
 
design
Gyoun was a three-seat twin-engine aircraft, and the performance requirements were as follows:

It is possible to equip a pressurized airtight chamber in the future.
The scout seat should be at the front.
Capable of local reconnaissance and maritime patrols.
The maximum speed is 667 km/h (360 kt, at an altitude of 6,000 m.
It has a cruising range of 7,410 km (4,000 nautical miles at 4,000 m) at a cruising speed of 436 km/h (250 kt).
Initially, the engine was planned to be equipped with a single "Nu" (5,000 hp) in the nose, which is a combination of two liquid-cooled H-type 24-cylinder "ME2A" (output 2,500 - 3,000 hp) under development by Mitsubishi Heavy Industries, but it was changed to Mitsubishi "MK10A" (output 2,400 hp) or "MK10C" twin-engine to ensure visibility for the occupants. Initially, the maximum speed that the MK10A could achieve was planned to be 685 km/h (370 kt, at an altitude of 8,000 m), but due to difficulties in the development of the MK10A and a change in the supercharger used, the maximum speed was reduced to 648 km/h (350 kt, at an altitude of 6,000 m), which was 19 km/h (10 kt) short of the required speed. In the future, it was estimated that the engine would be equipped with a three-speed supercharger and would be able to achieve a maximum speed of about 722 km/h (390 kt at an altitude of 10,000 m).

The laminar flow type "LB wing" was adopted for the main wing, and the structure was divided into an outer wing and a center wing so that it could be easily connected to the fuselage. In addition, the fuselage and wing spars[2] structure, materials, and assembly jigs were shared with the land-based bomber "Galaxy" developed at the Air Engineering Factory at the same time, thereby shortening the development period. In the galaxy, the bomb bay is used as a fuel tank, and the wings are also equipped with semi-integral tanks.
 
In addition, during development, by Technical Major Masao Yamana, Aichi Aircraft's "Atsuta 30" liquid-cooled inverted V-type 12-cylinder engine equipped with an exhaust turbine is twinned and built into the fuselage, and the maximum speed is 741 km / h (400 kt, altitude 10,000 m)[8][9], cruising range 3,334 - 3,704 km (1,800 - 2,000 m). An alternative proposal was submitted that emphasized speed rather than cruising power. This idea was regarded as influential by the leadership and led to the later Keiun, but there was also strong opposition that it was unsuitable as a practical aircraft due to the complexity of the aircraft structure.

Specifications (planned values, final time)
Source: "Japan Aviation Academic History (1910-1945)" p. 10, "Japan Aircraft Catalogue Aichi Air Engineering Factory" p. 186.

Length: 15.0 m
Wingspan: 19.0 m
Wing area: 50.0 m2
Own weight: 10,500 kg
Gross weight: 14,000 kg
Engine: Mitsubishi MK10A[7] or MK10C[6] Air-cooled double-row radial 18-cylinder (MK10A: 2,400 hp) × 2
Maximum speed: 648 km/h (350 kt, altitude at altitude of 6,000 m), 704 km/h (380 kt, altitude of 9,000 m)
Cruising range: 7,408 km (4,000 nautical miles at 4,000 m)
Crew: 3 people

From Japanese source
 
Hi!
Overall length of Gyoun and Ginga was 15m.

 

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If I adjust the length, the span of Gyoun is strange.:confused:
 

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View attachment 731188
ORIGINAL blueprint for fuselage assembly from the document “P1Y1 fuselage strength calculation book”. I have the original pdf and if anyone need that pls reply to this comment
Do you have any on the later ginga variants perhaps? Such as the P1Y2-P1Y6
 
The opportunity to have these new engines reactivated the Gyoun, using a Ginga as a prototype, propelled by the two turbojets in under wing nacelles position. The final model was known as Tenga and would have probably been propelled by two Ne-130 turbojets with a power equivalent to that of a German Jumo 004. The Tenga could have just been built as suicide bomber within the Kokoku Heiki No.2 programme, carrying an anti ship bomb inside. The most important modifications compared to the Ginga series included the adoption of a solid nose cone and the installation of the main undercarriage legs between the engines and the fuselage. This single seat aircraft also included the usual Kokoku Heiki complements of machine guns in the nose and rockets launchers under the wings.
So the Tenga evolved from the R1Y2 project? Definitely a surprise to learn that.
Also, considering the addition of the solid nose cone to the suicide attacker version, why the 13mm machine guns?
 
So the Tenga evolved from the R1Y2 project? Definitely a surprise to learn that.
Also, considering the addition of the solid nose cone to the suicide attacker version, why the 13mm machine guns?



Tenga evolved from P1Y1
In August 1944 the Japanese Technical Office Kaigun Koku Hombu published the specifications for the project Kokoku Heiki (Empire Weapon). It required the manufacturing of three classes of suicide airplanes that carrying a bomb of 800 kg would be capable of attacking the invasion fleets.

Kokoku Heiki Go.1 was a transformation program of existing naval airplanes to optimize their use in suicide missions. Based on the experience acquired with the Zero and the Val, the proposal was to modify the Kawanishi N1K1-J Shiden, the Mitsubishi J2M Raiden, the Yokosuka D4Y Suisei, the Nakajima B6N Tenzan and the Aichi B7A Ryusei.

Kokoku Heiki Go.2 should be a suicide bomber propelled by two centrifugal turbojets TsU-11, Ne-12 or Ne-30. Nakajima’s proposal was to manufacture the Maru-Ten whereas Yokosuka/Kugisho proposed the R2Y2 Keiun and the Tenga.

Kokoku Heiki Go.3 should be a conventional and easy to manufacture airplane, using non-strategic materials and designed to allow the installation of several types of reconditioned surplus engines. Kawanishi proposed the Tokko-Ki, Nakajima the Tsurugi, Sowa the Toka and Tachikawa the Ta-Go.

The 20 mm guns were removed to reduce weight, leaving two type 97 machine guns of 7.7 mm as the only armament to defend from the Allied fighters. It had been ascertained that the Kamikaze pilot could better estimate distances and angles for an optimal impact if the tracer bullets were shot during the terminal dive.

By the end of 1944, the suicide bombers started to use I.S.R. type rockets of 12 cm to distort the aiming of the AA Allied gunners during the terminal dive. These rockets had been originally developed for Antiaircraft Artillery usage, with incendiary pellets and shrapnel warhead, in imitation of the German Föhn. They could be mass shot from a square matrix or one by one from iron tubes similar to the German W.GR 21.The Suisei carried two or four tubes under the wings, something that was generalized for all the airplanes of the Kokoku Heiki Go.1.
 
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Tenga evolved from P1Y1
In August 1944 the Japanese Technical Office Kaigun Koku Hombu published the specifications for the project Kokoku Heiki (Empire Weapon). It required the manufacturing of three classes of suicide airplanes that carrying a bomb of 800 kg would be capable of attacking the invasion fleets.

Kokoku Heiki Go.1 was a transformation program of existing naval airplanes to optimize their use in suicide missions. Based on the experience acquired with the Zero and the Val, the proposal was to modify the Kawanishi N1K1-J Shiden, the Mitsubishi J2M Raiden, the Yokosuka D4Y Suisei, the Nakajima B6N Tenzan and the Aichi B7A Ryusei.

Kokoku Heiki Go.2 should be a suicide bomber propelled by two centrifugal turbojets TsU-11, Ne-12 or Ne-30. Nakajima’s proposal was to manufacture the Maru-Ten whereas Yokosuka/Kugisho proposed the R2Y2 Keiun and the Tenga.

Kokoku Heiki Go.3 should be a conventional and easy to manufacture airplane, using non-strategic materials and designed to allow the installation of several types of reconditioned surplus engines. Kawanishi proposed the Tokko-Ki, Nakajima the Tsurugi, Sowa the Toka and Tachikawa the Ta-Go.

The 20 mm guns were removed to reduce weight, leaving two type 97 machine guns of 7.7 mm as the only armament to defend from the Allied fighters. It had been ascertained that the Kamikaze pilot could better estimate distances and angles for an optimal impact if the tracer bullets were shot during the terminal dive.

By the end of 1944, the suicide bombers started to use I.S.R. type rockets of 12 cm to distort the aiming of the AA Allied gunners during the terminal dive. These rockets had been originally developed for Antiaircraft Artillery usage, with incendiary pellets and shrapnel warhead, in imitation of the German Föhn. They could be mass shot from a square matrix or one by one from iron tubes similar to the German W.GR 21.The Suisei carried two or four tubes under the wings, something that was generalized for all the airplanes of the Kokoku Heiki Go.1.
So does this mean that the Tenga and the R2Y2 (not including the interceptor type of the latter) were never intended for more traditional attacker/bomber uses? I mean this as in R2Y2 having a similar intention to the HS-132 (minus the divebombing), and the Tenga being similar to the Ar-234 and B-45.
 
By the same way, an amazing fact that Kyokko the night fighter also had JET version, at the same time, the P1Y7(not Tenga) was also a Jet version of Ginga.
Tenga was an individual project and shouldn't be count as a variation of Ginga, however there would be a Ginga with two TR30s for test purpose
 
By the same way, an amazing fact that Kyokko the night fighter also had JET version, at the same time, the P1Y7(not Tenga) was also a Jet version of Ginga.
Tenga was an individual project and shouldn't be count as a variation of Ginga, however there would be a Ginga with two TR30s for test purpose
Does that mean there were 3 jet projects pursued at various points in time by the IJN (Kyokko conversion, P1Y7, Kugisho Tenga) which used the Ginga's airframe as a starting point? Would appreciate it if there is more info available on the P1Y7 and how it'd differ from the Tenga project.
I've never heard of the TR30 before, is it a synonym to the Ne series turbojet or something of indigenous Japanese design?
 
Does that mean there were 3 jet projects pursued at various points in time by the IJN (Kyokko conversion, P1Y7, Kugisho Tenga) which used the Ginga's airframe as a starting point? Would appreciate it if there is more info available on the P1Y7 and how it'd differ from the Tenga project.
I've never heard of the TR30 before, is it a synonym to the Ne series turbojet or something of indigenous Japanese design?
I looked up the TR-30 and the Smithsonian came up:
Apparently it was an enlarged TR-12B.

EDIT:
According to this page the "TR-30" might just be another name for the Ne-30(?):
 
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Does that mean there were 3 jet projects pursued at various points in time by the IJN (Kyokko conversion, P1Y7, Kugisho Tenga) which used the Ginga's airframe as a starting point? Would appreciate it if there is more info available on the P1Y7 and how it'd differ from the Tenga project.
I've never heard of the TR30 before, is it a synonym to the Ne series turbojet or something of indigenous Japanese design?
1. TR30 is exactly NE30
2. There are actually 4 jet variants except Tenga. They are:the jet Kyokko,the jet version of Ginga Prototype 3(jet engine was on the fuselage),the jet version of P1Y7(ginga type 15)that use TR10 or Hatsukaze motorjet,and the test base for Tenga
 

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