Type 91 torpedo

Type 91 torpedo
250px Type 91 torpedoes aboard an aircraft carrier.
Type	Aerial torpedo
Place of origin	Japan
Service history
In service	1931–1945
Used by	Imperial Japanese Navy
Wars	World War II
Production history
Designer	Rear Admiral Shoji Naruse and his team
Designed	1930–1945
Unit cost	20,000 yen (in the year 1941)
Specifications
Weight	848 kg (1,870 lb)
Length	5.270 m (17.29 ft)
Diameter	45 cm (18 in)
Maximum firing range	2,000 m (2,187 yd)
Warhead weight	323.6 kg with high explosive 235 kg, (713.4 lb with 518 lb) for Type 91 warhead rev.3
Engine	wet-heater type, 8-cylinder radial engine 200hp
Wingspan	69 cm (27¼ in. in the air), 66 cm (26 in. in the water)
Speed	42 knots (77.8 km/h, 48.3 mile/h)
Steering system	gyrocompass guided vertical rudder control system, gyroscope guided anti-rolling controller system
Launch platform	single-engine carrier-based attack aircraft, twin-engine land-based attack aircraft

The Type 91 was an aerial torpedo of the Imperial Japanese Navy which was designed to be launched from an aircraft. It was used in naval battles in World War II.

The Type 91 aerial torpedo had two unique characteristics:

• Wooden attachments on the tail fins, that acted as aerodynamic stabilizers, which were shed upon water entry.
• An angular acceleration control system (PID controller) to control rolling movements, which was very advanced for its time.

This system made it possible to release the Type 91 not only at a cruising speed of 180 knots (or 333 km/h, 207 mile/h) at an altitude of 20 m (66 ft), but also in a power-glide torpedo-bombing run at the Nakajima B5N2 Kate's maximum speed of 204 knots (or 378 km/h, 234 mile/h).

The Type 91 torpedo was 450 mm (17¾ in) diameter. There were five models put into service, with high explosive warheads weighing 213.5 kg to 526.0 kg (or 470.7 lb to 1160 lb) and having effective ranges of 1,500 m to 2,000 m (or 1,640 yd to 2,187 yd) at 42 knots (77.8 km/h or 48.34 mph).

Since the Type 91 torpedo was the only practical aerial torpedo of the Imperial Japanese Navy, it was simply known as the Koku Gyorai, or aerial torpedo. Surface warships and submarines used other types of torpedo, namely the Type 93 and Type 95 respectively, while the Type 97 torpedo was designed for use by midget submarines.

Thunder fish

The Thunder fish, type 91 torpedo (modification 2), was a shallow water aerial torpedo that was designed for and used in the attack on Pearl Harbor in 1941. Conventional torpedoes when launched from aircraft would dive to 100 ft before turning up to hit their targets. The waters of the lagoon at Pearl Harbor were much shallower so wooden fins were added to allow for shallow launching at low altitude.

The name Thunder fish is a literal translation of the Japanese gyorai, meaning "torpedo" (gyo = fish, rai = thunder).

The tactic was practised at a bay on Kyūshū island which resembled Pearl Harbor before being used in the attack in December 1941, launched from "Kate" B5N torpedo bombers. The plan for attack was designed by naval air strategist Minoru Genda for Admiral Isoroku Yamamoto in the face of opposition from the majority Japanese navy view that victory could be achieved by the "The Great All-Out Battle" tactic of luring United States battleships into a major action at sea.

The torpedo measured 18 feet 0 inches (5.49 m) in length, with a diameter of 1 foot 5.7 inches (0.450 m), and weighed 1,841 pounds (835 kg), with an explosive charge of 452 pounds (205 kg). It had a range of 2,200 yards (2,012 m) and a speed of 42 knots. A slight variant was used to sink HMS Prince of Wales and HMS Repulse, launched from "Betty" G4M bombers in an action in the South China Sea three days after Pearl Harbor on December 10, 1941.

Specifications

Here is the list of the series of Type 91 aerial torpedoes, production models.

Type 91 Aerial Torpedo, rev.2 Specifications

Item	-
High explosive	204 kg (449.7 lb)
Speed	42 knots (48.33 mile/h)
Range	2,000 meter (2,187 yard)
Diameter	45 cm (17¾ inch)
Weight	838 kg (1,847 lb)
Length	5.427 meter (17.81 ft)
Engine	200 hp, wet-heater type, 8-cylinder radial engine

Variations

Type 91 Aerial Torpedo and Type 91 Warhead, operational models

Main body	Warhead	High explosive (kg)	Speed (knots)	Range (m)	Total Length (m)	Diameter (m)	Total Weight (kg)	Head Length (m)	Head Weight (kg)	Comments
Type91	Type91	149.5	42	2,000	5.270	0.45	784	0.958	213.5	-
Rev.1	Rev.1	149.5	42	2,000	5.270	0.45	784	0.958	213.5	Supported shedding wooden tail plates in 1936
Rev.2	Rev.2	204.0	42	2,000	5.470	0.45	838	1.158	276.5	Body reinforced in 1938, anti-rolling controller in 1941
Rev.3	Rev.3	235.0	42	2,000	5.270	0.45	848	1.460	323.6	-
Rev.3	Rev.3_rev.	235.0	42	2,000	5.270	0.45	848	1.460	323.6	Reinforced warhead
Rev.5	Rev.3_rev.	235.0	41	1,500	5.270	0.45	848	1.460	323.6	Precision forging and stainless cast steel in body
Rev.5	Rev.7	420.0	41	1,500	5.710	0.45	1080	1.900	526.0	Warhead designed to break bilge

The later, heavier models had a decreased range; this was not an operational problem as close launching was required for accuracy in any case. There were two versions in the Type 91 warhead rev.3, differing in design maximum launch speeds.

Other Japanese aerial torpedoes

The Type 92 electrical (battery powered) aerial torpedo never made it beyond trial stage.

The Type 94 aerial torpedo was based on the highly successful Type 93 torpedo. The Type 93, called the "Long Lance" by the Allied press, was a massive (2.8 tonnes fueled) weapon of superior performance, due largely to the use of compressed oxygen as a propellant instead of compressed air; pure oxygen has approximately five times the reactant capacity in regard to common fuels as the same mass of mixed gasses found in air. The Type 94 emerged from development somewhat smaller, similar to the Type 95 torpedo - a type also derived from the Type 93 and used successfully as a submarine weapon. It was nonetheless a heavy, unwieldy device and never deployed operationally.

Yokosuka air arsenal began development of a 2 tonne large aerial torpedo for 4-engine Nakajima G8N land-based attack aircraft, in spring 1944. It was called Shisei Gyorai M (Trial model torpedo M), or simply 2 tonne torpedo. This was an enlarged version of Type 91 aerial torpedo, its diameter was 533mm (or 21 in, the diameter of standard Imperial Navy submarine torpedo tubes), length 7.10 m (about 23 ft 4in), total weight 2,070 kg (4,564 lb), with a huge 750 kg (1,653 lb - about 50% larger than similar weapons of the era) warhead.

But the Type 91 aerial torpedo project members did not regard it as a series of Type 91 aerial torpedo. It would have been the largest aerial torpedo in the Imperial Japanese Navy Air Force, but the since the operating concept became outdated, that torpedo remained uncompleted work. This G8N or the 18th trial model 4-engine bomber was called "Type 18 prototype land-based attack aircraft".

Tactics

The original Type 91 aerial torpedo entered service in 1931, corresponding to the year 2,591 of the Imperial Japanese calendar, leading to its model designation. This was the beginning of a protracted developing process toward a true aerial torpedo culminating in 1941.

Classic tactic

The first revision of the Type 91 aerial torpedo needed to be launched carefully, with the airspeed not exceeding 130 knots (or 240 km/h, 150 mile/h) and at an altitude no higher than 30 m (98 ft), with slower airspeeds resulting in better precision. This 'classic' approach was actually easier to carry out in obsolete biplanes or planes with fixed landing gears, whereas the modern, fast Nakajima B5N as used by the IJN carrier strike force's 1st Air Flotilla was not an easy plane to handle at these slow airspeeds.

The development project team at Yokosuka Naval Arsenal of Ko-Hon or Imperial Japanese Navy Air Service reasoned that the maximum range of any aerial torpedo could be less than 2,000m (or 2,187 yd, 1.08 nautical mile). When aircraft launches a torpedo in running speed 40 knots, the targeted ship steaming at 30 knots would surely turn hard to maneuver around. It is mandatory for torpedo-bomber pilot attacking, or running into the target as close as possible.

The second tactic

Another approach, called the second tactic, was developed for torpedo-bombing runs in shallow water ports. Here, the aircraft was supposed to fly in at an even slower 100 knots (or 185 km/h, 115 mile/h) and at an altitude of 10 m (32.8 ft) in the midst of intense AA fire. The only way to do this in a B5N2 was to lower the landing gear and flaps to increase drag and lift. The aviators of torpedo-bombing units trained this in the shallow waters of Kagoshima Bay by late August 1941 but felt uncertain about their chances of success.

The first tactic

The torpedo-bomber unit of the carrier Akagi was the first to receive ten samples of the new rev.2 torpedo in August 1941. It was a marked improvement, allowing an approach in excess of 160 knots (or approx. 300 km/h, 185 mile/h) and at 20 m (66 ft) altitude.

Immediately all the torpedo units changed to the first tactic, the gears and flaps are retracted in the wings and flew in faster speed at higher altitude .

• A torpedo released at a range of 800 meters (875 yd) from the target at a speed of 300 km/h, at height of 60 meters (196 ft), would dive into the water entry point 290 meters ahead in 324 km/h, at an entry angle of 22 degrees, after 3.5 seconds. That torpedo runs under the water for 500 meter, and hits the target after 21 second.
• A torpedo released at a range of 620 meters (678 yd) from the target at a speed of 300 km/h (185 mile/h), at height of 10 meters (33 ft), would dive into the water entry point 120 meter (130 yd) ahead in 304 km/h (190 mile/h), in entry angle of 9.5 degrees, after 1.4 seconds. The torpedo will then run under the water for 500 meters (547 yd), and hitting the target after 21 seconds.

In the morning of the Coral Sea, on May 8, 1942, B5N torpedo-bomber units of The 5th Air Flotilla penetrated the American defenses at 0910[JST], swooped to USS Lexington (CV-2) and USS Yorktown (CV-5). USS Yorktown CV-5 was attacked by four B5N2s in one unit of Zuikaku (Lucky Crane), led by squadron leader Lt Cmdr Shimazaki, and averted all four torpedoes. Large USS Lexington CV-2 was attacked by 3 units of total fourteen B5N2s, and was struck by the last two torpedoes to port. The Lt Sato unit of Zuikaku attacked first, followed by the Lt Iwamura unit, and the last was the Lt Ichihara unit of Shokaku (Flying Crane), in the crane wings attack formation. Those B5Ns were approaching to the ship in the full speed over 204 knots (or 378 km/h, 235 mile/h) faster than known torpedo-bomber aircraft should. Captain Frederick Carl Sherman in the bridge of CV-2 watched a B5N shot down with the torpedo near the ship. He saw that the tail section of the torpedo was covered with box-like attachment. He reported that he had found the reason why the B5N2s could launch Type 91 aerial torpedo at such high speed.

Fast torpedo-bombing tactic

As for a high speed torpedo bombing run in 300 knots (or 556 km/h, 345 mile/h), the maximum altitude for release was limited at 300 – 350 m (984 - 1,148 ft). The strength of contra-rotating propeller limited launch height . A torpedo, tested at 100 m in very high speed from P1Y land-based attacker Ginga at Yokosuka arsenal, veered upon water entry because of a crack in a screw blade. The minimum release height was also limited to 40 m (131 ft) in a high speed run. If it were released lower than 30 m (98 ft) in a high speed run, the torpedo might skip on the water's surface.

With authorization from the Imperial Japanese Navy Air Force, Army Air Force pilot, Major Hideo Sakamoto established the fast torpedo-bombing tactic, with his Ki-67 twin-engine bomber aircraft having good maneuverability, at Yokosuka Naval airbase in January 1944. He found the releasing parameters of the tactic after 300 tests. A Ki-67 with 1 tons torpedo starts steep dive at an altitude of 1,500m (approx. 5,000 ft) above water level and launches the torpedo in two styles.

1. Launch in speed range 370–460 km/h, at 30-120m high (or speed 200-248knots (230-285mile/h) at altitude 98–394 ft)
2. Launch in speed range 460–560 km/h at 50-120m high (or speed 248-302knots (285-348mile/h) at altitude 164–394 ft)

Skidding right and left

Tactics were needed because the killed in action rate of aviators in torpedo bombing squadrons was high, 30 - 50% in the beginning of World War II. In the latter stages of the Pacific War, the rate was up to 90% and 100% during daytime operations.

Skilled aviators had their own tactics to survive, skidding right and left with varying speed (180 knots to 70 knots) at less than 10 meters high in the midst of water splashes of AA gunfire, to avoid a curtain of intense AA barrage controlled by the Fire-control system typical of US Navy warships.

A photo shows the typical tactic of torpedo bombing, a B6N Tenzan in torpedo bombing attack of USS Yorktown (CV-10). The original series of photos shows the sequential right and left side-skidding tactic of the crew. In this second photo, the B6N is skidding to its left, or toward the right in the photo, and the flak shell explodes to its right, or to the left in the picture. It was coming up to counterattack near the Truk islands, in the evening of February 17, 1944. It was one of four B6N Tenzan of a torpedo squadron in 2nd A.G or 582 A.G. Two out of four aircraft ditched on their way back and the crews were rescued. The remaining two aircraft returned safely to base. Original photo is PD, the Property of US Government.

Type 91 history

Chronological Table

1931 Type 91 aerial torpedo is into service, start production.

1936 Revision 1. Self-detachable wooden plates are introduced.

1937 Launch-tests at 500m and 1,000m with wooden damper.

1939 Revision 2 starts production. The sinking level after water entry becomes big problem.

1941 Revision 2 cleared the test of shallow water launching by introduction of anti-rolling controller. Battle of Pearl Harbor, Battle of offshore Malay.

1941 Revision 3 starts production.

1942 Battle of Indian Ocean, Battle of the Coral Sea, Battle of Midway, Battle of the Santa Cruz Islands.

1943 Revision 5 starts production.

1944 Battle of offshore the Marianas Islands, Aerial Battle of offshore Formosa.

Scientists and engineers developing aerial torpedo

Ninety One Association includes Rear Admiral Naruse, Lt Cmdr Haruo Hirota, Lt Cmdr Makoto Kodaira (Matsunawa), Naval assistant manager Iyeta, Naval engineer Noma, Naval engineer Moritoshi Maeda, Lieutenant Hidehiko Ichikawa, and Teruyuki Kawada, university student as naval apprentice.

Captain Fumio Aiko was assigned in charge of promoting the development project of Type 91 aerial torpedo since 1931. Capt F. Aiko concentrated human resources to make an aerial torpedo, ordered to analyze the cause and to make anti-rolling controller. He is very proud of the Type 91 aerial torpedo as his great achievement.

Delay of the development

In the beginning of 1934, Kan-Pon or Imperial Japanese Navy Technical Department, an operating division of the Ministry of the Navy of Imperial Japanese government, which had the primary responsibility for naval weapon systems, had their own plan and their own project for a Japanese aerial torpedo. In their plan, a big flying boat was to carry heavy Type 93 oxygen torpedoes, to launch at long range, and then turn back towards safety. This soon proved to be an unrealistic desk plan. Kan-Pon confidentially developed their own Type 94 aerial torpedo, an aerial version of the Type 93 oxygen torpedo. Their original challenge of the latest type of giant H6K Type 97 Large Flying Boat, Mavis was just accomplished the test flight successfully in 1934.

They even ordered to stop production of Type 91 torpedo, which significantly delayed the development schedule based on Type 91. This frustrated the project members of Yokosuka Naval Arsenal.

Wooden tail stabilizers

The project revised Type 91 aerial torpedoes, as the revision 1 supporting wooden tail plates, taken off on water entry, in 1936. The team demonstrated the launching tests of Type 91 aerial torpedoes wearing wooden shock-damper objects at altitude 500m (1,640 ft) and 1,000m (3,281 ft) in the following year, 1937. The project came up again and resumed the development of Type 91 aerial torpedo. Type 91 aerial torpedo of earlier revision had a frail body.

It was revised as the revision 2 by reinforced the frail body structure, in 1938.

Anti-rolling controller

Type 91 aerial torpedoes won the admiration by the anti-rolling controller with acceleration control system of early days. Type 91 already had a shed-off type wooden tail plates as aerodynamic stabilizer. But the running out problem merged as aircraft speed going up from 130 to 180 knots.

Before the anti-rolling controller was introduced, the early revision of Type 91 aerial torpedo had a serious problem as other aerial torpedoes had in those days. Roughly released in high speed, it even made double-roll in the air. When it dove into the swelling waves of the heavy sea, it got spinning moment at the hard impact on water entry. It was veering the running direction, going down to stick to the bottom of the shallow basin of a port, crashing at the depth limits 100m by the water pressure, jumping out of the water, skipping water surface, or even running backwards. Only the real razor aviators could make the sure torpedo-bombing run in the calm sea.

A tumbled torpedo runs out of control. Though the gyrocompass and the depth meter works well, the torpedo cannot control the running direction by tail rudders unless they are in the neutral position at first. Once the torpedo rolls, the horizontal and vertical rudders lose their positions, or even upside down, result in runaway.

Engineers and scientists of the project, led by Lieutenant Hirota, drew one conclusion from their years of tests and numerical analyses, in 1939. Since the specification of launch speed of aircraft was increased from 130knots to 180knots and faster, any aerial torpedo needed an anti-rolling system with not only damping stabilizer function but also acceleration controlling function, otherwise the torpedo would be falling into unstable-state. The idea of acceleration-control, or counter-steering function was thought of as impossible in those days. Two years passed.

The breakthrough on aerial torpedo design was made with the anti-rolling controller invented first by Iyeda, Assistant Manager of arsenal workmen, in spring 1941.

Ten days later, while the test of Iyeda system was in practice, Naval Engineer Noma invented another system, and it was put into final test in August 1941. It functions all the same with different mechanism. During the prototype tests, the Noma's system found out the better for having less time lags in response, so that the Noma system was adopted for production type of Type 91 aerial torpedo.

It looked merely a tiny mechanical air valve object controlling small roll rudders on both sides in the aft of the torpedo, was really the innovation of the torpedo technology world. It was the breakthrough for aerial torpedo. Type 91 rev.2 aerial torpedo first made it possible to use in the high seas.

The anti-rolling controller is actually a steering controller to stabilize the rolling motion of the torpedo by roll rudders on both sides. The roll rudders work within angler range +/-22.5 degrees, twisting in ailerons manner. When a torpedo is rolling or rolls to some degree, the anti-rolling controller twists those rudders in the counter-rolling direction. When a torpedo is rolling back to its neutral position of 0 degree, the controller sense it and switches roll rudders in the opposite direction to break angular velocity of torpedo rolling back, or countersteering. They naval engineers called this operation as countersteer as they modeled it to steer a ship.

It enabled to keep Type 91 rev.2 aerial torpedo running under the water no deeper than 20 meter (65.6 ft). Actually the cutting-edge pilots of torpedo-bomber squadrons in Dai Ichi Koku Sentai or The 1st Air Flotilla of the carrier strike force were able to launch their torpedo so as to sink in the water depth no more than 10 meter (32.8 ft) after water entry. Anti-rolling controller made aircraft possible to torpedo-bomb not only warships anchorage in shallow military port but also warships steam in chopped waves of heavy sea in full speed.

Increment of the explosive weight

The anti-rolling controller also made Type 91 aerial torpedo possible carrying heavier warhead section. Type 91 warhead and Type 91 rev.1 warhead, each weighs 213.5 kg (470.7 lb) with high explosive 149.5 kg (329.6 lb) only, but warhead rev.2 weighs 276 kg (595.2 lb) with high explosive 204 kg (449.7 lb). Warhead rev.7, which is for twin-engine bomber, weighs 526 kg (1160 lb) with high explosive 420 kg (925.9 lb). It was so designed to pierce the reinforced tough armor plates the latest USS warships developed during World War II.

Aerial torpedo technology of the Allies

Engineers and scientists of the Imperial Japanese Navy got a chance to inspect the torpedo technology of the Allies, in aerial torpedoes captured at South West Pacific bases in early 1942. The US Navy aerial torpedo, Mark 13 torpedo was found at Sangley Point, the military port in the Philippines. Fleet Air Arm aerial torpedoes of the Royal Navy were found at the base Kota Bharu, northeastern Malaysia, close to the Thai border.

There were none like Type 91 aerial torpedo rev.2. They were disappointed with the work of their rivals, because those were as if they had few intentions to deal seriously with the development of aerial torpedo technology. The US Navy's aerial torpedo had little differences aside from being capable of being loaded in aircraft and looks almost the same as the bigger Mark 13 ship torpedo. The Royal Navy had their traditional type aerial torpedo, which had been originally designed by White Head Company in 1925.

The structure of Type 91 aerial torpedo rev.2

Type 91 aerial torpedo is the first aerial torpedo, which is able to use practically in ocean. The scientific approach consistent with experimental evidence was adopted to lead development.

Type91_aerial torpedo rev3, structural drawing

Warhead

Length = 1,460 mm (57⅝in)

When a torpedo hits a ship, the inertia forces the aft mass in the initiator to thrust forward and ignite the high explosive in the initiator. The high explosive in the warhead will not detonate unless initiated as designed. A 20 mm explosive cannon shell can go through the warhead without igniting the stable high explosive in the warhead.

The warhead has T shaped strip parts to reinforce the internal-lower portion of the front shell against the heavy impact on water entry. For the production model, the warhead section needs five reinforced strip bands on the front-bottom of the inner shell, lap welded in a shape of cut lower half star, or the superpose of the letter T and the letter Λ, instead. The warhead also has two tiny stitch lines aligned on the front-top of the shell to enhance the explosion. The latest version had two hooks on the nose.

Type 91 aerial torpedo is to be launched by aircraft power gliding from high in the sky. The aerial torpedo, released at altitude 100m, is falling in speed nearly Mach 0.5 on water entries, and receives over 100G at the hard impact on the water surface.

Air chamber

L = 1,068 mm (42⅛in)

The air chamber is a cylinder of thin shell made by alloy of nickel chromium-molybdenum steel. This tough steel alloy was originally developed for steel armor plate of battleship. The chamber is charged with highly compressed normal air at 175 - 215 atm (2,500 - 3,000 psi), which burns fuel oil to produce driving power. It loses the pressure down to around 50 atm (710 psi) while running 2,000 m (6,600 ft) under the water.

Front float

L = 733 mm (28⅞in)

Front float section has a pure water tank, a fuel oil tank and a depth meter.

The depth meter is placed at the inner bottom of the section to detect the water depth level. It detects the displacement level of the water depth and controls the tail horizontal rudders (or elevators) proportionally, so that the torpedo keeps level running under the water.

Engine room

L = 427 mm (16⅞in)

This section is constructed free to coming in the water to help a cooling system of the engine in the torpedo. It has a starter, a Chowaki or pressure regulator, a wet-heat chamber, a main engine, and a horizontal rudder controller.

The starter starts controllers, one for vertical tail rudders, and another for roll rudders for anti-rolling in both side wing rudders, with horizontal tail rudders being locked at uppermost position, while the torpedo falls down to the water surface. It starts the main engine to propel when the torpedo hits the water. A thick bolt is stuck through the starter during loaded in aircraft as the lock. The bolt is pulled out from the torpedo when it is released. The bolt remains underneath the fuselage of aircraft.

The pressure regulator is called as Chowaki or harmonizing system for the engine, it actually is a two-stage pressure regulator with twin pressure-tunable regulation valves. It steps down the pressure of compressed air at 215 - 50 atm (3,000 - 711 psi) in the air chamber to the constant high-pressure air at 10 atm (142 psi). While the air pressure is declining as the torpedo is running under the water, the pressure regulator feeds the constant high-pressure air to the engine intake aspirator and keeps the constant running speed in 43 knots (or 80 km/h, 50 mile/h).

The wet-heat chamber is made by heat resistant steel. Type 91 aerial torpedoes use wet-heater engine like almost all other torpedoes in World War II. The general wet heater burning method drastically improved the combustion efficiency of torpedo engines. It burns the mixed gas of fuel oil and the high-pressure air with spraying pure water in the wet-heat block to produce burning steam gas fed to the engine. The high-pressure fuel oil gas is burning at a temperature 800 degrees C (1,500 degF). The sprayed pure water mists into the combustion gas, which produces vapor explosion, results in completely gasified fuel oil combustion.

The main engine is an 8-cylinder single-row radial piston engine.

The horizontal tail rudder controller is operated by the rod connection mechanism from the depth meter in the front float section.

Rear float

L = 1,002 mm (39½in)

A single drive shaft is going through the section to the tail. This rear float section has a machine oil tank, a rudder controller, an anti-rolling controller, and roll rudders on both sides.

The machine oil tank is center-mounted in the rear float section.

The rudder controller is a general gyrocompass controlled system, which is steering vertical rudders to keep the longitudinal axis of the torpedo in the sensed direction straight. Both the vertical rudder controller and the anti-rolling controller had their own gyroscope, which is to start rotating when the torpedo is released from aircraft. Each gyro has dual ring support mechanisms to move freely.

Anti-rolling controller

Carrier Zuikaku B5N2s in torpedo attacking at Coral Sea on May 8, 1942. Water splashes in front center and left are made by water entries of Type 91 aerial torpedoes.

File:Guadalcanal-Tulagi Operation, Mitsubishi G4M.jpg

G4M1s in torpedo attacking at Guadalcanal on August 8, 1942.

File:BB-57 Kates Santa Cruz NAN4-2-43.jpg

B5N2s in torpedo attacking at Santa Cruz on October 26, 1942

File:B6N2 in formation.jpg

B6N2s in formation flight with torpedoes wearing box type tail stabilizers

Aichi B7A Ryusei carrying torpedo with cross type tail stabilizer plates, 1945

The stabilizer or anti-rolling controller is a mechanical control system, whose control design needs numerical analysis of physical mathematics theory to fit stability. A spinning gyroscope of control system senses the tilt degree of roll, and then the controller is centering the roll of the torpedo.

The anti-rolling controller with the gyroscope can steer roll-rudders on both sides in angle range of +/- 22.5 ° . When the torpedo tilted, the anti-rolling controller steers roll-rudders (or ailerons) in twisting ailerons manner to produce counter-rolling moment.

When the torpedo tilted over 10 degree and is rolling back the angle toward the neutral center position, the tiny mechanical system in the control air valve works. When it rolls back within the tilt angle 10 degree, the controller now countersteers roll rudders switching back to the reverse angles to break the counter-rolling moment, and to prevent overshoot. The torpedo rolls over the neutral center position and keeps rolling to some degree. The torpedo then stops in opposite tilt at certain degree, and starts rolling back the angle toward the neutral center position. Then the controller senses the angle tilted and countersteers roll-rudders to break the moment. It is rolling over the neutral center position then stops at certain degree, vice versa, like an air cushion is bouncing and settled to the floor. The movement continues but damps to neutral the rolling angle within 2.0 to 3.6 second in the air.

In the test, the system working was observed and proved by the developed high-speed movie film, the top-view shot of the falling torpedo tested, taken from the bomb bay. The anti-rolling system also proved the controller functions effectively under the water surface by the running result after the water entry.

Roll rudders

Stabilizing rudder, or roll rudders (or ailerons) are put on both sides of the torpedo, being steered to produce counter-rolling moment. Each rudder is a small 8 cm² size square metal wing. Each roll rudder has been covered with a temporal wooden extended wing of 12 × 20 cm² (4¾in × 7⅞in), tighten with six aluminum sharing pins on both side-edges (three pins each) to get enough aerodynamic force in the air, that is to be shed and broken off when the torpedo gets the hard impact from the water surface on water entry. The remained original metal roll rudders are steering in the water running to converge the rolling movement arisen on water entry.

Tail section and twin screws

L = 530 mm (to the tip end of propelling screw hub) (20⅞in)

There are bevel gears driving coaxial contra-rotating double 4 blades screws to propel torpedo running straight under the water. Tail section has vertical and horizontal stabilizer fins in cross. Each fin has a controlling rudder in aft. Horizontal fins and rudders or elevators have wide span in longitudinal direction and work proportionally, while vertical fins are small, and rudders have very short span.

Shed off aerodynamic wooden stabilizer plates

File:Type91 AerialTorpedo TailSection and AeroDynamicTailStabilizer.PNG

Type91 aerial torpedo, tail section and aerodynamic tail stabilizer plates

Tail fins are covered with Kyoban or aerodynamic wooden stabilizer plates. They were introduced in 1936. It is shed off by the impact on water entry. This aerodynamic wooden stabilizer plates in the tail are in the shape of box cover for single-engine carrier-based torpedo-bombers Nakajima B5N and Nakajima B6N. In the case for twin-engine land-based torpedo-bombers G3M, G4M, P1Y, and Ki-67, the torpedo wears another type of aerodynamic wooden stabilizer plates covering tail fins in cross to extend their tail length in the air, which is less in drag resistance loss but needs more clearance heights in the bomb bay underneath the fuselage. In the case of land-based torpedo-bomber aircraft, a plate is needed to be set inside the bomb bay to groom the airflow, because the vortex coming in the bomb bay gives the turbulence behavior to the torpedo released.

A torpedo is released at a speed greater than 160 knots (or 300 km/h, 184 mph) in the air and then follows a parabolic path free-falling to the water. The aerodynamically designed wooden plates stabilize the up-and-down motion of the torpedo in the air keeping it aligned to the diving course. The wooden plates are shed as the torpedo hits the water, and the elevators or horizontal rudders set farthest forward lift the nose of the torpedo after water entry to start level running. The structure is simple and works well. The wooden head cap had been used before the anti-rolling controller system was introduced.

Screws

Screws are coaxial contra-rotating double screw, with 4 propeller blades each.

Each screw is wrought from a cube steel alloy mass into bold cross shape and punched through the center. Hammering punches of 1 tons and 3 tons shape 4 blades.

Propel section is compactly designed so that the front screw and the rear screw are put in 5 mm close to each other. A trouble happened in 1943, when a P1Y tested the torpedo released at altitude 100 m in high-speed power gliding. That torpedo veered the running direction. The hard impact on water entry made a front blade get cracked by the hit of a rear blade. The project members shared the recognition on the importance of annealing, quench hardening, and normalizing process of the screw blades, and so was done.

In the first annealing process, the metal is left in the oven at 700 °C (or 1,300 °F) for 2 hours then slowly cooled in lime powder. The metal is hammered out and machined in the shape of screw. Then the screw is put in the quench hardening process, kept at 850 °C (or 1,560 °F) for 1.5 hours, and is cooled in oil. In the last thermal normalizing process, the screw is put in 180 °C (or 356 °F) hot oil for 2 hours, then is left cooling in the air.

Material: SK chromium-molybdenum alloy steel

Process: Hammer out.

Rudder steering means

1. Full steering system

Vertical rudder system steers rudders tri-stated to full-right / neutral / full-left as the gyroscope senses. Type 91 aerial torpedo has long time constant period with respect to the longitudinal axis turn moment in the water.

2. Proportional steering system

Horizontal rudder system elevates the angle of rudders proportional to the angle of displacement the depth meter detect. Type 91 aerial torpedo has medium time constant period in longitudinal axis lift moment under the water.

3. Angular velocity steering system

Anti-rolling controller system steers both roll rudders tri-stated to full-up / neutral / full-down in twisting aileron manner. When the controller detect the rolling is coming back to the center position, the system countersteers roll rudders in opposite direction. This system uses countersteering function so as to dump unstable rolling oscillation movement. Type 91 aerial torpedoes has fast period in approx. 0.5 s time constant in rolling moment.

Structure of Anti-Rolling Controller

Haruo Hirota, Naval Lieutenant Commander

Makoto Kodaira, Naval Lieutenant

File:Type91 AerialTorpedo RollRudder.svg

Type91 aerial torpedo, roll rudder

File:Type91 AerialTorpedo MainRollController.svg

Type91 aerial torpedo, main roll controller

File:Type91 AerialTorpedo RollControllerMovement.GIF

Type91 aerial torpedo, roll controller movement

The structure of the anti-rolling controller is a set of gyro-controlled air valve system to steer the roll rudders on both sides of a torpedo.

The anti-rolling controller is composed with a gyroscope, a main controller, and an output booster. The most significant part is the main controller.

Gyroscope

The gyroscope senses the rolling tilt degree in real-time. It inputs push-pull control operation force to a pilot valve, sliding it inside the main controller to switch two output valves exclusively to the rudders.

Main Controller

The main controller controls two output air valves exclusively to steer roll rudders. It steers and countersteers those roll rudders. It steers the rolling-rudders with detecting the tilted degree of the torpedo rolling by the control of pilot valve. It countersteers those roll rudders when the torpedo is rolling back to neutral position, which results in detecting the acceleration of the rolling angular velocity derivative with respect to time.

Output Booster

The output booster or auxiliary valve has two inlets and two outlets ports. The output booster is working as a pair of air shutoff valves. It is connected in cascade to two output ports of the main anti-rolling controller, switches on and off directly the two powerful high pressure controlling air flows one for clockwise twist and the other for counter clockwise twist of roll rudders, exclusively to each other. It is so as to save the main controller system and to ensure proper operation under the heavy impact condition.

Sequential operation steps in aerial torpedo bombing

1. A release button is switched on in the cockpit.
2. Cartridge is ignited to cut a loading wire band. Torpedo is released and wire is falling freely.
3. The torpedo is falling and the safety bolt is pulled out. It starts gyroscopes of both the vertical rudder controller and the anti-rolling controller.

   Vertical rudders are kept in straight direction.

   Horizontal rudders (or elevators) are locked in uppermost position to prepare the water entry.

   Roll rudders start steering by the anti-rolling controller.

   ---Water Entry---

4. Hard impact to the water surface breaks off wooden air wing covers of side roll rudders and tail aerodynamic stabilizer plates or box.
5. Doubly rotate screws are unlocked at propel block.
6. Propel engine starts cool idling while running. (Engine starts rotating with high-pressure air only.)
7. Brakes on horizontal rudders (or elevators) are released. Depth meter starts working.

   Water pressure after the entry downs a plate to start firing combustion chamber of the engine.

8. Propel wet-heater engine starts hot running by burning fuel air gas, mixed with sprayed water.
9. Safety lock in the warhead is released while running.
10. High explosive explodes on the hit of the target.

---

Theory: Aerial torpedo motion equation

File:Type91 AerialTorpedo Vectors of MotionEqs.svg

Vectors of motion equations for aerial torpedo in the air

Rear Admiral Shoji Naruse explained in his class as follows.

The torpedo motion equation is the set of simultaneous ordinary differential equations, which is to model pitch motion of airborne aerial torpedo as follows.

Eq.1: Falling velocity of the torpedo equation

Eq.2: Horizontal vector velocity of the torpedo mass equation

Eq.3: Vertical vector velocity of the torpedo equation

Eq.4: Vertical vector acceleration of the torpedo mass equation

Eq.5: Angular velocity equation with respect to time

Eq.6: Angular velocity differential equation with respect to time

$\begin{array}{lcll} dx/dt &= &V_{X} &\cdots(Eq.1)\\ W/g \times \left(dV_{X}/dt \right) &= &- D \cos \varphi - L \sin \varphi &\cdots(Eq.2)\\ dz/dt &= &V_{Z} &\ldots (Eq.3)\\ W/g \times \left(dV_{Z}/dt\right) &= &D \sin \varphi - L \cos \varphi + W &\cdots(Eq.4)\\ d\theta/dt &= &\omega &\cdots(Eq.5)\\ I \times \left(d\omega/dt\right) &= &57.3M - bV\omega &\cdots(Eq.6) \end{array}$

where constant 57.3 of Eq.6 is the coefficient from 1 (radian) = 57.2958°

b V ω of Eq.6 is the damping moment, where b is defined as;

$b = - (\delta C_{mgH} / \delta \alpha_{H}) \times ( \rho S \mathit{l}/2) \times \mathit{l}_{H}\,$

Since the angular moment of a torpedo here is the lifting movement as follows;

$\omega\mathit{l}_{H} /V = ( \delta C_{mgH} /\delta\alpha_{H}) \times ( \rho S \mathit{l} /2 ) \times \mathit{l}_{H} \times V \times \omega \,$

V : The velocity of the torpedo

V_H : The horizontal axis velocity of the torpedo

V_Z : The vertical axis velocity of the torpedo

φ : The moving vector angle of the torpedo in reference to horizontal axis

θ : The posture angle of the torpedo in reference to the horizontal axis

α : The internal angle between φ and θ, which is equal to the lift angle of tail fins of the torpedo

W : Weight of the torpedo

g : Acceleration of gravity, 9.8 m/s²

I : Inertia coefficient with respect to lift moment at the gravity center of the torpedo

ω : Lifting angular velocity (radian)

D : Drag moment of force

L : Lift moment of force

M : Roll moment of force around the longitudial axis of the torpedo

ρ : Air density

S : Cross-section area of the torpedo

l : Total length of the torpedo

l_H : The length between the gravity center and the center of lift moment of tail fins of the torpedo

The value l_H is measured in wind-tunnel test, as drag moment of force coefficient differences between the torpedoes with and without box type attachment of wooden tail stabilizer plates;

$\mathit{l}_{H} = (-C_{mgH}\,\mathit{l}+C_{tHd})/C_{nH}\,$

where each coefficient is defined as;

C_nH = C_XH sin α + C_ZH cos α

C_tH = C_XH cos α + C_ZH sin α

C_X : Drag moment of force coefficient D / (1/2 ρ V² S)

C_Z : Lift moment of force coefficient L / (1/2 ρ V² S)

C_mg : Roll moment of force coefficient around the gravity center of the torpedo M / (1/2 ρ V² l)

C_XH : Drag moment of force coefficient of tail stabilizer box of torpedo

C_ZH : Lift moment of force coefficient of tail stabilizer box of torpedo

C_mgH : Roll moment of force coefficient around the gravity center of tail stabilizer box of the torpedo

Solving Eq.1 through Eq.4 with respect to movement under certain boundary conditions, we could derive the set of equations t, X, Z in definite integral equation form.

$X = \int_{\lambda_0}^{\lambda}\,\frac{d \lambda}{gC}\,+\,k\,\varphi(x), \,\, Z = \int_{\lambda_0}^{\lambda}\,\lambda\,\frac{d \lambda}{gC}\,+\,k\,\varphi(x)$

where, λ = - tan φ, λ₀ = - tan φ₀, at time t = 0

Definite integrals can be numerically solved by Composite Simpson's rule in the ordinary differential equations field.

Lifting motion Eq.5 can be numerically solved by The common fourth-order Runge-Kutta method to get values of ω.

Lifting stability of Torpedo Eq.6 can be numerically solved by Exponential moving average method for exponential equations.

Practical equation for lift moment

Lieutenant Commander Hirota proved the practical torpedo motions by his equations.

In the pitching movement, tail stabilizer box has the function not only aligning the longitudinal axis of torpedo in the moving direction or the vector of the center gravity, but also damping the lifting movement or pitching oscillation. The latter effect is the change of lift moment with respect to the angular velocity of the center gravity as follows.

$-(1/2) \times 57.3 C_1 \, \rho \, V^2 \, b \, S_1 \, (b/V) \, (d\theta / dt) \,$

ρ : Air density

V : Speed of the torpedo (constant)

C₁ : Lift moment coefficient by one degree with respect to the airflow vector to the plates of the aerodynamic tail stabilizer

b : The length between gravity center of torpedo and the lift moment center of the plates of the tail stabilizer

S₁ : Area sum of the horizontal plates of the tail stabilizer

θ : Angle of the longitudinal axis of the torpedo to the vector of the center gravity, where the angle is in radian.

The 1st derivative of the lift angle with respect to time, 57.3 (b/V) (dθ/dt) is the key factor to damp the pitch movement. The characteristics to damp the pitching factor improved the airborne stability and the course of the torpedo.

Practical equation for roll moment

First, the roll moment equation is set, then it is simplified in 2nd derivative of θ with respect to t, as follows:

$\begin{array}{lcll} I_2(d^2\theta/dt^2)&= &-K-M(d\theta/dt) &\cdots(Eq.7)\\ (d^2\theta/dt^2)+M/I_2(d\theta/dt)&= &0 &\cdots(Eq.8) \end{array}$

Here we set the initial conditions at t = 0 as dθ/dt = ω₀, θ = 0 to analyze the angular movement on the top neutral point, then we can simplify Eq.7 and Eq.8 as follows:

$\begin{array}{lcll} d\theta / dt&= &-(I_2\,/\,M)\,(K\,/\,I_2)\,+\,(\omega_0\,+\,K\,/\,M)\,e^{-(M/I_2)t} &\cdots(Eq.9)\\ \theta &= &-(K/M)t\,+\,(I_2/M)\,(\omega_0\,+\,K/M)\,(1\,-\,e^{-(M/I_2)t}) &\cdots(Eq.10) \end{array}$

where K and M are defined as follows:

K = - (1/2) C₂ ρ V² S₂ a

M = (1/2) × 57.3 C₁ S₃ (b₂² / 12 )ρ V

and the symbols above are the constants and variables as follows:

ρ : Air density

V : Speed of the torpedo (constant)

C₂ : Lift coefficient of 22.5° with respect to the airflow vector to the side roll rudder plates

a : The length between the aerodynamic centers of the lift moment force in two roll rudders

S₂ : The area of one roll rudder

b₂ : The width of the tail stabilizer

C₁ : Lift coefficient by one degree with respect to the airflow vector to the plates of the aerodynamic tail stabilizer

S₃ : Area sum of the plates of the tail stabilizer, where S₃ / 4 is used in the case of box type aerodynamic tail stabilizer.

I₂ : Inertia coefficient with respect to lifting moment at the gravity center of the torpedo

θ : Roll angle of the torpedo at a right angle with the longitudinal axis

In the practical iterative process in analyses, set certain angle value θ° to Eq.10 and gets value t. Put the value t to Eq.9 then we can get the angular velocity passing through the top neutral point.

Since numerical calculation analyses are plain and difficult to gain public understanding, Hirota made a very simple alternative qualitative explanation of Eq.7 for the countersteering theory to the outsiders of the project, then. It made sense to all by the characteristics of the equation with respect to roll angle, which was obtained through the results of his numerical analyses. Eq.7 represents the change of the rolling angular velocity of the torpedo, that is the 2nd order derivative of angle with respect to time.

The torpedo with anti-rolling controller can converge a big roll angle moment of the torpedo to the small to and fro rolling motion by the factor K and M of Eq.7. Anti-rolling controller can converge a big roll angle moment of the torpedo to the small to and fro rolling motion by changing K factor in the right hand side in Eq.7, which represents the roll moment produced by twisting the side roll rudders, as follows:

When the roll angle is over the range of +/-10 degree, the sign of the first term K factor in Eq.7 works always in positive to steer roll rudders. When the roll angle is coming back within the range of +/-10 degree, the first term K factor in Eq.7 changes the sign of value in negative to countersteer.

While the 2nd term M factor of right hand side in Eq.7, which represents the drag force of wooden tail stabilizer plates, always damps the rolling moment.

That is how Type 91 aerial torpedo can converge the rolling moment oscillation while falling in the air and running under the water.

Miscellaneous stories

Provision of the aerial torpedo technology to Germany

Germany approached Japan to transfer Japanese aerial torpedo technology and Type 91 aerial torpedoes. The Imperial Japanese Navy accepted that approach, and brought not only the technology — the plans arriving in Nazi hands after August 2, 1942, courtesy of Japanese submarine I-30 as part of a yanagi mission, meant to enable transfer of technology and strategic materials between the two leading Axis powers — but also a number of Type 91 aerial torpedoes to Germany in response, designated the Lufttorpedo LT 850 in German service.

Germany needed to know the aerial torpedo technology because the Italian battleship Littorio was heavily damaged in the Battle of Taranto on November 11, 1940, and the German battleship Bismarck was hit by a single torpedo, which jammed its rudder and steering gear for hours on May 26, 1941. Germany also needed aerial torpedoes to attack the Allied transport ships steaming in the Mediterranean Sea. It had previously imported Italian-made aerial torpedoes, which became unavailable following the Italian Armistice of Cassibile with the Allies in September 1943. The indigenous German aerial torpedo designs were badly restricted in launch speed and launch altitude.

Kawatana Naval Arsenal: Firm of Type 91 aerial torpedo

Kawatana Naval Arsenal was the production firm of Type 91 aerial torpedo. Type 91 aerial torpedo was first produced at Nagasaki Weapon Factory of Mitsubishi Heavy Industries in the beginning. Aerial torpedo was researched and developed at Yokosuka Naval Arsenal in Kanagawa Prefecture.

Later, Imperial Japanese Navy established two branch arsenals. One was Suzuka Naval Arsenal in Mie Prefecture. Another was Kawatana Naval Arsenal, the branch of Sasebo Naval Arsenal in Nagasaki Prefecture. Kawatana was specialized to torpedo production.

On August 9, 1945, the Nagasaki Weapon Factory was destroyed by the atomic bomb dropped on Nagasaki.

Postwar

The Imperial Japanese Navy was abolished in 1945. Japan declared a commitment to peace. The torpedo technology was prohibited by the war-renouncing Constitution Article 9. A few scientists got jobs in some universities, most were working in non-public corporations in the chaos of postwar Japan.

About 15 years later, Type 91 aerial torpedo project members knew the industrial machineries imported from United States to Japan powered by proportional-integral-derivative control devices at last. They saw those machineries, which proclaimed "high-sounding" title, with mingled feelings.

Some decades later, they called together at a historic inn named Yōshin-tei, Izu, Kanagawa-prefecture, Japan to establish a small association on January 16, 1978. They decided to raise money to make a tiny book Koku Gyorai Note, or Aerial Torpedo Notebook by private book service. They selected Yuta Tanaka as the 1st chairman. He soon died in 1979, and the major member Toshimori Maeda, died too. Satoshi Suzuki was selected as the 2nd chairman to publish the private book.

Type 91 torpedoes were now displayed at Etajima school of Japan Maritime Self-Defense (The Maritime Self Defense Force 1st Technical School) and Shimofusa Base. They had lost the roll rudders.

Type 91 torpedo retaining original form was once displayed at personal exhibition stand by a small wayside drive-inn cafe, named Yoroi-ya (armor house), in the pile of other dusty military junk parts the owner had, the engine of B6N2 Tenzan, broken radio communication systems, used cups, and rusted mountain artilleries from the Imperial Japanese army and navy, in Hyogo prefecture, Japan, till 2005. The stand was closed in 2005 and the exhibited junk articles were sold to neighboring farmers or military collectors.

An excavated Type 91 aerial torpedo was preserved at Resource Museum in JGSDF Camp Naha, 1st Combined Brigade of The Western Army, JGSDF, located in Naha city, Okinawa, Japan. It is retaining the original form. It was picked up as an unexploded ordnance by a bomb-disposal Squadron of JGSDF.

A captured Type 91 aerial torpedo is displayed at the U. S. Naval Academy, Annapolis, Maryland. It rests on two supports flanking a pathway in a small park in front of the Academy's Dahlgren Hall. Displayed on the other side of the pathway is a Type 93 Japanese Long Lance ship-launched torpedo.

References

Bibliography

• - text in Japanese, privately printed book.
• - photographic print copies of Imperial Japanese Navy Action Reports, text in Japanese.
• - text in Japanese, Prof. Ozawa is the designer of Ki-69.
• - text in Japanese, Seko was one of the last torpedo bombardiers of B6Ns.
• - text in Japanese.
• (August, 1945), Resources from Torpedo bombing section, Kawatana branch, Naval aerial technology arsenal, Imperial Japanese Navy.
• (August, 1945), Resources from the 1st torpedo section, Kawatana naval arsenal production firm, Imperial Japanese Navy.

External links

• A page with many statistics on Japanese WWII torpedoes.
• Partial German translation of this Wikipedia article