View source for Mizuno Shinryu

{{Short description|Japanese rocket interceptor project}}
{{Multiple issues|
{{More citations needed|date=February 2023}}
{{More footnotes|date=February 2023}}
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{{Infobox aircraft
 |name= Shinryū
 |image= File:Mizuno_Shinryu_Model_(2_viewed_angles)_artists_impression.jpg
 |caption= A diagram showing the Shinryū from several angles.
 |type= [[Interceptor aircraft|Interceptor]]
 |national_origin= [[Empire of Japan]]
 |manufacturer= [[Mizuno Corporation|Mizuno]]
 |designer= Yoshio Akita 
 |first_flight= mid-July 1945 (Jinryū)
 |introduction= 
 |retired= 
 |status= Cancelled
 |primary_user= [[Imperial Japanese Navy Air Service|IJN Navy Air Service]] (Intended)
 |more_users=
 |produced=
 |number_built= 5 "Jinryū"{{efn|name=ShinJin}} Glider Prototypes<br/>0 "Shinryū"{{efn|name=ShinJin}} (Design Only)
 |unit cost=
 |developed_from=
 |variants=
}}

The {{nihongo|'''Mizuno ''Shinryū/Jinryū'''''{{efn|name=ShinJin|For the purposes of this text, Shinryū II is used to help differentiate the interceptor from the glider. The [[kanji]] and is the same for both spellings but is pronounced differently. Both translations of Jinryū and Shinryū mean 'Divine Dragon'. Shinryū II is also used in contemporary texts and as such, is used here for recognition purposes. Whether the interceptor would have carried the same name as the glider is unknown.<ref name="MizunoSh">{{cite book|last=Dyer|first=Edwin M. III|title=Japanese Secret Projects: Experimental aircraft of the IJA and IJN 1939-1945|publisher=Ian Allan Publishing|location=Hersham|year=2009|edition=1st|pages=104–106|isbn=978-1857803-174}}</ref>
}}|{{linktext|神龍}}||"Divine Dragon"}} was a late-[[World War II]] Japanese rocket-powered [[Interceptor aircraft|interceptor]]. While the Jinryū was still in development, [[Mizuno Corporation|Mizuno]] began to develop an interceptor which both the [[Imperial Japanese Army Air Service|Army]] and [[Imperial Japanese Navy Air Service|Navy]] air force were in desperate need of to fend off the [[Boeing B-29 Superfortress]]. When [[Japanese Instrument of Surrender|Japan surrendered]] to the Allies on 15 August 1945, all aircraft that were under development were stopped, including the Jinryū & Shinryū II. The Shinryū II was the second aircraft developed in Japan to use a [[Canard (aeronautics)|canard]] design, after the [[Kyushu J7W Shinden]].

==Development==
In June 1944, the first [[Boeing B-29 Superfortress]]es appeared over Japan. It was the start of bombing campaign that would see key Japanese cities, infrastructure and industries reduced to ashes through conventional and firebombing raids. With the aircraft industry being a priority target, the {{nihongo|[[Imperial Japanese Navy Aviation Bureau]]|海軍航空本部|Kaigun Koku Hombu}} looked to ways to combat the B-29 menace. One concept was a point defence interceptor that could quickly rise to meet the bombers and so the Mizuno ''Shinryū'' was born. However, the development of the ''Shinryū'' began with designs for a far more conventional craft.

In November 1944, the Navy Aviation Bureau looked into the possibilities of an aircraft to undertake {{Nihongo|suicide missions|神風|[[kamikaze|shinpu]]}}. While the mission was not unique, the fact that the aircraft being investigated would be a glider was. The Bureau envisioned that gliders would be launched with rocket boosters from caves or shore positions and pilots would guide the aircraft and the {{convert|100|kg|lb|abbr=on}} explosive payload inside it into Allied ships or tanks should the Japanese home islands be invaded. The Bureau  assigned the {{nihongo|[[Yokosuka Naval Air Technical Arsenal]]|海軍航空技術廠|Kaigun Kōkū Gijutsu-shō}} at [[Yokosuka]] the task of turning the glider into reality. The project was led by Shigeki Sakakibara who staffed a number of teams that would each be responsible for one part of the glider. The different sections were the wings, the fuselage, control surfaces, aerodynamic testing and test flights once the prototype was complete. The Navy Aviation Bureau gave instructions that the glider must be built from as much wood as possible.

This restriction was imposed for two reasons. The first was that in using wood and keeping the use of metal to an absolute minimum, the glider could be manufactured in any small shop using only wood working tools, and secondly, as a consequence, what metals were available would be conserved for other military uses. Much of the glider's design was conceived by Yoshio Akita. A number of concepts were discussed and sketched and after much deliberation among Akita and his teams the design was complete by May 1945, and the [[Mizuno Corporation]], a small glider manufacturer better known for sports equipment, had almost finished the prototype.

[[File:Mizuno Jinryu first glider varient of the Shinryu.jpg|thumb|right|The Jinryu being inspected by [[Imperial Japan|Japanese]] personnel.]]

The glider was very simple and used a high-wing monoplane form. The straight and flat wings were wide but had a short span and were designed to ensure that the glider was easy to handle given that inexperienced pilots would be at the controls. Also, the platform would be able to accommodate the rocket engines that were to be used to boost the glider into the air. The pilot sat in an open cockpit. The design was sent to the Navy Aviation Bureau for review. Sakakibara studied the plans and projections and after his analysis it was felt the glider was flawed and changes were necessary.

After these had been made the design was approved. Work began on the revised ''Jinryū'',{{efn|name=ShinJin}} as the glider was now called, by the middle of June 1945. To hasten the construction, the finalised blueprints and work plans for the ''Jinryū'' were drawn up even as the components for the first prototype were being built. Construction of the ''Jinryū'' was again given to Mizuno. Working around the clock, the company completed two prototypes with such speed that wind tunnel testing of the design was still underway. In fact, the first flight of the ''Jinryū'' occurred even before the results of the testing had been provided to Tonsho and Sakakibara. Tashiichi Narabayashi was the pilot who flew the maiden flight in mid-July 1945 at the airfield in [[Ishioka, Ibaraki|Ishioka]], a city located in [[Ibaraki Prefecture]], about {{convert|90|km|mi|abbr=on}} northeast of Tokyo. The Jinryū was towed into the air by a [[Tachikawa Ki-9]], piloted by Saburo Fujikura, a man known for his skill in flying gliders prior to the beginning of the war.

For the first test, Narabayashi assessed the ''Jinryū's'' handling. On landing, his opinion was that the glider was stable and possessed good handling characteristics. For the second flight Narabayashi would investigate the ''Jinryū's'' diving capability and after a few bounces on the ground the Ki-9 and the Jinryū took off. At a height of {{convert|2300|m|ft|abbr=on}}, Narabayashi went to cast off from the Ki-9 but found that the tow rope release had stuck; however, he was able to cut the rope and proceed with the test flight. When Narabayashi put the ''Jinryū'' into a dive and had reached {{convert|300|km/h|mph|abbr=on}}, the glider began to vibrate to such a degree that he was unable to read the gauges. Pulling the nose up to bleed off speed, Narabayashi discovered that the vibrations ceased. During his descent Narabayashi examined the vibrations and after landing the issue was reviewed. The conclusion was that the tail was not sufficiently reinforced and the vertical stabiliser was too small.

The ''Jinryū'' was modified by adding some strengthening in the tail and fitting a second stabiliser. The changes were later validated both in the air and in the wind tunnel testing of the modified ''Jinryū'' model. Before flying the ''Jinryū'', Narabayashi had suspected that the aircraft would have stability problems, which proved to be the case. With the handling and flight characteristics of the ''Jinryū'' proven, the testing moved to the next phase - that of-powered flight. The glider was relocated to an airfield in [[Kasumigaura, Ibaraki|Kasumigaura]], about {{convert|19|km|mi|abbr=on}} north of Ishioka. Here, the ''Jinryū'' was modified to accept a group of three Toku-Ro I Type I rocket engines that together would produce {{convert|300|kg|lb|abbr=on}} of thrust during a 10-second burn.

Testing of the rocket array showed two serious flaws. The first was the quality of the rockets that resulted in a number of failures. The second was the inconsistency of the burn times. Narabayashi noted his concerns and forwarded them to Major Suganuma who had been placed in charge of the ''Jinryū'' project. In addition to expressing his doubts about the rocket engines, he also stated that the ''Jinryū'' would be unsuited for ''shinpu'' missions because, despite the changes made to the glider to improve the flight characteristics, it was a challenging aircraft to fly. Narabayashi suggested that instead of being used for ''shinpu'' operations, the glider should be modified to take six rocket engines each with a 30-second burn time. He estimated that at maximum burn the ''Jinryū'' could attain a speed of {{convert|750|km/h|mph|abbr=on}}, and for weapons he envisioned that it could carry ten explosive charges adapted from artillery shells used by the [[Imperial Japanese Army|IJA]] in their {{convert|100|mm|in|abbr=on}} guns (likely the [[Type 92 10 cm cannon|Type 92]]). Not only did Narabayashi agree that the ''Jinryū'' could be used against tanks and ships but added that it could also be used to attack US B-29 bombers.

Despite the issues with the rockets work continued on preparing the ''Jinryū'' for powered flight. Major Suganuma, however, would become the catalyst for the ''Shinryū II'''s{{efn|name=ShinJin}} continued development. Taking Narabayashi's concerns on board, Suganuma formed a team to revise the ''Jinryū'' and produce a design for an interceptor rather than a glider; Suganuma was especially interested in this idea since he had access to rocket engines that promised 32-second burn times. Two people were retained from the ''Jinryū'' project: Sakakibara, the lead designer, and Yoshio Tonsho who would oversee the construction of the prototype. Yujiro Murakami was tasked with the aerodynamic testing of the ''Shinryū II''. All of those assigned to develop the ''Shinryū II'' were ordered by Suganuma to maintain the utmost secrecy. Unlike the ''Jinryū'', the ''Shinryū II'' was to be built from the outset as an interceptor. Sakakibara would use a canard design that made this the second Japanese aircraft to be developed during the war with such a feature (the first was the [[Kyushu J7W Shinden]]). In addition, the main wings had a platform similar to a cropped delta. These design features were included as a means of ensuring stability in flight as well as good handling characteristics. Since the average Japanese pilot had little experience with canard equipped aircraft, the ''Shinryū II'' had spoilers fitted into the top of each main wing. Each spoiler was able to rotate between 60 degrees and 90 degrees and if the mechanism for controlling the spoilers was damaged, they would automatically return to the closed position. The pilot was provided with an enclosed cockpit. For power, the ''Shinryū II'' was to use four Toku-Ro I Type 2 rocket engines located in the rear of the fuselage. Each engine provided a 30-second burn time and all together up to {{convert|600|kg|lb|abbr=on}} of thrust could be delivered. Two rockets would be used to get the ''Shinryū II'' airborne while the other two engines would be used when making the attack. There was a concern regarding the operating temperatures of the Toku Ro rockets and two methods of cooling the engines were considered. The first would have utilised an air-cooled combustion chamber that would have required an air inlet using a bayonet mechanism in order to maintain air flow across the chamber. It also would have required specific positioning of the fuel injectors so as not to have the air flow disrupt the injection process. The second method would use injectors which sprayed a water and alcohol mixture onto the rocket nozzle, cooling it.

In reviewing the two solutions for cooling, it was determined that the water/alcohol system would be the simplest to implement. No provision was made for a wheeled landing gear system and skids were used. A nose skid was provided with a basic spring suspension to absorb the landing forces. Under each wing was a non-sprung skid arrangement supported by two struts. For take-off the ''Shinryū II'' was to use a two wheeled dolly similar to the one used by the [[Mitsubishi J8M|Mitsubishi J8M ''Shūsui'']] . Once airborne the pilot could jettison the dolly. In addition to conventional runway take-off procedures, other methods for launching the ''Shinryū II'' were considered but what exactly these were is not known. It can be speculated that towing the ''Shinryū II'' aloft was one consideration. Another may have been air dropping the ''Shinryū II'' in the same manner as the [[Yokosuka MXY-7 Ohka|Kūgishō MXY7 ''Ōka'']]. In both cases this may have preserved two of the rocket engines which would have been used up had the ''Shinryū II'' taken off from the ground. In order to combat the B-29, which could operate at altitudes up to {{convert|10000|m|ft|abbr=on}}, the ''Shinryū II'' was to be equipped with a pressurised cockpit or, if such a cockpit proved problematic, the pilot would wear a pressure suit.

For weapons, the ''Shinryū II'' was to be armed with eight rockets. Attached to the inside of the rear landing skid arrangement were four tubes, one on top of the other and angled downwards, which contained the rockets. There has been some conjecture as to the mission objective of the ''Shinryū II''. Some sources make the case that the ''Shinryū II'' was to be used like the MXY7 while others come to the conclusion that the ''Shinryū II'' was to attack armoured ground targets such as tanks. In both cases these sources state that the nose of the ''Shinryū II'' contained an impact fused explosive warhead and once the rocket armament was expended, the pilot would crash the aircraft into his final target using the warhead to deliver the ''[[coup de grâce]]''. However, analysis of the ''Shinryū II'' shows that neither mission was likely. The aircraft would have been far more complex to build than the [[Nakajima Ki-115|''Toka'']] or ''Ōka'' and the ''Shinryū II'' was constructed for maneuverability, high altitude operation and the means to land. In addition, using the ''Shinryū II'' for ''shinpu'' missions against tanks makes little sense when there were other simpler and more effective means (both already in service and under development) to eliminate armour.

[[File:Mizuno jinryu during take of, rockets are believed to have been activated.jpg|thumb|right|Mizuno Jinryū during landing]]

Perhaps this is a case of the Jinryū glider's role being applied to the ''Shinryū II'', or an assumption based on the fact that, like the IJN's other special attack aircraft such as the [[Nakajima Kikka|''Kikka'']], [[Kawanishi Baika|''Baika'']] and [[Nakajima Ki-115|''Toka'']], the ''Shinryū II'' possessed no letter/numerical designation. So, by extension, the ''Shinryū II'' must also have been a special attack weapon. This, of course, is not to say that the pilot could not choose to use the ''Shinryū II'' as a ''shinpu'' aircraft. As an interceptor, the ''Shinryū II'' had a similar role to the [[Mitsubishi J8M|Mitsubishi J8M ''Shūsui'']] and the German [[Bachem Ba 349|Bachem Ba 349 ''Natter'']], which the Japanese were aware of and obtained data on (although the plans never made it to Japan). Like the J8M and Ba349, and due to the limited range afforded by the rocket engines, the ''Shinryū II'' would have to be positioned close to targets that were likely to be bombed. And like the J8M, the ''Shinryū II'' would have used a jettisonable wheeled dolly to take-off while firing a pair of its rocket engines. Unlike the J8M which burned up all of its fuel at once, the ''Shinryū II'' had a second set of rocket engines which could be used to sustain flight endurance or to increase speed during the attack. In the same way as the Ba349, the ''Shinryū II'' would be armed with rocket projectiles, likely fired as a group to affect a spread pattern, to bring down the bomber target. Finally, akin to the J8M, once the fuel and ammunition were expended, the ''Shinryū II'' would glide back to its base to be recovered, refueled and rearmed.

The ''Shinryū II'' would never be built because the end of the hostilities in August 1945 terminated any further work on the design. Likewise, the ''Jinryū'' glider would never fly under power. After the failure of the rocket motors during ground tests, the war came to a close before more suitable and reliable motors could be acquired and tested. Mizuno completed a total of five ''Jinryū'' gliders.

==Variants==
;Mizuno Jinryū "Divine Dragon"{{efn|name=ShinJin}} 
:Special attack aircraft. Mizuno's only (known) plane to be ordered into production. 5 glider prototypes produced.
;Mizuno Shinryū II "Divine Dragon"{{efn|name=ShinJin}} 
:Rocket Interceptor with 4 rocket pods stacked on each other under each wing. Designed to intercept the [[B-29 Superfortress]] in a similar fashion to the [[Bachem Ba 349]]. None built.

==Operators==
;{{JPN}}
* [[Imperial Japanese Navy Air Service]]

==Specifications==
<!-- Deleted image removed: [[File:Mizuno Shinryu from WWII-Designed late with rocket propulsion but never exceeded beyond the initial stage of development.jpg|thumb|300px|Artist's Impression of the Shinryu in army colours]] -->
{{Aircraft specs
|ref=Japanese Secret Projects: Experimental aircraft of the IJA and IJN 1939-1945<ref name="MizunoSh"/>
|prime units?=met
<!--
        General characteristics
-->
|crew=1
|length m=7.6
|length note=
|span m=7
|span note=
|height m=1.8
|height note=
|wing area sqm=11
|wing area note=
|aspect ratio=<!-- sailplanes -->
|airfoil=<!--'''root:''' [[NACA airfoil|NACA ]]; '''tip:''' [[NACA airfoil|NACA ]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}</ref>-->
|empty weight kg=
|empty weight note=
|gross weight kg=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight note=
|fuel capacity=
|more general=
<!--
        Powerplant
-->
|eng1 number=4
|eng1 name=[[Toku-Ro I Type II]]
|eng1 type=solid-fuel rockets
|eng1 kn=1.5
|eng1 note=
<!--
        Performance
-->
|max speed kmh=300
|max speed note=
|cruise speed kmh=110
|cruise speed note=
|stall speed kmh=
|stall speed note=
|never exceed speed kmh=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed note=
|range km=4
|range note=
|combat range km=
|combat range note=
|ferry range km=
|ferry range note=
|endurance=<!-- if range unknown -->
|ceiling m=400
|ceiling note=
|g limits=<!-- aerobatic -->
|roll rate=<!-- aerobatic -->
|climb rate ms=
|climb rate note=
|time to altitude=
|wing loading kg/m2=
|wing loading note=
|fuel consumption kg/km=
|power/mass=
|thrust/weight=
|more performance=
<!--
        Armament
-->
<!--|armament=-->
|rockets=8 x unguided rockets
|bombs=1 × {{convert|100|kg|lb|abbr=on}} explosive warhead or 10 × explosive charges adapted from {{convert|100|mm|in|abbr=on}} artillery gun shells (likely the Type 92)
|guns=4 × {{convert|30|mm|in|sigfig=3|abbr=on}} [[Type 5 cannon]]s (Although suggested, there is no evidence that supports this).

|avionics=
}}

==See also==
{{aircontent|
|related=
* [[Kawanishi Baika]]
* [[Mitsubishi J8M]]
* [[Rikugun Ki-202]]
* [[Yokosuka MXY-7 Ohka]]
|similar aircraft=
* [[Bachem Ba 349 Natter]]
* [[Messerschmitt Me 163]]
* [[Mitsubishi J8M Shusui]]
|lists=
* [[List of fighter aircraft]]
* [[List of military aircraft of Japan]]
* [[List of rocket aircraft]]
|see also=
* Kawanishi K-200
* [[Kyushu J7W Shinden]]
* [[Nakajima Kikka]]
* [[Nakajima Ki-201]]
}}

==References==
{{Reflist}}
{{notelist}}

==External links==
* [http://www.j-aircraft.org/xplanes/hikoki_files/shinryu.htm Hikoki 1946 page on Shinryu]

{{Imperial Japanese Navy official aircraft names}}
{{DEFAULTSORT:Shinryu, Mizuno}}
[[Category:Aircraft manufactured in Japan]]
[[Category:1940s Japanese attack aircraft]]
[[Category:1940s Japanese fighter aircraft]]
[[Category:World War II suicide weapons of Japan]]
[[Category:Aircraft first flown in 1945]]
[[Category:Canard aircraft]]
[[Category:Rocket-powered aircraft]]