The Mizuno Shinryu was a late-World War II Japanese
rocket-powered suicide interceptor concept. The project never
proceeded beyond the initial phase of development.
In configuration, it was to be a canard-winged design, with
swept wings and tail fin. Two rocket engines were to be mounted in
the rear, and the nose was to be fitted with an explosive warhead.
Some versions of the design appear to have been intended to carry
unguided rockets under the wings for interception of enemy bombers,
similar to the intended role of the German Bachem Ba 349.
It is unclear today whether the engines were intended to provide
power for take-off (like the Bachem Ba 349), or to accelerate the
aircraft towards its target (like the Ohka). Similar to the Ohka,
it could have been launched from coastal air bases and caves, and
modified Mitsubishi G4M "Betty" or Yokosuka P1Y bombers. Its
intended role, whether anti-ship, anti-aircraft, or anti-tank is
still unclear.
Variants
Mizuno "Shinryƫ" Type 1 suicide rocket
glider
Mizuno "Shinryƫ" Type 2 rocket
interceptor
Specifications (Shinryu, as designed)
General characteristics
Crew: one, pilot
Powerplant: 2 × Tokuro-1, solid-fuel rockets,
1.5 kN (330 lbf) each
Armament
Warhead in nose and/or 8 × unguided
rockets
The Mizuno Shinryu
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