Description
Gray overall with green and brown nose bands and red tail struts.
In its early stages of development, this rocket was designated Mk 19. It is constructed of a light aluminum alloy and carries a high explosive charge. It is intended for use against large aircraft.
Rocket power is supplied by 16 grains of ballistic type propellant 19.2 mm x 350 mm. They are contained in the cylindrical barrel of the bomb, and are ignited electrically.
The nose section is ogival in shape, and carries the high explosive charge. A nose well is provided to take a special small impact fuze similar to A-3(a).
The tail section is constricted to form a venturi, and is fitted with fins, riveted in place, for stabilization. An error of 10 meters at a range of 500 meters is assumed by designers.
Two launching rails, 180° opposed, are attached to the barrel of the bomb.
The data on this bomb is the result of incomplete investigation, and must not be considered as specific, accurate information.
Hazardous Components
Filler - Unknown high explosive (1.32 lb, 0.6 kg)
Propellant - Unknown (4.4 lb, 2 kg)
See Also
General Information, Japanese Navy Bombs
Nose, A-3(a), Type 97 Mk 2 Model 2
Source(s)
