ROCKET, HIGH-EXPLOSIVE, 3.5-INCH AT, M28A2
No Image Available Filler and Weight
Composition B, 0
Body and Overall Weight
Steel, 9.00 lb
Color
Olive drab w/yellow markings
Type of Round, DODIC
Service, 1340-H600
Description:
The warhead is cylindrical and tapered. The forward end, called the ogive, is thin metal and hollow. The rear end, threaded internally to receive the fuze which is encircled by a safefy band. The warhead contains a copper cone whose apex faces aft and acts to shape the high explosive charge Composition B -(Comp B). The base detonating (BD) rocket fuze M404A2 consists of a body which contains the functioning parts; a safety band, a detonator and a booster pellet. The fuze body and safety band are olive drab. The fuze mechanism consists of an activating plunger, a setback spring, a setback sleeve, a firing pin assembly, a detent spring, an ejection pin and an ejection spring. The spring-loaded ejection pin passes through the fuze body. c . The motor assembly consists of a tube which houses the propellant and igniter. The fin assembly is securely attached to this tube. The front end of the tube is assembled to the base of the fuze. The rear end forms a nozzle. The cylindrical motor cavity is divided into four sections by two spacer plates which support the grains of propellant powder. d. Each grain of propellant is 5-in. long and approximately 3/8-in. in diameter. Three grains are placed in each of the four sections formed by the spacer plates. Each lot of propellant is adjusted at the time of manufacture to give standard velocity. The igniter ignites the propellant. e. The igniter consists of a short, cylindrical plastic case containing a small black powder charge and an electrical squib. It is assembled in the forward end of the motor on top of the propellant, spacer plates. The leads of the electrical squib, running parallel to the grains of propellant, pass from the igniter through the nozzle into the expansion cone. A green lead (ground) wire is connected to the aluminum support ring of the contact ring assembly. A red lead (positive) wire is attached to a pin which is insulated from the support ring, but is in contact with the copper contact band. These connections are positioned 180° apart. Blue lead is used for test purpose only. f . The fin assembly consists of six aluminum alloy fins and a contact ring assembly. The contact ring assembly, which encircles the fins, consists of three rings. The aluminum support ring, which is innermost, is separated from the copper contact ring by a plastic insulating ring, The fins are spot welded to the expansion cone, and the expansion cone is press fitted to the rear of the motor tube. The M24 and the M66 offroute mines utilizing M28A2 HEAT rockets are described in TM 43-0001-36. The BD rocket fuze M404A1 is similar to BD rocket fuze M404A2. The M404A1 differs principally in minor design changes of the functioning parts and the shape of the safety band.
Use:
The M28A2 HEAT rocket is used primarily against armored targets, tanks and secondary targets, such as gun emplacements, pillboxes and personnel. It is capable of penetrating heavy armor at angles of impact greater than 30°. In an antipersonnel role, it has a fragmentation area 10 yd wide and 20 yd deep.
Functioning:
a . When the safety band is removed, the ejection pin moves outward approximately 3/8 of an inch but still prevents all parts of the fuze mechanism from moving. When the rocket is in the firing chamber, the ejection pin is partially depressed by the chamber, thereby freeing the setback sleeve so it can move to the rear when the rocket is fired. The fuze is still safe, since the ejection pin prevents movement of the actuating sleeve and firing pin. b. If it becomes necessary to remove the rocket from the launcher, the ejection pin will move outward and re-engage the setback sleeve. This returns the fuze to its original safe condition. c_. When the rocket is fired, the force of inertia causes the setback sleeve to move rearward. It is held in its rearward position by the lockpin. When the rocket leaves the muzzle of the launcher, the ejection pin is thrown clear of the fuze by the ejection pin spring. The fuze is then fully armed. d. During flight, tie firing pin lever and firing pin spring prevent the firing pin from striking the detonator, The creep spring retards the forward movement of the plunger and actuating sleeve. The action of the creep spring prevents the fuzefrom firing should the rocket strike light objects such as thin brush or undergrowth. e. Upon impact with a more resistant object, the plunger and actuating sleeve move forward until the sleeve hits the firing pin lever. This causes the firing pin to strike and detonate the warhead.
Munition Components:
  • Fuze: Model M404A1 or M404A2;Type Base detonating;Diameter 2.0 in.
  • Propelling charge: Model M7;Type Solvent
  • Fuze: Model M404A1 or M404A2;Type Base detonating;Diameter 2.0 in.
  • Propelling charge: Model M7;Type Solvent
  • Fuze: Model M404A1 or M404A2;Type Base detonating;Diameter 2.0 in.
  • Propelling charge: Model M7;Type Solvent
Data Source:
TM 43-0001-30 Dec 1981
Munitions Tech Data Sheet:
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