Part 1 - Aircraft Bombs and Pyrotechnics; Chapter 4: M.C. 250-lb. Mks I and II (Service)Part 1 - Aircraft Bombs and Pyrotechnics; Chapter 4: M.C. 1,000-lb. Mks I and II (Service)
BRITISH EXPLOSIVE ORDNANCE
Part 1 - Chapter 4
Medium Capacity Bombs

M.C. 500-lb. Mks I - V (Obsolescent), and Mks VI - XII (Service)

Data

Fuzing

Nose Pistol No. 27, 42, or 44; Tail Pistol No. 28, 30, or 37

Color markings

Dark green over-all; ½-in. red band 2 in. from nose; 1-in. light green band around base of ogive

Tail No.

No. 2 Mk I; No. 25 Mks I or II; No. 26 Mk I; or No. 28 Mk I

Over-all length

70.6 in. (with long tail); 57.8 in. (with short tail)

Body length

41 in.

Body diameter

12.9 in.

Wall thickness

0.3 in. Mks I, II, VI, VII; 0.42 in. Mks III, IV, V, VIII - XII

Tail length

No. 25 Mks I, II, 28 in.; No. 28 Mks I, II, 14 in.

Tail width

12.9 in.

Total weight

Mk VIII with short tail, 499 lb. Amatol filled

Charge/weight ratio

50%

Body Construction: The bomb has parallel sides, with an ogival nose and a slight rear taper, similar in construction to U.S. General Purpose bombs.

With the exceptions as given below, exploder containers screw into the nose and base plate. Mk I: fabricated; rolled steel sheet, welded, with nose and tail welded on. Mk II: drawn tube; nose formed by "bottling" process; tail welded on. Mk III: cast. Mk IV: cast to 500-lb. G.P. dimensions. Mk V: same as Mk III, but center of gravity was off, so all were declared obsolescent immediately; used only with the long tail unit. Mks VI, VII, VIII and IX are same as Mks I, II, III, IV, respectively, with American dual suspension lugs added. Mk X: forged body; solid nose; fuzed only in tail. Mk XI: Mk VII with a solid nose. Mk XII: Mk VII with improved welds at the after end, and fuzed both nose and tail.

Tail Construction: The Tails No. 25 and No. 28 are similar in construction, each con-sisting of a cylindrical strut attached to a tail cone by four fins. The tail assembly is se-cured to the body by four spring clips which engage slots in the tail end of the body. Turnbuckle fittings are provided for two of the springs as a locking device. A reach rod running through the tail cone, engages the arming fork of the pistol, and carries the arm-ing vanes at its fits after end. The arming vanes protrude beyond the cylindrical strut and the fins on the short-type Tail Unit No. 28.

Suspension: Mks I – V of this bomb have a single suspension lug welded to the body, while Mks VI – XII have dual lugs for suspension from U.S. aircraft welded on in addition to a single lug.

Explosive Components

Detonator – (See Part 2, chap. 4, Detonators.)

Exploders – C.E. pellets

Filling – (Mk VIII), 210 lb. Amatol 50/50 or 60/40; 226 lb. Amatex 51/40/9; 222 lb. RDX/TNT 60/40; or 232 lb. Torpex 2.

Remarks: These bombs are supplied with a Tail Pistol No. 28 or No. 30, and may or may not be fuzed at the nose.

The short-type tail unit, such as the No. 28, Mk I, is used when the bombs are drop-ped from fighter-bomber aircraft.

The Anti-Disturbance Fuze No. 845, formerly incorporated in the nose of bombs fuzed with the Tail Pistol No. 37, is now obsolete.

Tail fins are usually painted red when time pistol is used.

Figure 16 – M.C. 500-lb. Bomb

Part 1 - Aircraft Bombs and Pyrotechnics; Chapter 4: M.C. 250-lb. Mks I and II (Service)Part 1 - Aircraft Bombs and Pyrotechnics; Chapter 4: M.C. 1,000-lb. Mks I and II (Service)