Bullpup (AGM-12B) 'Air-to-Surface' missile
Bullpup (AGM-12B)
'Air-to-Surface' Missile
This page was last updated:- 19th July 2006


Bullpup Background

In 1953, the United States Navy initiated a requirement for a short-range 'Air-to-Ground' guided missile. This came out of the poor bombing results achieved while attempting to destroy bridges during the Korean War conflict. The aim was to reduce the exposure of ground-attacking aircraft to enemy fire by utilising a 'Stand-Off' offensive capability and greater accuracy in destroying specific targets, than with conventional 'Free-Fall' bombs.

In 1954, the contract to develop and produce the missile was awarded to Martin Marietta - designation ASM-N-7 Bullpup. This became the United States Navy and Air Forces' first successful Tactical 'Air-to-Ground' Guided missile.

In April 1959, the ASM-N-7 Bullpup production version entered service with the United States Navy. This was a 'Roll-Stabilised' missile with a solid-fuel rocket motor.

Control of the missile was by visual 'Line-of-Sight' by the operator, and a relatively simple 'stick-operated' radio control system. Once the target had been detected, the 'Operator' would launch the missile and track it with the help of two flares mounted either side of the rocket motor at the rear of the missile. This was then manually guided onto the target.


Drawbacks

Because of the crude manual guidance system employed to control the flightpath of the Bullpup, there were severe limitations with this missile system. The major problem was that the aircraft, missile and target had to remain in a straight line for a successful attack. Though Potentially of 'Stand-Off' strike capability, this meant however that the launch aircraft was unable to concentrate on it's own survival from enemy fire while completing it's attack, if the resultant missile delivery was to achieve results.


Royal Navy Service

An improved version of the ASM-N-7 was tested with a new propulsion system, the ASM-N-7a. The solid-fuel propellant was replaced with a liquid-fuelled rocket motor, known as LR58-RM-4, and produced by Thiokol (Reaction Motors). The advantages of this were an increase in operational range and storable propellants. The warhead was a derrivative of a conventional 250lb bomb. This model was designated ASM-N-7a Bullpup-A and entered operational service with the US Navy in 1960.

At this time, the Royal Navy were themselves expressing interest in this 'Stand-off' strike capability for their fleet carrier aircraft. To this end, extensive 'Weapon Trials' were carried out by Blackburns' at Holme-on-Spalding Moor during the early 1960's to evaluate the ASM-N-7a Bullpup-A - A major test aircraft utilised for this was NA.39 XK525. Full acceptance being achieved following trials at RAE West Freugh and the Aircraft & Armament Experimental Establishment (A&AEE) Boscombe Down.

The missile became a major component of the Buccaneer S.Mk.1 weapons' arsenal during the aircraft types 'Operational Service' with the Royal Navy. However, as had been previously show by the US Navy, the Bullpup was neither a reliable or very accurate weapon.


ASM-N-7a Bullpup-A missile 'Carriage Trials' - NA.39 - 'XK525' - Holme-on-Spalding Moor, early 1960's
ASM-N-7a Bullpup-A missile 'Carriage Trials'
NA.39 - 'XK525' - Holme-on-Spalding Moor, early 1960's

In 1963, the old designation system was replaced and the ASM-N-7a Bullpup-A missile variant was re-designated AGM-12B Bullpup-A. Improved versions of this missile were developed over the years, but the inherent problems from the initial design i.e. visual range and manual flightpath targeting, meant that the type was severely limited in operation. The Royal Navy never invested in any of these uprated versions of the Bullpup design.


Conclusion

The AGM-12B Bullpup-A remained in service with the Royal Navy Buccaneer S.Mk.2's into the late 1960's, but for many years the weapon of choice had become the rocket projectile pod. The Fleet Air Arm utilised the 36-tube 2in rocket pod.

The Bullpup filled an important area of the early Buccaneers' offensive armament, but at the end of the day it's limitations outweighed it's effectiveness and hence was rarely considered for operational use.
Technical Specifications
Designation AGM-12B Bullpup-A (ASM-N-7a)
Contractor Martin Marietta (Designer)
Maxson Electronics (Production)
Year (Into Service) 1964 (Royal Navy), 1960 (US Navy)
Type Air-to-Surface Missile
Wingspan 3ft 1in
Length 10ft 6in
Core Diameter 1ft
Launch Weight 569lb
Speed (Max) Mach 1.8 (1,187kts, 1,365mph)
Range (Effective) 41/2 miles
Range (Max) 7 miles
Propulsion Thiokol (Reaction Motors) LR58-RM-4
Liquid-fuelled rocket motor (12,000lb thrust)
Guidance Visual Guidance by Radio Command
Warhead 250lb High-Explosive Bomb warhead


Source - Buccaneer: The story of the last all-British strike aircraft (Tim Laming)
The Buccaneers (Air Commodore Graham Pitchfork)
Wings of Fame - volume 14 (Aerospace Publishing Ltd)
Hawker Siddeley/Blackburn Buccaneer (Paul Jackson & Peter Foster)
(see Reference Library page for full details)
Additional Info. - Federation of American Scientists
Directory of U.S. Military Rockets and Missiles

All profile artwork is the copyright property of the author Andy White
"All Rights Reserved"
- Copyright (c) Andy White 2004 - 2006