Raptor performs first drop of small
diameter bomb. An F-22 Raptor
drops a small diameter bomb from its weapons bay during a test mission
Sept. 5 [2007]. The test marks the first airborne separation of a small
diameter bomb from the internal weapons bay of an F-22.
Testing of the SDB with the F-22 is part of the Increment 3.1 upgrade
to the aircraft. Major Jack Fischer, 411th Flight Test Squadron test
pilot noted that
"Targets we can't get with most weapons, we can get with the F-22
because we have stealth, with this weapon and aircraft,
there is no place we can't reach and no place for an enemy to hide." (Photo by Darin
Russell, Text by
95th Air Base Wing Public Affairs, US Air Force)
Background
The SDB was conceived during the 1990s to provide
an internally carried weapon which would allow the F-22A Raptor,
and later JSF, to attack multiple targets. The design is sized so that
the F-22 can carry eight rounds in its main weapon bays.
The SDB was operationally deployed last year, and first
dropped in combat during a close air support sortie in Iraq, on October
5th, 2006.
Development of the SDB followed the Miniature
Munitions
Demonstration Technology (MMTD) program during the 1990s.
The US Air Force intends to procure 24,000 or more
rounds for carriage on new and legacy combat aircraft; of these half
will be baseline weapons equipped for attacking fixed targets, and the
remainder a variant equipped to attack moving targets.
Design aims for the SDB included a capability to
penetrate hardened targets and provide better accuracy than the JDAM.
The MMTD effort included a focus on key technologies
including the Hard Target Smart Fuze, High Energy Explosives,
Penetrator Design, Optimal Guidance, Robust Autopilot, Differential
GPS/INS, and an Advanced Seeker. The Optimal Guidance is a unique
feature, it is designed to align the bomb body exactly with the
weapon's velocity vector at the point of impact, as this
maximises penetration of the target - all of the bomb's kinetic
energy is used to drive the weapon in - older guidance systems did not
achieve this and velocity components tangential to the impact would at
best waste energy, at worst contribute to premature casing rupture.
The production SDB is equipped with Rockwell
Collins GPS receiver, with a Harris anti-jam module, and a
Honeywell inertial unit, a KDI Precision Products reprogrammable
electronic fuse (airburst, contact and delay modes), HR Textron tailfin
actuators, MBDA diamondback foldout wings, with a TAM Garland 50 lb
forged casing warhead. A Mil-Std-1760 interface is used. The launcher
is a Sargent Fletcher pneumatic ejector system in the Boeing BRU-61/A
bomb rack.
SRI are providing differential GPS
ground stations, required to enhance SDB accuracy over JDAM and other
conventional munitions.
The glide wings provide a quoted
delivery range of around 60 nautical miles for a high altitude release.
The weapon performs a 180 degree roll post launch as the stowed
configuration has the folded wings beneath the weapon.
The cited blast radius is 26 ft
(cf 82 ft with 2,000-lb JDAM). Boeing claim the ability to penetrate
more than 5 ft of steel reinforced concrete making the SDB competitive
against the BLU-109/B for many targets.
The SDB will be most effective in
the urban and broader close air support, battlefield interdiction,
Destruction of Enemy Air Defences (DEAD) lethal suppression and
counter-air strike airfield attack roles. Against soft skinned vehicles
and structures, armour, point emplacements, runways, aircraft shelters
and SAM/SPAAG systems this weapon will be highly lethal.
Where the SDB will be less than
effective is against deep / hardened bunkers, large infrastructure
targets, large buildings, industrial plant, bridges, large trench
systems, vehicle parks, infantry on the move and other area or large
point targets. These remain the domain of larger specialised bunker
busting weapons, or large explosive bombs such as the Mk.83/BLU-110
(1,000 lb), Mk.84/BLU-117/BLU-119 (2,000 lb), BLU-109/116/118
(2,000 lb), BLU-113/122 (5,000 lb).
The GBU-40/B / GBU-42/B
Small
Diameter Bomb II is in development, it will be equipped with a
multimode terminal seeker and two way datalink, and is expected to
enter production at the end of the decade.


Above
Boeing
GBU-39/B
Small Diameter Bomb; below weapon in flight (USAF
Photo).
Specifications
- GBU-39/B Small Diameter Bomb
| Diameter |
7.5 inches |
| Length |
70.8 inches |
| Weight |
285 lb
|
| Warhead |
Steel penetration casing
with 50 lb explosive
|
| Guidance |
Differential GPS/INS |
| Accuracy |
CEP less than JDAM
|
Range for High Altitude Drop
|
~60 nautical miles
|
| Penetration |
~6 ft of reinforced
concrete |
| Carriage |
F-15E
Strike Eagle
F-16 Fighting Falcon
F-22 Raptor
F-35 Lightning II
A-10 Thunderbolt II
F-117 Nighthawk
B-1 Lancer
B-2 Spirit
B-52 Stratofortress |
|