QUOTE(SUNNY92 @ Jul 5 2008, 12:54 AM)

I am sure with a little improvement, Pakistani produced "Hafar" system can be just as effective.
Yes today we are developing a new and an improved version of the HAFR, known as HAFR II at AWC (Air Weapon Complex)
Details;1)Target penetration bomb used to neutralize concrete targets like runways, bunkers etc.
2)The effect of destruction is obtained by high speed penetration and then upheaval of hard targets by exploding the warhead with minimum risk to the delivering aircraft.
3)The bomb can be released at high speeds and low altitude to avoid enemy defenses.
4)Upon delivery, the bomb decelerates to a very low speed to obtain the penetration angle and to increase the safety distance between the bomb and the releasing aircraft. Subsequently the firing of the rocket motor accelerates the bomb to a very high speed for penetration into the hard target.
Release envelope 450 < IAS < 600 Knots
Z > 200 feet
Consists of four main sub-assemblies:-
1)The Warhead: located at the front and weighs approximately 100 kg
2)The Sequencer Assembly: located immediately behind the warhead and controls the sequence of operations
3)The Parachute Section: attaches to the rear skirt of the booster by a jettisonable clamp ring and contains two drag chutes (deceleration and main)
4)The Rocket Motor: double base propellant, burns for 0.45 seconds and provides a thrust of 10 tons
(X)Can be carried on NATO standard suspension systems
Safety1)No electrical ignition
2)Drag chutes are not locked during captive flight
3)The rocket motor does not fire if drag chutes are not deployed for sufficient time
4)The warhead fuze pyrotechnical train stays out of line before firing of rocket motor.
OperationStored in a special sealed container, allowing installation on the aircraft directly from the container without any pre-installation assembly or adjustment.
Retarded phase: 1)Deployment of the first drag chute
2)Ejection of the first drag chute and deployment of the main chute
3)Measurement of the acceleration/time conditions
Acceleration phase:1)Ejection of the main chute and ignition of the rocket motor
2)Accelerates to 280 m/s in 0.45seconds
3)Impact and explosion after penetration
In case of emergency jettisoning, bomb drops completely inert.DimensionsOverall Length: 2491 mm
Length excluding the Front Fairing: 2414 mm
Maximum Body Diameter: 223 mm
Maximum Span: 430 mm
Approximate Overall Propelled Weight: 165 kg
Approximate Launch Weight: 200 kg