2. ABDALI-1
System: Abdali-1
Alternative Name: Hatf-II
Type: SRBM
Range: 180 km (108 miles)
Payload: 500 kg
Warhead: Single Conventional HE
Propellant Fuel: Solid
Guidance System: Inertial
Velocity: -
Apogee: -
CEP: 250 m
Stage(s): 1
Height: 9.750 m
Diametre: 0.550 m
Weight: 2,520 kg - 3,000 kg (lift-off)
TEL: ? (mounted on vertical rail launcher)
Developer: NDC
Test Dates: 03.07.1997, 28.05.2002, 26.03.2003
Launch Location(s): Sonmiani, District Lasbela, Balochistan
Status: Deployed, Under Production
3. GHAZNAVI-1
System: Ghaznavi-1
Alternative Name: Hatf-III
Type: SRBM
Range: 290 km (180 miles)
Payload: 500 kg
Warhead: Single Conventional/Nuclear
Propellant Fuel: Solid
Guidance System: Inertial
Velocity: -
Apogee: -
CEP: 250 m
Stage(s): 1
Height: 8.5 m (9.64 m?)
Diametre: 0.8 m
Weight: 4,000 kg (launch)
TEL: 8x8 MAZ-543
Developer: PMO
Test Date(s): 26.05.2002, 03.10.2003 (at 0842 hrs PST or 0342 hrs GMT)
Launch Location(s): Sonmiani, District Lasbela, Balochistan
Status: Undergoing Testing
4. SHAHEEN-1
System: Shaheen-1
Alternative Name: Hatf-IV
Type: MRBM
Range: 750 km (430 miles)
Payload: 1,000 kg
Warhead: Nuclear
Propellant Fuel: Solid
Guidance System: Terminal
Velocity: -
Apogee: -
CEP: 50 m
Stage(s): 1
Height: 9.100 m
Diametre: 1.000 m
Weight: 6,200 kg (lift-off)
TEL: 8x8 MAZ-543 (modified)
Developer: NDC
Test Dates: Static engine tests: 1997, 1998. Flight tests: 15.04.1999 (at 0958 hrs PST or 0458 hrs GMT ) over 450 km, flight time was 6 minutes, 12 seconds, 04.10.2002 (at 0830 hrs PST or 0230 hrs GMT), 08.10.2002, 08.10.2003 (at 0813 hrs PST or 0313 GMT) (ground-burst test of warhead), 14.10.2003 (air-burst test of warhead)
Launch Location(s): Sonmiani, District Lasbela, Balochistan
Status: Deployed (06.03.2003), Under Production
5. GHAURI-I
System: Ghauri-I
Alternative Name: Hatf-V
Type: MRBM
Range: 1,500 km (930 miles)
Payload: 700 kg (1,547 lbs.)
Warhead: 15 to 35 kT Nuclear
Propellant Fuel: Liquid - TM 185 (20% High Octane Jet Fuel, 80% Kerosene), AK-27I Oxidizer (27% N2O4, 73% HNO3), Iodium Inhibitor
Guidance System: Inertial
Velocity: -
Apogee: 350 km
CEP: 250 m/820 ft at 1,500 km
Stage(s): 1
Height: 15.852-16.000 m
Diametre: 1.320-1.350 m
Weight: 16,000 kg (16 tonnes), 14,000 kg (14 tonnes) (fuel)
TEL: 6x4 (prime-mover with 8-wheel trailer)
Developer: KRL
Test Dates: 06.04.1998 (at 0723 hrs covering 1,100 km/682 miles in 9 minutes, 58 seconds), 25.05.2002
Launch Location(s): 06.04.1998 Test: Malute, Tilla Jogian, District Jhelum, Punjab; 25.05.2002 Test: Dallana, District Dera Ghazi Khan, Punjab near the Suleiman Range, monitoring station was set up at Basti Jarh, 6 km from the launch site on the D.G. Khan-Quetta Road
Status: Deployed (08.01.2003) with Pakistan Army's 47th Artillery Brigade, Under Production
6. GHAURI-II
System: Ghauri-II
Alternative Name: Hatf-VI
Type: MRBM
Range: 2,000/2,300 km (1,240/1,440 miles)
Payload: 1,000/700 kg
Warhead: Single Nuclear
Propellant Fuel: Liquid
Guidance System: -
Velocity: -
Apogee: 350 km
CEP: 250 m
Stage(s): 1
Height: 18.000 m
Diametre: 1.320-1.350 m
Weight: 17,800 kg
TEL: 6x4 (prime-mover with 8-wheel trailer)
Developer: KRL
Test Dates: 14.04.1999 (covering 1,150 km)
Launch Location(s): Malute, Tilla Jogian, District Jhelum, Punjab
Status: Operationalized, Under Production
7. Shaheen-2
System: Shaheen-2
Alternative Name: None
Type: IRBM
Range: 2,500 km (1,500 miles)
Payload: 1,000 kg
Warhead: Nuclear
Propellant Fuel: Solid
Guidance System: Terminal
Velocity: -
Apogee: -
CEP: 50 m
Stage(s): 2
Height:
Diametre:
Weight:
TEL: 12x4
Developer: NDC
Test Date(s): Not Flight Tested, warhead tested in 2003
Launch Location(s): Not Applicable
Status: Awaiting Testing
8. GHAURI-III
System: Ghauri-III
Alternative Name: Hatf-VII?
Type: IRBM
Range: 2,500/3,500 km?
Payload: 1,000/700 kg
Warhead: Nuclear
Propellant Fuel: -
Guidance System: -
Velocity: -
Apogee: -
CEP: 250 m
Stage(s): 2
Height:
Diametre:
Weight:
TEL: ?
Developer: KRL
Test Date(s): Not Flight Tested, 29.09.1999 (static engine test)
Launch Location(s): Static engine test was carried out at Kahuta, District Rawalpindi, Punjab, flight test was postponed after being scheduled for launch from Mankera, District Mianwali, Punjab on 28.05.2002,
Status: Under Research & Development