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Battlefield Range Ballistic Missiles (BRBM)
HATF- I
The Hatf I is a tactical and subsonic unguided battlefield range ballistic missile jointly designed and developed by the Space Research Commission and the Kahuta Research Laboratories (KRL) in 1980s. After its successful tests, theHatf-I entered in the service with Pakistan Army in 1990. It is deployed as an artillery rocket and has been replaced by the improved Hatf-IA and Hatf-IB, which have a maximum range of 100 km.
The code name Hatf in Arabic variant means "Deadly" or "Vengeance". The name comes from the sword of Muhammed, al Hataf.
Specification
Weight 1,500 kg (3,300 lb)
Length 6 m (19 ft 8 in)
Diameter 0.56 m (22 in)
Warhead 500 kg (1,100 lb) Single/Sub-munitions, Conventional/Nuclear
Engine single stage
Propellant Solid Fuel
Operational range
Hatf-I: 70 km (43 mi)
Hatf-IA/IB: 100 km (62 mi)
Guidance system
Hatf-I/IA: unguided
Hatf-IB: Inertial guidance system
Launch platform
Transporter Erector Launcher (TEL)
Nasr (Hatf IX)
The Hatf IX is a solid fueled tactical ballistic missile system developed by National Development Complex (NDC) of Pakistan.
The ISPR described the system as "Multi-tube Ballistic Missile" because the launch vehicle carries multiple missiles. Its existence was revealed after a test in 2011 and it appears to have entered service after further testing in 2013.
Specification
Warhead plutonium nuclear warhead
Blast yield 0.5-5 kilotons
Engine Single-stage rocket motor
Propellant Solid Fuel
Operational range 60 km (37.3 mi)
Short range ballistic missiles (SRBM)
Ghaznavi
The Ghaznavi, is a hypersonic and surface to surface short range ballistic missile designed and developed by the National Development Complex, in service with the Pakistan Army's strategic command since 2004. With an optimal range of 290 km, it is named after the 11th century Muslim Turkic conqueror Mahmud of Ghazni. The missile has a length of 9.64 m, diameter of 0.99 m, launch weight of 5256 kg and is powered by a single stage solid fuel rocket motor. It is believed influenced from a Chinese design, the M-11 (NATO reporting name: CSS-7).
Weight 5,256 kg
Length 9.64 m
Diameter 0.88 m
Warhead ~700 kg of conventional HE/NE
Engine Single-stage solid fuel rocket motor
Propellant Solid fuel
Operational range 290–320 km
Abdali-I
The Abdali-I is a supersonic and tactical surface-to-surface short-range ballistic missile (SRBM) designed and developed by the Space and Upper Atmosphere Research Commission (SUPARCO), and currently in operational service with the Pakistan Armed Forces.
The Abdali program was conceived and originally designed by the Space Research Commission in 1990s. The program's first derivative was originally designed as the two-stage version of the Hatf-I, essentially a solid-propellant stage was attached to the bottom of a Hatf-I. However, the program was canceled in 1994, likely due to the purchase of the M-11 missiles from the People’s Republic of China.In 1995, SUPARCO successfully persuaded and designed a new module for the Abdali program which was started the same year.
Specification
Weight 1,750 kg
Length 9.75 m
Diameter 0.56 m
Warhead Single Conventional HE
NE 500 Kg
Engine Single stage solid propellant
Operational range 180 km
Guidance system Inertial, Terminal
Ghauri (HATF-5)
The Ghauri–I is aland-based surface-to-surface medium-range ballistic missile, in current service with the Army's Strategic Forces Command— a subordinate command of Strategic Plans Division.
Designed and developed by Missile factory, Pyongyang the missile system uses a single stage liquid fuel rocket motor to carry a payload of 700 kg to a range of 1,500 km. Two variants of the Ghauri were produced under the secretive missile research programme started in 1987 and the development of a third variant was cancelled. The Ghauri-II uses increased motor assembly length and improved propellants for an increased range of 2,300 km (1,400 mi).
The missile is named after Shahabuddin Muhammad Ghauri, while the "Hatf" designation originates from the name of the sword or lance of Muhammad.
Specification
Weight 15,850 kg (34,940 lb)
Length 15.90 m (52.2 ft)
Diameter 1.35 m
Engine Single stage liquid fuel rocket engines
Propellant Liquid fuel
Flight altitude 350 km reached in first test flight
Guidance system Inertial guidance system (IGS)
Shaheen - I
The Shaheen-I is a land-based supersonic and short-to-intermediate range surface-to-surface guided ballistic missile jointly designed and developed by the joint venture of NESCOM and the National Defence Complex (NDC).
It is dedicated and named after a species of Falcon found in the mountains of Pakistan. The Shaheen I is also designated Hatf IV. Both the Shaheen I and Shaheen IA are Pakistan's equivalent to the United States Pershing 1 and Pershing 1a missiles.
Specification
Weight Shaheen I (9,500 kg), Shaheen IA (10,000 kg)
Length 12 m
Diameter 1.0 m
Warhead 1000 kg single warhead
Engine Solid-fuel rocket
Propellant Solid-fuel
Operational range
Shaheen I (750 km)
Shaheen IA (900 km)
Medium Range Ballistic Missile (MRBM)
Ghauri-II
The Ghauri-II is a surface-to-surface medium range guided ballistic missile designed and developed by the Khan Research Laboratories. It is a single-stage liquid fuel missile system and a longer ranged variant of the Ghauri-I. The development of Ghauri-II took place in a direct response to India's Agni II. It was developed by increasing the length of the motor assembly and using improved propellants.
The Ghauri–II enjoyed distinction of being Pakistan's longest range missile until its limit was exceeded by the successful launch of the Shaheen-II which was tested in 2004.
Specification
Weight 17,800 kg
Length 18.00 m
Diameter 1.35 m
Warhead 1200 kg conventional or nuclear
Engine Single-stage liquid propellant rocket motor
Propellant Liquid fuel
Operational range 1500-1800 km
Guidance system Inertial guidance system (INS), GPS satellite guidance
Launch platform Transporter erector launcher (TEL)
Shaheen-II
The Shaheen-II is a land-based supersonic surface-to-surface medium-range guided ballistic missile. The Shaheen-II is designed and developed by the NESCOM and the National Defense Complex (NDC) of Pakistan. The Shaheen missile series is named after a falcon that lives in the mountains of Pakistan. The missile is considered to be Pakistan's equivalent to the US Pershing II.
Specifications
Weight 25,000 kg (Re-entry vehicle 1,050 kg)
Length 17.5 m
Diameter 1.4 m
Warhead Conventional high-explosive or nuclear
Engine Two-stage Solid-fuel rocket motor
Operational range 2,000 km
Flight altitude 100-300 km
Guidance system Inertial navigation system , GPS satellite guidance
Launch platform Transporter erector launcher (TEL)
HATF- I
The Hatf I is a tactical and subsonic unguided battlefield range ballistic missile jointly designed and developed by the Space Research Commission and the Kahuta Research Laboratories (KRL) in 1980s. After its successful tests, theHatf-I entered in the service with Pakistan Army in 1990. It is deployed as an artillery rocket and has been replaced by the improved Hatf-IA and Hatf-IB, which have a maximum range of 100 km.
The code name Hatf in Arabic variant means "Deadly" or "Vengeance". The name comes from the sword of Muhammed, al Hataf.
Specification
Weight 1,500 kg (3,300 lb)
Length 6 m (19 ft 8 in)
Diameter 0.56 m (22 in)
Warhead 500 kg (1,100 lb) Single/Sub-munitions, Conventional/Nuclear
Engine single stage
Propellant Solid Fuel
Operational range
Hatf-I: 70 km (43 mi)
Hatf-IA/IB: 100 km (62 mi)
Guidance system
Hatf-I/IA: unguided
Hatf-IB: Inertial guidance system
Launch platform
Transporter Erector Launcher (TEL)
Nasr (Hatf IX)
The Hatf IX is a solid fueled tactical ballistic missile system developed by National Development Complex (NDC) of Pakistan.
The ISPR described the system as "Multi-tube Ballistic Missile" because the launch vehicle carries multiple missiles. Its existence was revealed after a test in 2011 and it appears to have entered service after further testing in 2013.
Specification
Warhead plutonium nuclear warhead
Blast yield 0.5-5 kilotons
Engine Single-stage rocket motor
Propellant Solid Fuel
Operational range 60 km (37.3 mi)
Short range ballistic missiles (SRBM)
Ghaznavi
The Ghaznavi, is a hypersonic and surface to surface short range ballistic missile designed and developed by the National Development Complex, in service with the Pakistan Army's strategic command since 2004. With an optimal range of 290 km, it is named after the 11th century Muslim Turkic conqueror Mahmud of Ghazni. The missile has a length of 9.64 m, diameter of 0.99 m, launch weight of 5256 kg and is powered by a single stage solid fuel rocket motor. It is believed influenced from a Chinese design, the M-11 (NATO reporting name: CSS-7).
Weight 5,256 kg
Length 9.64 m
Diameter 0.88 m
Warhead ~700 kg of conventional HE/NE
Engine Single-stage solid fuel rocket motor
Propellant Solid fuel
Operational range 290–320 km
Abdali-I
The Abdali-I is a supersonic and tactical surface-to-surface short-range ballistic missile (SRBM) designed and developed by the Space and Upper Atmosphere Research Commission (SUPARCO), and currently in operational service with the Pakistan Armed Forces.
The Abdali program was conceived and originally designed by the Space Research Commission in 1990s. The program's first derivative was originally designed as the two-stage version of the Hatf-I, essentially a solid-propellant stage was attached to the bottom of a Hatf-I. However, the program was canceled in 1994, likely due to the purchase of the M-11 missiles from the People’s Republic of China.In 1995, SUPARCO successfully persuaded and designed a new module for the Abdali program which was started the same year.
Specification
Weight 1,750 kg
Length 9.75 m
Diameter 0.56 m
Warhead Single Conventional HE
NE 500 Kg
Engine Single stage solid propellant
Operational range 180 km
Guidance system Inertial, Terminal
Ghauri (HATF-5)
The Ghauri–I is aland-based surface-to-surface medium-range ballistic missile, in current service with the Army's Strategic Forces Command— a subordinate command of Strategic Plans Division.
Designed and developed by Missile factory, Pyongyang the missile system uses a single stage liquid fuel rocket motor to carry a payload of 700 kg to a range of 1,500 km. Two variants of the Ghauri were produced under the secretive missile research programme started in 1987 and the development of a third variant was cancelled. The Ghauri-II uses increased motor assembly length and improved propellants for an increased range of 2,300 km (1,400 mi).
The missile is named after Shahabuddin Muhammad Ghauri, while the "Hatf" designation originates from the name of the sword or lance of Muhammad.
Specification
Weight 15,850 kg (34,940 lb)
Length 15.90 m (52.2 ft)
Diameter 1.35 m
Engine Single stage liquid fuel rocket engines
Propellant Liquid fuel
Flight altitude 350 km reached in first test flight
Guidance system Inertial guidance system (IGS)
Shaheen - I
The Shaheen-I is a land-based supersonic and short-to-intermediate range surface-to-surface guided ballistic missile jointly designed and developed by the joint venture of NESCOM and the National Defence Complex (NDC).
It is dedicated and named after a species of Falcon found in the mountains of Pakistan. The Shaheen I is also designated Hatf IV. Both the Shaheen I and Shaheen IA are Pakistan's equivalent to the United States Pershing 1 and Pershing 1a missiles.
Specification
Weight Shaheen I (9,500 kg), Shaheen IA (10,000 kg)
Length 12 m
Diameter 1.0 m
Warhead 1000 kg single warhead
Engine Solid-fuel rocket
Propellant Solid-fuel
Operational range
Shaheen I (750 km)
Shaheen IA (900 km)
Medium Range Ballistic Missile (MRBM)
Ghauri-II
The Ghauri-II is a surface-to-surface medium range guided ballistic missile designed and developed by the Khan Research Laboratories. It is a single-stage liquid fuel missile system and a longer ranged variant of the Ghauri-I. The development of Ghauri-II took place in a direct response to India's Agni II. It was developed by increasing the length of the motor assembly and using improved propellants.
The Ghauri–II enjoyed distinction of being Pakistan's longest range missile until its limit was exceeded by the successful launch of the Shaheen-II which was tested in 2004.
Specification
Weight 17,800 kg
Length 18.00 m
Diameter 1.35 m
Warhead 1200 kg conventional or nuclear
Engine Single-stage liquid propellant rocket motor
Propellant Liquid fuel
Operational range 1500-1800 km
Guidance system Inertial guidance system (INS), GPS satellite guidance
Launch platform Transporter erector launcher (TEL)
Shaheen-II
The Shaheen-II is a land-based supersonic surface-to-surface medium-range guided ballistic missile. The Shaheen-II is designed and developed by the NESCOM and the National Defense Complex (NDC) of Pakistan. The Shaheen missile series is named after a falcon that lives in the mountains of Pakistan. The missile is considered to be Pakistan's equivalent to the US Pershing II.
Specifications
Weight 25,000 kg (Re-entry vehicle 1,050 kg)
Length 17.5 m
Diameter 1.4 m
Warhead Conventional high-explosive or nuclear
Engine Two-stage Solid-fuel rocket motor
Operational range 2,000 km
Flight altitude 100-300 km
Guidance system Inertial navigation system , GPS satellite guidance
Launch platform Transporter erector launcher (TEL)