pak ballistic missiles
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A ballistic missile is amissile that follows a sub-orbital
ballistic flightpath with theobjective of delivering one or morewarheads to a predetermined
target
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The missile is only guided during therelatively brief initial powered phaseof flight
its course is subsequently governed
by the laws oforbital mechanicsand ballistics
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Ballistic Missile
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Ballistic Missile ProgramEvolution
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Ballistic Missile Type
Intermediate Range
Medium Range
Short Range
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Short Range
Hatf-I
Abdali
Ghaznavi Shaheen-I
M-11
Nasr
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Hatf Series
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Hatf - I
Warhead : 500 kg Single/Submunitions,Conventional/Nuclear
Engine : Single stage
Propellant : Solid
Operational range : Hatf-I: 70 km (43mi)
Hatf-IA/IB:100 km (62 mi)
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Hatf I (Contd.)
Guidance system : Hatf-I/IA : UnguidedHatf-IB:Inertial guidance
system
Launch platform :Transporter erectorlauncher
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Hatf Varients
Hatf I
Maximum range : 70 km
Payload : 500 kg, unguided. Hatf IA
Maximum range : 100 km
Payload : 500 kg, unguided.
Hatf IB
Maximum range : 100 km
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Abdali - I
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Abdali-I
In service : Since 1996
Manufacturer : National DefenceComplex
Weight : 1,750 kg
Length : 9.75 m
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Abdali - I
Diameter : 0.56 m
Warhead : 500 kg SingleConventional HE/Nuclear
Engine : Single stage
Propellant : Solid propellant
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Operational range : 180 km
Guidance system : Inertial, Terminal
Launch platform :Transporter erectorlauncher
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Ghaznavi
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Ghaznavi
The Hatf-III was named GhaznaviMissile
It is based on a Chinese design, theM-11 (NATO reporting name: CSS-7)
First test-launched in lateSeptember/early October 2003
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Ghaznavi
In service : March 2004
Weight : 5,256 kg
Length : 9.64 m
Diameter : 0.88 m
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Ghaznavi
Warhead : Conventional highexplosive or nuclear warhead
Engine : Single-stage solid fuelrocket motor
Propellant : Solid fuel
Operational range : 290 km
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Shaheen
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Shaheen
Equipped with the latest PSAC (Post-Separation Attitude Correction) system
Can adjust the warhead trajectory forgreater accuracy
Can evade anti-ballistic missile defencesystems
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Shaheen
In service : 6 March 2003
Manufacturer : National DefenceComplex
Varients : Shaheen I (1999)Shaheen IA (2012)
Weight : Shaheen I (9,500 kg)Shaheen IA (10,000 kg)
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Shaheen
Length : 12 m
Diameter : 1 m
Warhead :1000 kg single warhead
3-5 200-300 kg MIRVed warheads
Engine : solid fuel rocket motor
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Shaheen
Propellant : Solid fuel
Operational range : Shaheen I (750km)Shaheen IA (1500km)
Launch platform :Transporter erectorlauncher
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M 11(Dongfeng 11)
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M 11(Dongfeng 11)
In service : Early 1990
Manufacturer : CASIC Sanjiang SpaceGroup (also Base 066)
Weight : 4,200kg
Length : 7.5 m
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M 11(Dongfeng 11)
Diameter : 0.8 m
Warhead : 500 kg SingleConventional HE/Nuclear
Engine : Single stage
Propellant : Solid propellant
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M 11(Dongfeng 11)
Operational range : 280 - 350 km
Guidance system : Inertial, Terminal
Launch platform :Transporter erector
launcher
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Nasr
Also known as Hatf IX, is a solid fuelledbattlefield range ballistic missile
Developed as a "low-yield battlefielddeterrent" targeted at "mechanized forceslike armed brigades and divisions
Believed that the system is deployed todeter and respond to India's "Cold Start
Doctrine"
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Nasr
In service : 19 April 2011
Manufacturer : National DevelopmentComplex
Warhead : Sub-kiloton tactical nuclearwarhead (
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Nasr
Propellant : Solid fuel
Operational range : 60 km
Launch platform :Transporter erectorlauncher
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Ghauri
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Ghuari - 1
first test-fired on 6 April 1998 from Malute
Two variants of the Ghauri were producedunder the Pakistani missile research anddevelopment program
United States government states that theGhauri design is based on North Korea'sRodong-1 (also known as Nodong-1)missile
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Ghuari - 1
In service : 12 January 2003
Manufacturer : Kahuta ResearchLaboratories (KRL)
Weight : 15,850 kg
Length : 15.90 m
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Ghuari - 1
Diameter : 1.35 m
Engine : Single stage liquid fuelrocket motor
Propellant : Liquid fuel
Operational range : 1,500 km
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Ghauri - 1
Flight altitude : 350 km reached in firsttest flight
Guidance system : Inertial guidancesystem (INS)
Launch platform :Transporter erectorlauncher
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Ghauri-II
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Ghauri-II
A longer ranged variant of the Ghauri-I
Developed by increasing the length of themotor assembly and using improvedpropellants
First flight test occurring in 1998
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Ghauri-II
In service : Early 2000
Manufacturer : Kahuta ResearchLaboratories
Weight : 17,800 kg
Length : 18.00 m
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Ghauri-II
Diameter : 1.35 m
Warhead : 1200 kg conventional ornuclear
Engine : Single-stage liquidpropellant rocket motor
Propellant : Liquid fuel
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Ghauri-II
Operational range : 2,000 km (with 1,200kg payload)
2,500 km (with 750 kgpayload)
Guidance system : Inertial guidancesystem (INS), GPS satelliteguidance
Launch platform :Transporter erectorlauncher
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Shaheen-II
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Shaheen-II
Is a MRBM developed by NESCOM'sNational Defence Complex
Is among most advanced missiles inPakistans arsenal
The missile is stated to have a CEP of 30-50m
Shaheen-II warhead may change its
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Shaheen-II
In service : 9 March 2004
Manufacturer : National DefenceComplex
Weight : 25,000 kg(Re-entry vehicle 1,050 kg)
Length : 17.5 m
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Shaheen-II
Diameter : 1.4 m
Warhead : Conventional high-explosiveor nuclear
Engine : Two-stage solid fuel rocketmotor
Operational range : 2,500 km
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Shaheen-II
Flight altitude : 100-300km
Guidance system : Inertial navigationsystem
GPS satellite guidance
Launch platform :Transporter erectorlauncher
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Ghauri - III
Development for Ghauri-III started around1999
Developed by Pakistan with the logisticalsupport of China
It has three liquid fuel rocket stages
Further development was stopped by thenhead of state Gen. Parvez Musharraf
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Ghauri - III
Manufacturer : Kahuta ResearchLaboratories
Warhead : Conventional or nuclear
Engine : Multi-stage liquid fuelrocket
Propellant : Liquid fuel
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Ghauri - III
Operational range : 3,000-3,500 km
Guidance system : Inertial guidance
Launch platform : Transporter erectorlauncher
Development cancelled in : May 2000 byGen. Musharraf
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Shaheen-III
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Shaheen-III
Designer : NESCOM and SUPARCO
Manufacturer : Nescom and Suparco
Warhead : Conventional or nuclear
Engine : Multi-stage Solid fuel rocket
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Shaheen-III
Propellant : Solid-fuel system
Guidance system : Inertial guidance
Launch platform :Transporter erectorlauncher (TEL)
Transport : Spaceport or TEL
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Shaheen - IA
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Shaheen - IA
Is an intermediate-range missile
Successfully test-fired ballistic missile onApril 25, 2012
Capable of delivering nuclear warheads as
far as Beijing and Eastern Europe
capable of hitting targets up to 2,500 to
3,000km away - putting India well within
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can carry nuclear and conventionalwarheads