Agni (missile) vs Fateh-110: Specs Compared

ABallistic missiles

Agni (missile)

Medium-range ballistic missile (Agni-I, Agni-II, Agni Prime) Intermediate-range ballistic missile (Agni-III, Agni-IV) Intercontinental ballistic missile (Agni-V, Agni VI)

BBallistic missiles

Fateh-110

Tactical SRBM

First system

Second system

At a glance

Side by side

Length comparisonOne shared metre scale

Agni (missile)Agni-II

21 m

Length source ↗

Fateh-110Length

8.9 m

Length source ↗

Lengths retain their source configuration and measurement scope.

Measured figures

Head to head

14 of 22 rows sourced on both sides

21mAgni-II

8.9m

Length

All recorded figures & sources

15 m

Agni-I

Single source

21 m

Agni-II

Single source

17 m

Agni-III

Single source

20 m

Agni-IV

Single source

10.5 m

Agni-P

Single source

17.5 m

Agni-V

Single source

15 m (Agni-I) 21 m (Agni-II) 17 m (Agni-III) 20 m (Agni-IV) 17.5 m (Agni-V) 10.5 m(Agni-P)^[source]

8.9 m

Length

Single source

8.90 m^[source]

2mAgni-III, Agni V

600mm

Diameter

All recorded figures & sources

1 m

Agni-I, Agni-II

Single source

2 m

Agni-III, Agni V

Single source

1.2 m

Agni-IV

Single source

1.15 m

Agni P

Single source

1.1 m

Agni VI

Single source

1.0 m (Agni-I, Agni-II) 1.2 m(Agni-IV) 2.0 m (Agni-III, Agni V) 1.1 m (Agni VI) 1.15 m (Agni P)^[source]

0.6 m

Diameter

Single source

0.60 m^[source]

55tAgni VI

3.5t

Mass

All recorded figures & sources

12,000 kg

Agni-I

Single source

16,000 kg

Agni-II

Single source

50,000 kg

Agni III

Single source

17,000 kg

Agni-IV

Single source

11,000 kg

Agni P

Single source

50,000 kg

Agni-V

Single source

55,000 kg

Agni VI

Single source

12,000 kg (Agni-I) 16,000 kg (Agni-II) 50,000 kg (Agni III) 17,000 kg (Agni-IV) 50,000 kg (Agni-V) 55,000 kg (Agni VI) 11,000 kg (Agni P)^[source]

3,500 kg

Mass

Single source

3,500 kg^[source]

11,000–12,000kmOperational; Agni VI

300kmOperational; Operational range

RangeScopes differ

All recorded figures & sources

700–1,200 km

Operational; Agni-I

Single source

2,000–3,500 km

Operational; Agni-II

Single source

3,000–5,000 km

Operational; Agni-III

Single source

3,500–4,000 km

Operational; Agni-IV

Single source

1,000–2,000 km

Operational; Agni Prime

Single source

7,000–8,000 km

Operational; Agni-V

Single source

11,000–12,000 km

Operational; Agni VI

Single source

700–1,200 km (Agni-I) 1,000–2,000 km (Agni Prime) 2,000–3,500 km (Agni-II) 3,000–5,000 km (Agni-III) 3,500–4,000 km (Agni-IV) 7,000–8,000 km (Agni-V) 11,000–12,000 km (Agni VI)^[source]

300 km

Operational; Operational range

Single source

300 km^[source]

—

500kgWarhead weight

Warhead mass

All recorded figures & sources

500 kg

Warhead weight

Single source

500 kg^[source]

Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.

Configuration

Details

Agni (missile) and Fateh-110 configuration
Specification	Agni (missile)	Fateh-110
Speed	24 Mach (Agni-V)^[source]	Mach 4^[source]
Type	Medium-range ballistic missile (Agni-I, Agni-II, Agni Prime) Intermediate-range ballistic missile (Agni-III, Agni-IV) Intercontinental ballistic missile (Agni-V, Agni VI)^[source]	Tactical SRBM^[source]
Place of origin	India^[source]	Iran^[source]
In service	Active^[source]	2002–present^[source]
Used by	India^[source]	See Operators^[source]
Designer	Defence Research and Development Organisation^[source]	—
Manufacturer	Bharat Dynamics Limited^[source]	Iran^[source]
Warhead	Conventional high explosive -unitary, penetration, cluster munitions , incendiary weapon , thermobaric , strategic nuclear weapon^[source]	high explosive or submunition^[source]
Engine	Composite rocket motor^[source]	Single stage, solid fuel rocket^[source]
Propellant	Solid fuel^[source]	—
Flight altitude	300 km (Agni-I) 230 km (Agni-II), 350 km (Agni-III)^[source]	—
Guidance system	Mid-course: Ring laser gyro inertial navigation system with GPS / NavIC satellite guidance Terminal: Imaging infrared homing , radar scene correlation, active radar homing^[source]	Inertial & electro-optical terminal (according to Iranian state media) GNSS (according to Western analysts)^[source]
Launch platform	Road/Rail mobile^[source]	Mobile launcher^[source]
Wars	—	Syrian civil war 2026 Iran War^[source]
Reported operators	—	Reported operator · Iran Reported operator · Ba'athist Syria Reported operator · Russia

FORCETALLY

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Agni (missile)

Fateh-110

Speed

24 Mach (Agni-V)^[source]

Mach 4^[source]

Type

Medium-range ballistic missile (Agni-I, Agni-II, Agni Prime) Intermediate-range ballistic missile (Agni-III, Agni-IV) Intercontinental ballistic missile (Agni-V, Agni VI)^[source]

Tactical SRBM^[source]

Place of origin

India^[source]

Iran^[source]

In service

Active^[source]

2002–present^[source]

Used by

India^[source]

See Operators^[source]

Designer

Defence Research and Development Organisation^[source]

—

Manufacturer

Bharat Dynamics Limited^[source]

Iran^[source]

Warhead

Conventional high explosive -unitary, penetration, cluster munitions , incendiary weapon , thermobaric , strategic nuclear weapon^[source]

high explosive or submunition^[source]

Engine

Composite rocket motor^[source]

Single stage, solid fuel rocket^[source]

Propellant

Solid fuel^[source]

—

Flight altitude

300 km (Agni-I) 230 km (Agni-II), 350 km (Agni-III)^[source]

—

Guidance system

Mid-course: Ring laser gyro inertial navigation system with GPS / NavIC satellite guidance Terminal: Imaging infrared homing , radar scene correlation, active radar homing^[source]

Inertial & electro-optical terminal (according to Iranian state media) GNSS (according to Western analysts)^[source]

Launch platform

Road/Rail mobile^[source]

Mobile launcher^[source]

Wars

—

Syrian civil war 2026 Iran War^[source]

Reported operators

—

Reported operator · Iran
Reported operator · Ba'athist Syria
Reported operator · Russia