Credit
Universalashic · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Agni-Ilarger figure on 3 of 4
Hwasong-11Alarger figure on 1 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source15 m[source]
Length
Single sourceConfiguration
| Specification | Agni-I | Hwasong-11A |
|---|---|---|
| Type | Short Range Ballistic Missile[source] | Short-range ballistic missile[source] |
| Place of origin | India[source] | North Korea[source] |
| In service | 1979 —present[source] | 2019–present[source] |
| Used by | Strategic Forces Command[source] | North Korea ( Korean People's Army Strategic Force ) Russia[source] |
8.77 m (28.8 ft)[source]
Maximum; 2.5 km/s (
Single source2.5 km/s (9000 km/h)[source]
Warhead weight
Single source1,000 kg (2,200 lb) - 2,500 kg (5,500 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer | Defence Research and Development Organisation[source] | — |
|---|
| Manufacturer | Bharat Dynamics Limited[source] | February 11 Plant[source] |
|---|
| Unit cost | ₹ 25 crore (US$2.6 million) to ₹ 35 crore (US$3.6 million)[source] | — |
|---|
| No. built | 70 (2017 est.)[source] | — |
|---|
| Warhead | Conventional high explosive -unitary, penetration, cluster munition , incendiary , thermobaric , strategic nuclear weapon[source] | 500–1,500 kg (1,100–3,300 lb), nuclear and conventional[source] |
|---|
| Engine | Single stage composite rocket motor[source] | Solid-fueled engine[source] |
|---|
| Propellant | Solid fuel[source] | Solid composite[source] |
|---|
| Flight ceiling | 370 km[source] | — |
|---|
| Guidance system | Mid-course: RLG - INS + multi- GNSS Terminal: Radar scene matching[source] | Inertial navigation system (INS), possible satellite navigation[source] |
|---|
| Accuracy | 25 m CEP[source] | 35–200 m (115–656 ft)[source] |
|---|
| Launch platform | 8 × 8 Tatra transporter erector launcher /rail mobile[source] | 8×8 wheeled TEL Tracked launcher Railway car Silo[source] |
|---|
| Wars | — | Russo-Ukrainian war[source] |
|---|
| Designed | — | 2018[source] |
|---|
| Developed into | — | See § Variants[source] |
|---|
| Flight altitude | — | 50–60 km (31–37 mi)[source] |
|---|