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At a glance
Dhanush (howitzer)larger figure on 0 of 1
M-46 field gunlarger figure on 1 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | Dhanush (howitzer) | M-46 field gun |
|---|---|---|
| Type | Howitzer[source] | Towed field gun[source] |
| Place of origin | India[source] | Soviet Union[source] |
| In service | 2019 - present[source] | — |
| Used by | Indian Army[source] | — |
| Wars | 2025 India–Pakistan conflict[source] |
Width
Single source2.45 m (8 ft)[source]
Maximum; for Ramjet Shell
Single sourceMaximum; L/45
Single sourceMaximum; (L/52) >
Single source38 km (L/45) 42 km (L/52) >60 km (for Ramjet Shell )[source]
Maximum; base-bleed
Single sourceMaximum; rocket assisted
Single sourceMuzzle velocity
Single source930 m/s (3,051 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Vietnam War Cambodian Civil War Eritrean War of Independence South African Border War Six-Day War Yom Kippur War Ethiopian Civil War Angolan Civil War Uganda–Tanzania War Sino-Vietnamese conflicts (1979–1991) Lebanese Civil War Iran–Iraq War Sri Lankan Civil War First Nagorno-Karabakh War Yugoslav Wars Kosovo War Syrian Civil War Yemeni Civil War (2014–present) Second Nagorno-Karabakh War Tigray War Israeli–Lebanese conflict Russo-Ukrainian War[source] |
| Designer | Ordnance Factory Board[source] | — |
|---|
| Designed | 2010 - 2013[source] | 1946–1950[source] |
|---|
| Manufacturer | Advanced Weapons and Equipment India Limited (previously Ordnance Factory Board )[source] | MOTZ[source] |
|---|
| Unit cost | ₹ 14 crore (US$1.5 million)[source] | — |
|---|
| Produced | 2014 - present[source] | 1951–1971[source] |
|---|
| No. built | >72 (excl. 12 prototypes)[source] | — |
|---|
| Action | Auto gun alignment and positioning[source] | — |
|---|
| Breech | Screw type[source] | Horizontal sliding-wedge[source] |
|---|
| Recoil | Electro-rheological/Magneto-rheological[source] | hydro-pneumatic[source] |
|---|
| Elevation | Servo based, -3°/+70°[source] | −2.5° to 45°[source] |
|---|
| Traverse | Servo based, 30° left or right from centreline[source] | 50°[source] |
|---|
| Feed system | Electrically operated ammunition handling[source] | — |
|---|
| Sights | Thermal sight Gunners display[source] | — |
|---|
| Shell | — | 130 x 845 mm R (R/184.6mm) separate-loading charge and projectile[source] |
|---|
| Carriage | — | Split-trail[source] |
|---|
| Reported operators |
|
|
|---|
Maximum; unassisted
Single source27.15 km (16.87 mi) (unassisted) 35 km (22 mi) (base-bleed) 44 km (27 mi) (rocket assisted)[source]