FORCETALLY
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At a glance
Measured figures
Length
Single source1 m (3 ft 3 in )[source]
Naze'at 10-H rocket · Length (mm) · Length
Single sourceConfiguration
| Specification | MATADOR | Naze'at |
|---|---|---|
| Type | Recoilless gun[source] | Artillery rocket[source] |
| Place of origin | Germany Israel Singapore[source] | — |
| In service | 2000–present[source] | — |
| Used by | See Operators[source] | Iran Syria[source] |
| Wars | Gaza War (2008–09) Russo-Ukrainian War Russian invasion of Ukraine Gaza war[source] |
Naze'at 6-H rocket · Length (mm) · Length
Single sourceLength (mm): 6290[source]Naze'at 6-H rocket · Length (mm)
Length (mm): 8020[source]Naze'at 10-H rocket · Length (mm)
Mass
Single source10.350 kg (22 lb 13.1 oz )[source]
Effective; Effective firing range
Single source500 m (1,600 ft)[source]
Maximum; Naze'at 10-H rocket · Max. range (km) · Maximum firing range
Single sourceMaximum; Naze'at 6-H rocket · Max. range (km) · Maximum firing range
Single sourceNaze'at 10-H rocket · Min. range (km) · Range
Single sourceNaze'at 6-H rocket · Min. range (km) · Range
Single sourceOperational; Operational range
Single source100–130 km[source]
Max. range (km): 100[source]Naze'at 6-H rocket · Max. range (km)
Min. range (km): 80[source]Naze'at 6-H rocket · Min. range (km)
Max. range (km): 130[source]Naze'at 10-H rocket · Max. range (km)
Min. range (km): 110[source]Naze'at 10-H rocket · Min. range (km)
Caliber · source measurement 1
Single sourceCaliber · source measurement 2
Single sourceCaliber · source measurement 3
Single source90 mm (3.5 in ) 60 mm (2.4 in ) 110 mm (4.3 in )[source]
Muzzle velocity
Single source250 m/s (820 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Designer | Singapore Armed Forces , Rafael Advanced Defense Systems , Defence Science and Technology Agency[source] | — |
|---|
| Designed | 1999[source] | — |
|---|
| Manufacturer | Dynamit Nobel Defence[source] | Iran[source] |
|---|
| Unit cost | ~€5,000[source] | — |
|---|
| Feed system | Single-shot, disposable[source] | — |
|---|
| Sights | Integral optical sights Night vision device on a Picatinny rail[source] | — |
|---|
| Variants | — | Naze'at 4 Naze'at 5 Naze'at 6 Naze'at 10[source] |
|---|
| Engine | — | Solid fuel rocket[source] |
|---|
| Accuracy | — | CEP less than 5% of its range[source] |
|---|
| Launch platform | — | Transporter erector launcher[source] |
|---|
| C.E.P (%) | — | C.E.P (%): <5% Max. range[source]Naze'at 6-H rocket · C.E.P (%) C.E.P (%): <5% Max. range[source]Naze'at 10-H rocket · C.E.P (%) |
|---|
| Average Action Time (s) | — | Average Action Time (s): 9[source]Naze'at 6-H rocket · Average Action Time (s) Average Action Time (s): 10[source]Naze'at 10-H rocket · Average Action Time (s) |
|---|
| Specific Impulse (s) | — | Specific Impulse (s): 240[source]Naze'at 6-H rocket · Specific Impulse (s) Specific Impulse (s): 240[source]Naze'at 10-H rocket · Specific Impulse (s) |
|---|
| Propellant Weight (kg) | — | Propellant Weight (kg): 420[source]Naze'at 6-H rocket · Propellant Weight (kg) Propellant Weight (kg): 865[source]Naze'at 10-H rocket · Propellant Weight (kg) |
|---|
| Type of Propellant | — | Type of Propellant: Solid ( HTPB )[source]Naze'at 6-H rocket · Type of Propellant Type of Propellant: Solid ( HTPB )[source]Naze'at 10-H rocket · Type of Propellant |
|---|
| Service life | — | Service life: 7 years[source]Naze'at 6-H rocket · Service life Service life: 7 years[source]Naze'at 10-H rocket · Service life |
|---|
| Country of origin | — | Iran[source]Inventory Origin column; table 8, row 16, cell 5; revision 1377604549; retrieved 2026-09-30 |
|---|
| Reported operators | — |
|
|---|
