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At a glance
Bateleur FV2larger figure on 1 of 1
Naze'atlarger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source8.53 m (28 ft 0 in)[source]
Naze'at 10-H rocket · Length (mm) · Length
Single sourceConfiguration
| Specification | Bateleur FV2 | Naze'at |
|---|---|---|
| Type | Multiple rocket launcher[source] | Artillery rocket[source] |
| Place of origin | South Africa[source] | — |
| In service | 1979–present[source] | — |
| Used by | South African National Defence Force[source] | Iran Syria[source] |
| Designer | Denel , Somchem[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)
Maximum; road
Single source90 km/h (56 mph) (road)[source]
V10 diesel
Single sourceV10 diesel 268hp[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Cartridge | HE-Fragmentation: 2.68 m (8 ft 10 in)[source] | — |
|---|
| Barrels | 40[source] | — |
|---|
| Rate of fire | 1 per sec[source] | — |
|---|
| Transmission | ZF 56-65 Synchromesh[source] | — |
|---|
| Suspension | Kwêvoël 100 10-ton 6x6 truck[source] | — |
|---|
| Manufacturer | — | Iran[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 |
|
|
|---|
Maximum; 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 source