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BRadar & sensors
medium-range anti-aircraft missile and gun fire control system
Measured figures
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Central acquisition radar (3D-CAR) | Mark 92 Guided Missile Fire Control System |
|---|---|---|
| Country of origin | India[source] | — |
| Manufacturer | Bharat Electronics Limited[source] | — |
| Designer | Electronics and Radar Development Establishment ( DRDO )[source] | — |
| Type | Primary surveillance radar[source] | medium-range anti-aircraft missile and gun fire control system[source] |
| Frequency |
|---|
S band[source] |
| — |
| Altitude | 18 kilometres (11 mi)[source] | — |
|---|
| Azimuth | >±0.5°[source] | — |
|---|
| Elevation | 5 Mrad upto 100 Km[source] | — |
|---|
| Other names | ROHINI REVATHI[source] | — |
|---|
| Origin | — | US-built[source] |
|---|
| Design relationship | — | licensed USN version of the Thales Nederland WM-25 fire control system[source]Licenceddesignrelation only, not ThalesWM25manufacturer inference |
|---|
| In service | — | 1975[source] |
|---|
| Radar architecture | — | two or three radar sub-systems depending on the model[source] |
|---|
| Sights and sensors | — | track while scan radar (Search) and a tracking radar both housed in an egg shaped radome[source] |
|---|
| Illuminator | — | Separate Target Illumination Radar or STIR[source]Additionalilluminationradar wherefitted; notallMods |
|---|
| Current service evidence | — | STIR radars are still in use on non-USN vessels[source] |
|---|
| Reported operators |
| — |
|---|