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Measured figures
Configuration
| Specification | M53/59 Praga | Project Kusha |
|---|---|---|
| Type | Self-propelled anti-aircraft gun[source] | Long-range surface-to-air missile[source] |
| Place of origin | Czechoslovakia[source] | India[source] |
| In service | 1959−1992 (Czechoslovakia)[source] | 2028 (planned)[source] |
| Used by | See operators[source] | Indian Air Force (on order) Indian Navy (planned) |
Width
Single source2.35 m (7 ft 9 in)[source]
driver, commander and two gun operators
Single source4 (driver, commander and two gun operators)[source]
Effective; Effective firing range
Single sourceMaximum; horizontal
Single sourceMaximum; vertical
Single sourceOperational; Operational range
Single source3,000 m (9,800 ft)[source]
9,700 m (31,800 ft) (horizontal) 6,300 m (20,700 ft) (vertical)[source]
500 km (310 mi)[source]
Operational; M1
Single sourceOperational; M2
Single sourceTatra T912-2 6-cylinder air-cooled diesel at 2,200 rpm
Single sourceTatra T912-2 6-cylinder air-cooled diesel 110 hp (82 kW) at 2,200 rpm[source]
per barrel (cyclic)
Single sourceper barrel (practical)
Single source450−500 rpm per barrel (cyclic) 150 rpm per barrel (practical)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Gulf War Yugoslav Wars Second Congo War[source] | — |
|---|
| Produced | 1959–1978[source] | — |
|---|
| No. built | 900+[source] | — |
|---|
| Shell | Armour-piercing incendiary (API) High-explosive incendiary (HEI)[source] | — |
|---|
| Barrels | — |
|---|
| Action | Gas-operated[source] | — |
|---|
| Elevation | -10° – +85°[source] | — |
|---|
| Traverse | 360°[source] | — |
|---|
| Feed system | 50-round box magazines[source] | — |
|---|
| Armor | Steel, 10 mm (0.39 in) max (estimated)[source] | — |
|---|
| Main armament | 30 mm twin AA autocannon (600−900 rounds)[source] | — |
|---|
| Power/weight | 11.57 hp/t (8.63 kW/t)[source] | — |
|---|
| Transmission | Manual with 4 forward and 2 reverse gears[source] | — |
|---|
| Fuel capacity | 120 L (26 imp gal; 32 US gal)[source] | — |
|---|
| Manufacturer | Praga[source] | Radars and control systems Bharat Electronics Missiles Bharat Dynamics Limited Solar Industries[source] |
|---|
| Designer | — | Defence Research and Development Laboratory Bharat Electronics[source] |
|---|
| Designed | — | 2023 - present[source] |
|---|
| Warhead | — | High explosives , fragmentation[source] |
|---|
| Detonation mechanism | — | Optical proximity fuze , hit-to-kill[source] |
|---|
| Engine | — | Dual pulse rocket motor + booster[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight altitude | — | 30 km (98,000 ft)[source] |
|---|
| Guidance system | — | Mid-course: INS + GNSS -assisted mid-course adjustment Terminal: AESA mmWave RF / IIR hybrid[source] |
|---|
| Launch platform | — | Transporter Erector Launcher[source] |
|---|
| Source measurement | — | The missile system might be used to bridge the gap between the MR-SAM (80 km) and S-400 (400 km). It is being developed as an area-defence system. The Indian Air Force will be the lead agency for this air defence system.[source]Project Kusha · Development; only the objects and conditions stated in this passage The seekers are being developed by Research Centre Imarat , while the Defence Research and Development Laboratory is in charge of interceptor development. As of August 2024, DRDO was about to start the fabrication process of 5 M1 missiles (range of 150 km). DRDO has also placed order for 20 sets of airframes, 20 sets of rocket motors, 50 sets of kill vehicles (warhead), onboard & ground transceivers for telemetry . The missiles are expected to begin testing in early 2025.[source]Project Kusha · Development; only the objects and conditions stated in this passage The maiden test of the missile system was conducted on 23 July 2026 from the Launch Complex IV (LC-IV) of the Integrated Test Range (ITR) at the Abdul Kalam Island . The missile was fired against an electronic target simulating high-speed and high-altitude aerial adversaries. The system's performance envelope was validated by the interceptor's successful kill beyond 142 km, despite the intended engagement distance of 120 km.[source]Project Kusha · Trials; only the objects and conditions stated in this passage The missile system, often compared to Russia's S-400 missile system , includes three variants of interceptor missiles, designated M1, M2 and M3. The missiles will have ranges of 150 km (93 mi), 250 km (160 mi) and 350–400 km (220–250 mi), respectively. While all the variants will share the same kill vehicle, they will have different boosters to meet different ranges. This system will also feature advanced long-range surveillance and fire control radars. The air defence system will be capable of detecting and destroying enemy assets like cruise missiles , hypersonic weapons , stealth fighter jets, and drones at around 250 km range and larger aircraft like airborne early warning and control at a range of 350 km.[source]Project Kusha · Design; only the objects and conditions stated in this passage Gallium nitride transmit-receive modules (T/R modules) and digital beam-forming will be used in Project Kusha's S-band Long Range Battle Management Radar to provide an expanded surveillance coverage beyond 500 km against airborne threats. The 360-degree rotating S-band AESA radar will be more resistant to electronic jamming, have better target resolution against low- RCS threats, and will reject clutter more effectively.[source]Project Kusha · Design; only the objects and conditions stated in this passage The development of a long-range naval version that can intercept anti-ship ballistic missile hitting up to Mach 7 is underway, with a range of more than 250 km (160 mi). According to DRDO, the interceptor missile will prioritize saturation strikes above single-target precision alone, with a single-shot kill probability of over 80 percent, and above 90 percent in coordinated salvo engagements.[source]Project Kusha · Design; only the objects and conditions stated in this passage |
|---|
| Reported operators |
|
|
|---|
Operational; M3
Single sourceM1 : 120–150 km (75–93 mi) M2 : 250 km (160 mi) M3 : 350–400 km (220–250 mi)[source]