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Measured figures
Configuration
| Specification | AIM-54 Phoenix | SMART (missile) |
|---|---|---|
| Type | Long range BVR air-to-air missile[source] | Anti-submarine missile[source] |
| Place of origin | United States[source] | India[source] |
| In service | 1974–present[source] | — |
| Used by | United States Navy (former) Iranian Air Force[source] | Indian Navy[source] |
Wingspan
Single source2 ft 11 + 1 ⁄ 2 in (0.9 m)[source]
AIM-54A/B
Single sourceAIM-54C
Single sourceAIM-54A/B - 976 lb (443 kg) AIM-54C – 1,015 lb (460 kg)[source]
Maximum; AIM-54A/B - Mach 4.3 (
Single sourceMaximum; ) AIM-54C – Mach 5 (
Single sourceMaximum; Maximum speed · source measurement 3
Single sourceMaximum; Maximum speed · source measurement 4
Single sourceAIM-54A/B - Mach 4.3 (1,460 m/s; 4,800 ft/s) AIM-54C – Mach 5 (1,700 m/s; 5,600 ft/s)[source]
Mach 2.5[source]
Warhead weight
Single source133 lb (60.33 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer |
|---|
Hughes Aircraft Company[source] |
Defence Research and Development Organisation[source] |
| Designed | 1960–1966[source] | 2018–19[source] |
|---|
| Manufacturer | Hughes Aircraft Company Raytheon Corporation[source] | — |
|---|
| Unit cost | US$ 477,131 (1974 FY)[source] | — |
|---|
| Produced | 1966-1993[source] | — |
|---|
| Warhead | AIM-54A/B - HE continuous rod AIM-54C – HE Mk 82; WDU‐29/B continuous rod[source] | Advanced Light-Weight Torpedo[source] |
|---|
| Detonation mechanism | Proximity fuze[source] | — |
|---|
| Engine | Solid propellant rocket motor[source] | Two- stage solid rocket[source] |
|---|
| Flight ceiling | 103,500 ft (31.5 km)[source] | — |
|---|
| Guidance system | Semi-active radar homing and terminal phase active radar homing[source] | INS + mid-course update via datalink[source] |
|---|
| Launch platform | Grumman F-14 Tomcat[source] | 8 × 8 BEML - Tatra TEL Surface ship[source] |
|---|
| References | Janes[source] | — |
|---|
| Role | — | canister-based, long-range supersonic anti-submarine missile[source] |
|---|
| Source measurement | — | SMART is a canisterised hybrid system, made up of a long-range missile carrier that can travel at supersonic speed and a lightweight torpedo as payload, for anti-submarine warfare (ASW) role. The objective behind the project was to develop a quick-reaction system that can launch torpedoes from standoff distance . The missile has a range of 643 km (400 mi) carrying a lightweight torpedo of range 20 km (12.5 mi) with 50 kg high explosive warhead. SMART uses two-way data link connected to airborne or ship based submarine detection and identification systems. SMART can be launched from a surface ship or a truck-based coastal battery.[source]SMART (missile) · Description; only the objects and conditions stated in this passage |
|---|
| Reported operators |
| — |
|---|