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Measured figures
Super 530D
Single sourceSuper 530F
Single sourceConfiguration
| Specification | Super 530 | Typhon missile system |
|---|---|---|
| Speed | Super 530F: Mach 4.5 Super 530D: Mach <5.0[source] | — |
| Warhead | 30 kg (66 lb) high-explosive fragmentation[source] | — |
| Detonation mechanism | Super 530F: RF Super 530D: Semi-Active Radar[source] | — |
| Engine | Solid-fuel rocket motor[source] | HEMTT[source] |
| Guidance system | Semi-active radar homing (SARH)[source] |
Super 530F: 3.54 m (11 ft 7 in) Super 530D: 3.80 m (12 ft 6 in)[source]
Super 530D
Single sourceSuper 530F
Single sourceSuper 530F: 0.88 m (2 ft 11 in) Super 530D: 0.62 m (2 ft)[source]
Super 530D
Single sourceSuper 530F
Single sourceSuper 530F: 245 kg (540 lb) Super 530D: 270 kg (600 lb)[source]
Operational; Super 530D
Single sourceOperational; Super 530F
Single sourceSuper 530F: 25 km (16 mi) Super 530D: 40 km (25 mi)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
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| Former operator · France | France[source] | — |
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| Former operator · Brazil | Brazil[source] | — |
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| Former operator · Iraq | Iraq[source] | — |
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| Former operator · Spain | Spain[source] | — |
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| Former operator · Jordan | Jordan[source] | — |
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| Former operator · Kuwait | Kuwait[source] | — |
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| Former operator · Qatar | Qatar[source] | — |
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| Role | French short to medium-range air-to-air missile[source] | — |
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| National origin | France[source] | — |
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| Source measurement | The Super 530F and Super 530D share the same general aerodynamic features and internal layout with cruciform low aspect ratio wings, cruciform aft controls, and 30 kg high explosive fragmentation warhead. However the 530D has a lengthened stainless steel body. This allows it to accommodate a more powerful dual-thrust solid propellant motor and a new seeker assembly. The new seeker includes doppler filtering for improved low altitude performance and digital micro-processing to enable the seeker to be reprogrammed against new threats.[source]Super 530 · Lead; only the objects and conditions stated in this passage The 530D has a claimed maximum interception altitude of 24,400 m (80,100 ft), with a snap-up capability of 12,200 m (40,000 ft), and a snap-down capability to targets at 60 m (200 ft). The missile has a range of 40 km and a maximum speed of less than Mach 5.[source]Super 530 · Lead; only the objects and conditions stated in this passage | — |
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| Type | — | Transporter erector launcher[source] |
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| Place of origin | — | United States[source] |
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| In service | — | 2023–present[source] |
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| Used by | — | United States Army[source] |
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| Manufacturer | — | Lockheed Martin[source] |
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| Reported operators |
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