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Measured figures
Configuration
| Specification | TL-10 | Typhon missile system |
|---|---|---|
| Speed | ≈ Mach 0.85[source] | — |
| Type | anti-ship / air-to-surface missiles[source] | Transporter erector launcher[source] |
| Place of origin | China[source] | United States[source] |
| In service | prior to 2006 – present[source] | 2023–present[source] |
Wingspan
Single source568 mm (22.4 in)[source]
Operational; Operational range
Single source4–25 km (2.5–15.5 mi)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Used by | China[source] | United States Army[source] |
|---|
| Manufacturer | Hongdu Aviation Industry Corporation[source] | Lockheed Martin[source] |
|---|
| Produced | prior to 2006[source] | — |
|---|
| Warhead | 30 kg (66 lb)[source] | — |
|---|
| Detonation mechanism | Semi-armor-piercing[source] | — |
|---|
| Engine | rocket motor[source] | HEMTT[source] |
|---|
| Propellant | dual thrust chamber, solid rocket motor[source] | — |
|---|
| Guidance system | INS , active radar homing ( ARH ), imaging infrared (IIR), TV/CCD, semi-active laser (SAL)[source] | — |
|---|
| Launch platform | Air & surface[source] | — |
|---|
| Reported operators |
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