FORCETALLY
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Measured figures
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Single sourceKS–172
Single sourceConfiguration
| Specification | Novator KS-172 | Typhon missile system |
|---|---|---|
| Type | Long range air-to-air missile[source] | Transporter erector launcher[source] |
| Place of origin | Russia/India[source] | United States[source] |
| In service | N/A(;)[source] | 2023–present[source] |
| Used by | Russian Air Force[source] |
6.01 m (19.7 ft) + 1.4 m (4.6 ft) (KS–172)[source]
KS–172
Single source61 cm (24 in) (KS–172)[source]
KS–172
Single source40 cm (16 in) (KS–172)[source]
KS–172
Single source748 kg (1,650 lb) (KS–172)[source]
Maximum; 1.1 km/s; Mach 3.3) (KS–172
Single sourceMaximum; Maximum speed
Single source4,000 km/h (2,500 mph; 1.1 km/s; Mach 3.3) (KS–172)[source]
Operational; At least possibly
Single sourceOperational; Operational range
Single sourceAt least 200 km, possibly 300–400 km (160–210 nmi)[source]
Warhead weight
Single source50 kg (110 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
United States Army[source] |
| Designer | NPO Novator[source] | — |
|---|
| Designed | 1991[source] | — |
|---|
| Manufacturer | NPO Novator Defence Research and Development Organisation[source] | Lockheed Martin[source] |
|---|
| Warhead | HE fragmentation (KS–172)[source] | — |
|---|
| Engine | Tandem rocket booster (KS–172)[source] | HEMTT[source] |
|---|
| Propellant | Solid fuel[source] | — |
|---|
| Flight altitude | 3 m (9.8 ft)–30,000 m (98,000 ft) (KS–172)[source] | — |
|---|
| Guidance system | Mid-course: Inertial navigation with mid-course guidance Terminal: Active radar homing (KS–172)[source] | — |
|---|
| Launch platform | Su-27 , Su-30 , Su-35 , Su-30MKI , (proposed), MiG-31 BM[source] | — |
|---|
| Reported operators | — |
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