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At a glance
Kh-29larger figure on 1 of 2
Zuni (rocket)larger figure on 1 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Kh-29L/T
Single sourceKh-29TE
Single sourceConfiguration
| Specification | Kh-29 | Zuni (rocket) |
|---|---|---|
| Type | Air-to-surface missile[source] | Air-to-surface rocket[source] |
| Place of origin | Soviet Union[source] | United States[source] |
| In service | 1980s–present[source] | — |
| Used by | Warsaw Pact, China, India, Iraq[source] | United States military French Air Force Ukrainian Air Force[source] |
| Wars |
Kh-29L/T: 390 cm (12 ft 10 in) Kh-29TE: 387.5 cm (12 ft 9 in)[source]
Length
Single source77 inches (2,000 mm)[source]
Warhead weight
Single source320 kg (705 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Iran–Iraq War Second Libyan Civil War Syrian Civil War Russian intervention in the Syrian civil war Russo-Ukrainian War Russo-Ukrainian war[source]
| — |
| Designer | Matus Bisnovat Georgiy I. Khokhlov[source] | — |
|---|
| Designed | 1975[source] | — |
|---|
| Manufacturer | Vympel / Tactical Missiles Corporation[source] | — |
|---|
| Produced | 1980–present[source] | 1957–present[source] |
|---|
| Warhead | HE armour-piercing[source] | various[source] |
|---|
| Detonation mechanism | Impact[source] | — |
|---|
| Engine | Fixed thrust solid fuel rocket[source] | Solid-fuel rocket[source] |
|---|
| Guidance system | Kh-29L: semi-active laser guidance Kh-29T/TE: passive homing TV guidance Kh-29D: infrared homing guidance (IIR) Kh-29MP: active radar homing[source] | None[source] |
|---|
| Launch platform | Kh-29L&T: MiG-27K, MiG-29, Su-22, Su-27UB, Su-30MK, Su-39 Kh-29L only: Su-25 Kh-29T only: Su-35 Also: Mirage F1 E, Su-17/22 , Su-24 , Su-33 , Su-34 , Su-37[source] | — |
|---|
| Reported operators |
| — |
|---|