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At a glance
Flakpanzer Gepardlarger figure on 2 of 2
MIM-23 Hawklarger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Overall
Single sourceOverall: 7.68 m (25 ft 2 in)[source]
Length
Single sourceConfiguration
| Specification | Flakpanzer Gepard | MIM-23 Hawk |
|---|---|---|
| Type | Self-propelled anti-aircraft gun[source] | Surface-to-air missile[source] |
| Place of origin | Switzerland West Germany[source] | United States[source] |
| In service | 1976–present[source] | August 1960 –present[source] |
| Used by | See Operators[source] | — |
| Wars |
16 feet 8 inches (5.08 m)[source]
Wingspan
Single source3 feet 11 inches (1.19 m)[source]
Radar retracted
Single sourceRadar retracted: 3.29 m (10 ft 10 in)[source]
driver, gunner, commander
Single source3 (driver, gunner, commander)[source]
10- cylinder , 37,400 cc (2,280 cu in ) MTU multi-fuel engine
Single source10- cylinder , 37,400 cc (2,280 cu in ) MTU multi-fuel engine 830 PS (819 hp, 610 kW)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Russo-Ukrainian War[source] |
Cold War War of Attrition Chadian–Libyan War Iran–Iraq War Gulf War Second Libyan Civil War 2020 Turkish intervention in Libya Russo-Ukrainian War Russian invasion of Ukraine[source] |
| Designer | Oerlikon-Bührle AG (Switzerland) Contraves (Switzerland) Siemens-Albis AG (Switzerland) Krauss-Maffei AG (vehicle - West Germany)[source] | — |
|---|
| Manufacturer | Krauss-Maffei AG (licence production)[source] | Raytheon Company[source] |
|---|
| Armor | conventional steel[source] | — |
|---|
| Main armament | 2 × 35 mm Oerlikon GDF autocannon , each with 320 rounds anti-air ammunition and 20 rounds anti-tank[source] | — |
|---|
| Secondary armament | 2 × quad 76 mm smoke grenade dischargers[source] | — |
|---|
| Power/weight | 17.5 PS/t[source] | — |
|---|
| Suspension | Torsion bar suspension[source] | — |
|---|
| Warhead | — | 119 pounds (54 kg) blast fragmentation warhead[source] |
|---|
| Engine | — | solid-fuel rocket engine[source] |
|---|
| Flight ceiling | — | 65,000 feet (20,000 m)[source] |
|---|
| Guidance system | — | Semi-active radar homing[source] |
|---|
| Reported operators | — |
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|---|