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At a glance
Nimrod (missile)larger figure on 1 of 3
Python (missile)larger figure on 2 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source265 cm[source]
Length
Single sourceConfiguration
| Specification | Nimrod (missile) | Python (missile) |
|---|---|---|
| Type | long-range air-to-surface missile[source] | Short-range air-to-air missile[source] |
| Manufacturer | Israel Aerospace Industries[source] | Rafael Advanced Defense Systems[source] |
| Guidance | semi-active laser guidance system[source] Semi-active laser homing[source] | — |
| Launch platform | towed launchers, light combat vehicle launchers, helicopters , and fixed-wing aircraft[source] |
3.1 metres (10 feet )[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Aircraft: BAE Sea Harrier CASA C-101 Aviojet F-4E Kurnass 2000 F-5E/F Tiger-II McDonnell Douglas F-15 Eagle General Dynamics F-16 Fighting Falcon Dassault Mirage III Dassault Mirage 5 Dassault Mirage 2000 Eurofighter Typhoon IAI Nesher/Dagger/Finder IAI Kfir HAL Tejas KAI T-50 Golden Eagle Leonardo M-346FA Master Saab JAS 39 Gripen Sukhoi Su-30MKI Su-25KM Scorpion[source] |
| Used by | Israel Defense Forces[source] | See operators[source] |
|---|
| Propulsion | Single stage solid-propellant rocket motor[source] | — |
|---|
| Warhead | High-explosive anti-tank (HEAT), fragmentation high explosive (HE), thermobaric , or anti-personnel[source] | 11 kg (24 lb 4 oz)[source] |
|---|
| Country of origin | Israel[source]Inventory Origin column; table 4, row 5, cell 2; revision 1349150138; retrieved 2026-09-30 | — |
|---|
| Place of origin | — | Israel[source] |
|---|
| Wars | — | Yom Kippur War Falklands War 1982 Lebanon War 2006 Lebanon War[source] |
|---|
| Unit cost | — | Shafrir series: Shafrir-1: US$20,000[source] |
|---|
| Produced | — | Shafrir series: 1961–1983 Python series: 1980–present[source] |
|---|
| Detonation mechanism | — | proximity[source] |
|---|
| Engine | — | solid fuel rocket motor[source] |
|---|
| Flight altitude | — | N/A[source] |
|---|
| Guidance system | — | infrared homing + 320×240 pixel dual waveband electro-optical imaging seeker, lock on after launch, with infrared counter-counter-measures (IRCCM)[source] |
|---|
| Reported operators |
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