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At a glance
AIM-7 Sparrowlarger figure on 1 of 1
K-13 (missile)larger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Operational; AIM-7C
Single sourceOperational; AIM-7D
Single sourceOperational; AIM-7E/E2
Single sourceOperational; AIM-7F/M/P
Single sourceAIM-7C: 26 km (14 nmi) AIM-7D: 44 km (24 nmi) AIM-7E/E2: 50 km (27 nmi) AIM-7F/M/P: 70 km (38 nmi)[source]
Operational; Operational range
Single sourceR-3S / R-3R · effective
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | AIM-7 Sparrow | K-13 (missile) |
|---|---|---|
| Type | Medium-range, semi-active radar homing air-to-air missile[source] | Short-range infrared homing air-to-air missile[source] |
| Place of origin | United States[source] | Soviet Union[source] |
| In service | 1958–present[source] | 1961[source] |
| Used by | Australia, Canada, Egypt, Greece, Iran, Iraq, Israel, Italy, Japan, Jordan, Kuwait, Malaysia, Saudi Arabia, Singapore, South Korea, Spain, Taiwan, Turkey, United Kingdom, United States[source] | See Operators[source] |
| Wars | Vietnam War Iran–Iraq War Gulf War Russo-Ukrainian War[source] | — |
| Unit cost | $125,000[source] | — |
| Produced | AIM-7D: 1959 AIM-7F: 1976 AIM-7M: 1982[source] | — |
| No. built | >70,000[source] | — |
| Variants | Sparrow I: AIM-7A Sparrow II: AIM-7B Sparrow III: AIM-7C, AIM-7D, AIM-7E, AIM-7E2/ Skyflash / Aspide , AIM-7F, AIM-7M, AIM-7P, RIM-7M, AGM-45[source] | — |
| Warhead | High explosive blast-fragmentation AIM-7C/D/E: 65 pounds (29 kg) AIM-7F/M: 88 pounds (40 kg)[source] | 7.4 kg (16 lb)[source] |
| Engine | AIM-7A/B/C – Aerojet 1.8KS7800 solid rocket AIM-7D/E – Rocketdyne MK 38/MK 52 solid rocket AIM-7F/M/P – Hercules MK-58 solid-propellant rocket motor[source] | solid-fuel rocket engine[source] |
| Guidance system | semi-active radar homing[source] | infrared homing[source] |
| Launch platform | Aircraft: McDonnell Douglas F-4 Phantom II McDonnell Douglas F-15 Eagle McDonnell Douglas F-15E Strike Eagle General Dynamics F-16 Fighting Falcon Grumman F-14 Tomcat F/A-18 Hornet JA-37 Viggen F-104S Starfighter Tornado F.3 ADV F/A-18E/F Super Hornet Mitsubishi F-2[source] | MiG-21 , MiG-23 , MiG-19 , MiG-17 Sukhoi Su-17/20/22[source] |
| Manufacturer | Raytheon[source] | Vympel[source] |
| Guidance | — | (R-3S) infrared homing ; (R-3R) SARH[source] |
| Launch weight | — | (R-3S) 75 kg (166 lb); (R-3R) 93 kg (205 lb)[source] |
| Explosive content | — | 5.3 kg (11.68 lbs) of TGAF-5 (40% TNT, 40% RDX, 20% Aluminium powder)[source] |
| Fuze | — | type 428 proximity fuze and I-107 Contact fuze (R-3R)[source] |
| Former operator · Bulgaria | — | Bulgaria[source] |
| Former operator · Guinea | — | Guinea[source] |
| Reported operators |
|
|
R-3S / R-3R · max
Single source