tiers | |
---|
categories | "WEG" |
"Air Defense" |
"Man-Portable Air-Defense Systems (MANPADS)" |
"United States" |
"PRO_Bangladesh" |
"PRO_Bosnia and Herzegovina" |
"PRO_Chad" |
"PRO_Chile" |
"PRO_Colombia" |
"PRO_Egypt" |
"PRO_Finland" |
"PRO_Georgia" |
"PRO_Germany" |
"PRO_Greece" |
"PRO_India" |
"PRO_Iran (Islamic Republic of)" |
"PRO_Iraq" |
"PRO_Israel" |
"PRO_Japan" |
"PRO_Lithuania" |
"PRO_Morocco" |
"PRO_Netherlands" |
"PRO_North Korea (Democratic People's Republic of Korea)" |
"PRO_Norway" |
"PRO_Pakistan" |
"PRO_Portugal" |
"PRO_Slovenia" |
"PRO_South Korea (Republic of Korea)" |
"PRO_Switzerland" |
"PRO_Turkey" |
"PRO_United Kingdom of Great Britain and Northern Ireland" |
"PRO_United States of America" |
"Air" |
"Tier3" |
|
---|
notes | "The FIM-92 Stinger is a Man-Portable Air-Defense System (MANPADS) that operates as an infrared homing surface-to-air missile (SAM). It can be adapted to fire from a wide variety of ground vehicles and helicopters (as an AAM). Developed in the United States, it entered service in 1981 and is used by the militaries of the United States and 29 other countries. It is principally manufactured by Raytheon Missile Systems and is produced under license by EADS in Germany and by Roketsan in Turkey, with 70,000 missiles produced." |
---|
dateOfIntroduction | 1981 |
---|
countryOfOrigin | "United States" |
---|
proliferation | "Bangladesh, Bosnia and Herzegovina, Chad, Chile, Colombia, Egypt, Finland, Georgia, Germany, Greece, India, Iran (Islamic Republic of), Iraq, Israel, Japan, Lithuania, Morocco, Netherlands, North Korea (Democratic People's Republic of Korea), Norway, Pakistan, Portugal, Slovenia, South Korea (Republic of Korea), Switzerland, Turkey, United Kingdom of Great Britain and Northern Ireland, United States of America" |
---|
selectedregions | |
---|
checkedregions | |
---|
checkedcountries | "Bangladesh" |
"Bosnia and Herzegovina" |
"Chad" |
"Chile" |
"Colombia" |
"Egypt" |
"Finland" |
"Georgia" |
"Germany" |
"Greece" |
"India" |
"Iran (Islamic Republic of)" |
"Iraq" |
"Israel" |
"Japan" |
"Lithuania" |
"Morocco" |
"Netherlands" |
"North Korea (Democratic People's Republic of Korea)" |
"Norway" |
"Pakistan" |
"Portugal" |
"Slovenia" |
"South Korea (Republic of Korea)" |
"Switzerland" |
"Turkey" |
"United Kingdom of Great Britain and Northern Ireland" |
"United States of America" |
|
---|
dis | name | "US STINGER" |
---|
string | "03.01.225.001.007.001.000" |
---|
|
---|
images | "Stinger_(A).png" |
"Stinger_(B).jpg" |
"Stinger_(C).jpg" |
|
---|
sections | name | "System" |
---|
properties | name | "Alternative Designation" |
---|
value | "FIM-92; FIM-92A Basic Stinger" |
---|
|
name | "System" |
---|
value | "Grip-stock (with battery coolant unit, IFF, impulse generator, and seeker redesign), missile, night sight, radio and other acquisition aides" |
---|
|
name | "In Service" |
---|
value | "1981-Present" |
---|
|
name | "Crew " |
---|
value | "1, Normally 2 with a loader" |
---|
|
|
---|
|
name | "Armament" |
---|
sections | name | "Weapon 1" |
---|
properties | |
name | "Length " |
---|
value | "1.52 m + launch tube" |
---|
|
name | "Diameter " |
---|
value | "INA" |
---|
|
name | "Fire on Move" |
---|
value | "Yes, in short halt" |
---|
|
name | "Reaction Time " |
---|
value | "6 seconds tracking and missile activation (3-5 cooling)" |
---|
|
name | "Reload Time " |
---|
value | "less than 10 seconds" |
---|
|
name | "System Weight" |
---|
value | "15.2 kg launch-ready, 2.6 kg belt-pack IFF" |
---|
|
name | "Time between Launches " |
---|
value | "INA" |
---|
|
|
---|
|
|
---|
|
name | "Munition" |
---|
sections | name | "Munition 1" |
---|
properties | name | "Altitude, Maximum " |
---|
value | "3500" |
---|
units | "m" |
---|
|
name | "Combat Load, Dismount " |
---|
value | "2.0" |
---|
units | "rds" |
---|
|
name | "Combat Load, from AD vehicle " |
---|
value | "5.0" |
---|
units | "rds" |
---|
|
name | "Combat Load, one" |
---|
value | "1.0" |
---|
|
name | "Diameter " |
---|
value | "70.0" |
---|
units | "mm" |
---|
|
name | "Fuze Type" |
---|
value | "Contact with time delay" |
---|
|
name | "Guidance" |
---|
value | "Cooled 2nd gen passive IR homing (4.1-4.4 mm)" |
---|
|
name | "Length " |
---|
value | "1.52" |
---|
units | "mm" |
---|
|
|
name | "Probability of Hit" |
---|
value | "INA" |
---|
units | "PCT" |
---|
|
name | "Propulsion" |
---|
value | "Solid fuel, dual-thrust (ejector motor and sustainer motor)" |
---|
|
name | "Range, Maximum " |
---|
value | "4,000+" |
---|
units | "m" |
---|
|
name | "Range, Minimum " |
---|
value | "200.0" |
---|
units | "m" |
---|
|
name | "Seeker Field of View " |
---|
value | "INA" |
---|
|
name | "Self-Destruct Time" |
---|
value | "20.0" |
---|
units | "sec" |
---|
|
name | "Speed " |
---|
value | "745 m/s, Mach 2.2" |
---|
|
name | "Target Maneuver Limit" |
---|
value | "Up to 8 g" |
---|
|
name | "Tracking Rate" |
---|
value | "INA" |
---|
|
|
|
name | "Weight " |
---|
value | "1.0" |
---|
units | "kg" |
---|
|
name | "Weight " |
---|
value | "10.0" |
---|
units | "kg" |
---|
|
|
---|
|
|
---|
|
name | "Fire Control System" |
---|
sections | name | "Day Sight" |
---|
properties | name | "Acquisition Range " |
---|
value | "4000+" |
---|
units | "km" |
---|
|
name | "Field of View " |
---|
value | "INA" |
---|
|
name | "Field of View " |
---|
value | "INA" |
---|
|
name | "Type" |
---|
value | "Ring and bead, most launchers Optical sight with lead bias available." |
---|
|
|
---|
|
name | "Night Sight" |
---|
properties | name | "Type" |
---|
value | "Optional AN/PAS-18, Wide- Angle Stinger Pointer System (WASP) thermal sight." |
---|
|
|
---|
|
name | "Night Sights" |
---|
properties | name | "Acquisition Range " |
---|
value | "20-30 km side or tail aspect, 10 km head-on aspect" |
---|
|
name | "Field of View " |
---|
value | "20 deg x 12 deg" |
---|
|
|
---|
|
name | "Radar" |
---|
properties | name | "Radar Equipment" |
---|
value | "Providing Omni-directional
Reporting of Targets at Extended Ranges (REPORTER), German/Dutch EW system with I/J band radar and IFF. Range: 40 km.
Altitude: 15-4000 m.
" |
---|
|
name | "Radar Other" |
---|
value | "Several U.S. and foreign radars are available for use with
Stinger." |
---|
|
|
---|
|
|
---|
properties | name | "ADAD" |
---|
value | "British passive thermal IR scanners on remote tripod or vehicle mount with 240 o FOV automatic cueing system." |
---|
|
name | "IFF" |
---|
value | "AN/PPX-1 trigger-activated on grip-stock, with battery belt-pack" |
---|
|
name | "Target Alert Display Set (TADDS)" |
---|
value | "US portable graphic display set w/audio alert, VHF radio, and IFF." |
---|
|
|
---|
|
|
---|
variants | name | "The MANPADS has been adapted for launch from APC or IFV chassis. It has also been adapted for light utility vehicles and combat support vehicles, such as the German Wiesel-based Fliegerfaust-2 (FLF-2). A variety of air defense launcher systems can use Stinger, Mistral, or other MANPADS." |
---|
notes | "" |
---|
|
name | "FIM-92A" |
---|
notes | "Stinger Basic: The basic model." |
---|
|
name | "FIM-92B" |
---|
notes | "Stinger POST: In this version, the infrared seeker head was replaced by a combined IR/UV seeker that utilized rosette scanning. This resulted in achieving significantly higher resistance to enemy countermeasures (flares) and natural disturbances. Production ran from 1981 to 1987; a total of 600 missiles were produced.[" |
---|
|
name | "FIM-92C" |
---|
notes | "Stinger RMP: The resistance to interference was increased again by adding more powerful digital computer components. Moreover, the software of the missile could now be reconfigured in a short time in order to respond quickly and efficiently to new types of countermeasures. Until 1991, some 20,000 units were produced for the U.S. Army alone." |
---|
|
name | "FIM-92D" |
---|
notes | "Various modifications were continued with this version in order to increase the resistance to interference." |
---|
|
name | "FIM-92E" |
---|
notes | "Stinger—RMP Block I: By adding a new rollover sensor and revised control software, the flight behavior was significantly improved. Additionally, the performance against small targets such as drones, cruise missiles and light reconnaissance helicopters was improved. The first deliveries began in 1995. Almost the entire stock of U.S. Stinger missiles was replaced by this version." |
---|
|
name | "FIM-92F" |
---|
notes | "A further improvement of the E version and the current production version." |
---|
|
name | "FIM-92G" |
---|
notes | "An unspecified upgrade for the D variant.[" |
---|
|
name | "FIM-92H" |
---|
notes | "Indicates a D variant that has been upgraded to the E standard." |
---|
|
name | "Stinger—RMP Block II" |
---|
notes | "This variant was a planned developed based on the E version. The improvements included an imaging infrared seeker head from the AIM-9X. With this modification, the detection distance and the resistance to jamming was to be greatly increased. Changes to the airframe would furthermore enable a significant increase in range. Although the missile reached the testing phase, the program was dropped in 2002 for budgetary reasons." |
---|
|
name | "FIM-92J" |
---|
notes | "Block 1 missile upgrade to replace aging components to extend service life an additional 10 years. Upgrades include a proximity fuse warhead section, equipped with a target detection device to increase effectiveness against unmanned aerial vehicles." |
---|
|
name | "FIM-92K" |
---|
notes | "variant of FIM-92J designed to use a vehicle datalink rather than the missile's own seeker for targeting." |
---|
|
|
---|
type | "WEG" |
---|
version | 1 |
---|