Properties (54)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:spacecraft
|
| gptkbp:component |
varies by country
integrated with command and control systems radar, missile, launcher |
| gptkbp:deployedTo |
various military bases
ground-based |
| gptkbp:design |
by_Mikhail_Yangel
|
| gptkbp:developedBy |
gptkb:Soviet_Union
|
| gptkbp:diameter |
0.5 m
|
| gptkbp:electronic_warfare |
used in various conflicts
|
| gptkbp:engine |
solid-fuel rocket
|
| gptkbp:exportedTo |
Warsaw_Pact_countries
|
| gptkbp:firstIntroduced |
1961
|
| gptkbp:hasCapacity |
1961
|
| https://www.w3.org/2000/01/rdf-schema#label |
SA-3 Goa
|
| gptkbp:launchSite |
mobile launcher
vertical launch mobile and fixed |
| gptkbp:length |
8.5 m
|
| gptkbp:manufacturer |
gptkb:Moscow_Institute_of_Thermal_Technology
|
| gptkbp:maxTakeoffWeight |
2,500 kg
|
| gptkbp:militaryRank |
air defense forces
|
| gptkbp:missileSystem |
surface-to-air
|
| gptkbp:modifications |
various upgrades
|
| gptkbp:notableUsers |
Soviet_Union,_Egypt,_Syria
|
| gptkbp:operationalRange |
25 km
|
| gptkbp:operationalStatus |
active
ground-based air defense limited against low-flying targets |
| gptkbp:productionCompany |
1950s to 1960s
|
| gptkbp:provides |
semi-active
radar |
| gptkbp:range |
25 km
|
| gptkbp:resources |
semi-active radar homing
|
| gptkbp:retirementYear |
still in use
|
| gptkbp:services |
high
15,000 m |
| gptkbp:speed |
Mach_2.5
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:S-300
gptkb:S-300_family |
| gptkbp:supportRole |
air defense
proven in conflicts |
| gptkbp:targets |
aircraft
radar system |
| gptkbp:technology |
SA-2 Guideline
radar technology |
| gptkbp:training |
required for operators
extensive training needed |
| gptkbp:type |
high-explosive
missile system |
| gptkbp:updates |
ongoing improvements
|
| gptkbp:usedBy |
Various countries
|
| gptkbp:weight |
1,200 kg
|