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gptkbp:instanceOf
|
missile
|
|
gptkbp:component
|
integrated with command systems
|
|
gptkbp:country
|
gptkb:Soviet_Union
|
|
gptkbp:deployedTo
|
Eastern_Bloc_countries
|
|
gptkbp:design
|
gptkb:Moscow_Institute_of_Thermal_Technology
modular design
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:engineType
|
liquid rocket engine
|
|
gptkbp:exportedTo
|
some_Eastern_Bloc_countries
|
|
gptkbp:firstDeployment
|
1958
|
|
gptkbp:firstFlight
|
1955
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
M-17
|
|
gptkbp:launched
|
vertical launch
manual and automated
|
|
gptkbp:launchSite
|
mobile ground launcher
fixed and mobile
|
|
gptkbp:launchVehicle
|
ground vehicle
|
|
gptkbp:legacy
|
influenced future missile designs
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Moscow_Institute_of_Thermal_Technology
|
|
gptkbp:maxTakeoffWeight
|
3,000 kg
|
|
gptkbp:operationalRange
|
50 km
|
|
gptkbp:operationalRole
|
air defense
|
|
gptkbp:operationalStatus
|
obsolete
|
|
gptkbp:productionCompany
|
1950s
1953
|
|
gptkbp:propulsion
|
liquid-fueled rocket engine
|
|
gptkbp:provides
|
active radar homing
inertial navigation system
|
|
gptkbp:range
|
up to 100 km
|
|
gptkbp:relatedPatent
|
gptkb:M-15
|
|
gptkbp:releaseYear
|
1958
|
|
gptkbp:resources
|
semi-active radar homing
|
|
gptkbp:retirementYear
|
1990s
advancements in missile technology
|
|
gptkbp:security
|
limited
|
|
gptkbp:services
|
gptkb:Soviet_Union
|
|
gptkbp:speed
|
Mach_2.5
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:S-300
gptkb:S-300_series
|
|
gptkbp:supportRole
|
limited
|
|
gptkbp:targets
|
ground-based radar
aircraft and missiles
|
|
gptkbp:technology
|
gptkb:S-75_Dvina
|
|
gptkbp:training
|
used for training purposes
M-17T
|
|
gptkbp:type
|
high-explosive
surface-to-air missile
nuclear or conventional
|
|
gptkbp:weight
|
2,500 kg
|
|
gptkbp:wingspan
|
3.5 m
|
|
gptkbp:yearEstablished
|
1957
|