|
gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
|
gptkbp:ceiling
|
21,000 m
|
|
gptkbp:controls
|
radar command guidance
|
|
gptkbp:designation
|
MIM-3
|
|
gptkbp:developedBy
|
gptkb:Project_Nike
|
|
gptkbp:diameter
|
30 cm
|
|
gptkbp:engine
|
solid-fuel booster and liquid-fuel sustainer
|
|
gptkbp:guidanceSystem
|
command guidance
|
|
gptkbp:introduced
|
1954
|
|
gptkbp:length
|
9.96 m
|
|
gptkbp:manufacturer
|
gptkb:Western_Electric
|
|
gptkbp:namedAfter
|
gptkb:Nike_(Greek_goddess_of_victory)
|
|
gptkbp:notableFor
|
first operational guided surface-to-air missile in the US
|
|
gptkbp:originalName
|
Nike I
|
|
gptkbp:platform
|
fixed ground-based launcher
|
|
gptkbp:primaryUser
|
gptkb:Greece
gptkb:Italy
gptkb:Japan
gptkb:Taiwan
gptkb:Turkey
gptkb:United_States
gptkb:West_Germany
|
|
gptkbp:range
|
48 km
|
|
gptkbp:retired
|
1974
|
|
gptkbp:speed
|
Mach 2.3
|
|
gptkbp:successor
|
gptkb:MIM-14_Nike_Hercules
|
|
gptkbp:usedBy
|
gptkb:United_States_Army
|
|
gptkbp:usedIn
|
gptkb:Cold_War
|
|
gptkbp:warheadType
|
high-explosive
122 kg
|
|
gptkbp:weight
|
1,000 kg
|
|
gptkbp:bfsParent
|
gptkb:MIM-14_Nike_Hercules_missile
|
|
gptkbp:bfsLayer
|
7
|
|
http://www.w3.org/2000/01/rdf-schema#label
|
MIM-3 Nike Ajax
|