|
gptkbp:instanceOf
|
gptkb:surface-to-air_missile
|
|
gptkbp:controls
|
gptkb:SAGE_system
|
|
gptkbp:countryOfOrigin
|
gptkb:United_States
|
|
gptkbp:deployment
|
BOMARC Missile Sites
|
|
gptkbp:designation
|
CIM-10 (from 1962)
IM-99 (initial)
|
|
gptkbp:diameter
|
0.45 m
|
|
gptkbp:engine
|
solid-fuel rocket booster
Marquardt ramjet
|
|
gptkbp:guidanceSystem
|
semi-active radar homing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CIM-10 Bomarc
|
|
gptkbp:introduced
|
1957
|
|
gptkbp:length
|
13.7 m
|
|
gptkbp:manufacturer
|
gptkb:Boeing
gptkb:Michigan_Aerospace_Research_Center
|
|
gptkbp:notableEvent
|
first long-range anti-aircraft missile in the world
|
|
gptkbp:numberBuilt
|
over 500
|
|
gptkbp:primaryUse
|
air defense
|
|
gptkbp:range
|
400 km
|
|
gptkbp:retired
|
1972
|
|
gptkbp:speed
|
Mach 2.8
|
|
gptkbp:testFlights
|
1952
|
|
gptkbp:usedBy
|
gptkb:United_States_Air_Force
gptkb:Royal_Canadian_Air_Force
|
|
gptkbp:warheadType
|
gptkb:W40_nuclear_warhead
conventional high-explosive warhead
|
|
gptkbp:weight
|
7,000 kg
|
|
gptkbp:wingspan
|
5.5 m
|
|
gptkbp:bfsParent
|
gptkb:USAF_Bomarc_missile_program
|
|
gptkbp:bfsLayer
|
7
|