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gptkbp:instanceOf
|
cruise missile
|
|
gptkbp:developedBy
|
gptkb:India
gptkb:Russia
|
|
gptkbp:diameter
|
0.6 m
|
|
gptkbp:engineType
|
solid fuel
liquid fuel
|
|
gptkbp:exportedTo
|
gptkb:Brazil
gptkb:India
gptkb:Philippines
gptkb:Russia
gptkb:UAE
|
|
gptkbp:firstFlight
|
successful
|
|
gptkbp:firstIntroduced
|
2001
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|
gptkbp:futurePlans
|
BrahMos-NG
hypersonic variant
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
BrahMos missile system
|
|
gptkbp:launched
|
vertical launch
horizontal launch
inclined launch
|
|
gptkbp:launchSite
|
air
land
sea
|
|
gptkbp:length
|
8.4 m
|
|
gptkbp:maxTakeoffWeight
|
3,000 kg
|
|
gptkbp:militaryRank
|
anti-ship
land-attack
submarine-launched
air-to-surface
surface-to-surface
|
|
gptkbp:offers
|
3 million USD
|
|
gptkbp:operationalStatus
|
in service
|
|
gptkbp:pairing
|
BrahMos Aerospace
|
|
gptkbp:productionCompany
|
1998
|
|
gptkbp:provides
|
active radar homing
inertial navigation
|
|
gptkbp:range
|
290 km
|
|
gptkbp:security
|
high speed
maneuverability
low radar cross-section
|
|
gptkbp:speed
|
gptkb:Mach_2.8
|
|
gptkbp:successor
|
BrahMos-II
|
|
gptkbp:type
|
200 kg
conventional
supersonic
|
|
gptkbp:userCountries
|
gptkb:Brazil
gptkb:India
gptkb:Philippines
gptkb:Russia
gptkb:UAE
|
|
gptkbp:wingspan
|
3 m
|