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gptkbp:instanceOf
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gptkb:aircraft
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|
gptkbp:armament
|
gptkb:GAU-12/U_25mm_rotary_cannon
Hardpoints for external stores
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|
gptkbp:countryOfOrigin
|
gptkb:United_States
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gptkbp:crew
|
1
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gptkbp:designer
|
gptkb:Burt_Rutan
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gptkbp:displayedAt
|
gptkb:Mojave_Air_and_Space_Port
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|
gptkbp:emptyWeight
|
1,134 kg
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|
gptkbp:engineThrust
|
2,200 lbf
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|
gptkbp:engineType
|
gptkb:Pratt_&_Whitney_Canada_JT15D-1_turbofan
|
|
gptkbp:firstFlight
|
1986
|
|
gptkbp:height
|
2.44 m
|
|
gptkbp:length
|
9.14 m
|
|
gptkbp:manufacturer
|
gptkb:Scaled_Composites
|
|
gptkbp:maximumSpeed
|
482 knots
|
|
gptkbp:maxTakeoffWeight
|
2,041 kg
|
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gptkbp:nameMeaning
|
Agile Responsive Effective Support
|
|
gptkbp:nickname
|
gptkb:ARES
|
|
gptkbp:notableFeature
|
Asymmetric design for cannon recoil compensation
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gptkbp:numberBuilt
|
1
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gptkbp:primaryUser
|
gptkb:Scaled_Composites
|
|
gptkbp:purpose
|
Designed as a low-cost alternative to the A-10 Thunderbolt II
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|
gptkbp:range
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1,200 nmi
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gptkbp:role
|
Observation aircraft
Light attack aircraft
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|
gptkbp:serviceCeiling
|
12,200 m
|
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gptkbp:status
|
gptkb:Prototype
|
|
gptkbp:wingspan
|
7.32 m
|
|
gptkbp:bfsParent
|
gptkb:Burt_Rutan
|
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gptkbp:bfsLayer
|
6
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|
https://www.w3.org/2000/01/rdf-schema#label
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Rutan Model 151 ARES
|