Editing Lockheed XF-90 (section)

==Specifications (XF-90A)==
[[File:Lockheed XF-90 3-view line drawing.png|frameless|right|3-view line drawing of the Lockheed XF-90]]

{{Aircraft specs
|prime units?=imp
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|crew=one
|length ft=56
|length in=2
|length m=17.12 
|span ft=40
|span in=0
|span m=12.20 
|height ft=15
|height in=9
|height m=4.80 
|wing area sqft=345 
|wing area sqm=32 
|empty weight lb=18,050 
|empty weight kg=8,204 
|gross weight lb=27,200 
|gross weight kg=12,363 
|max takeoff weight lb=31,060 
|max takeoff weight kg=14,118 
|eng1 name=[[Westinghouse J34]]-WE-15 
|eng1 type=[[turbojet]]s
|eng1 number=2
|eng1 lbf=4,100  
|eng1 kn=18.2 
|max speed mph=665 
|max speed kmh=1,064 
|range miles=2,300 
|range km=3,680 
|ceiling ft=39,000 
|ceiling m=11,890 
|climb rate ftmin=5,555 
|climb rate ms=28.2 
|wing loading lb/sqft=79 
|wing loading kg/m2=386 
|thrust/weight=0.30
|armament=
* 6 × 20 mm (.79 in) cannons
* 8 × 5 in (127 mm) [[HVAR]] rockets
* Up to 2,000 lb (907 kg) of bombs
}}