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Lockheed XB-30
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==Specifications (as proposed)== {{Aircraft specs |prime units?=imp | ref= | crew=12 | length ft=104 | length in=8 | length m=31.91 | span ft=123 | span in=0 | span m=37.50 | height ft=23 | height in=9 | height m=7.25 | wing area sqft=1646 | wing area sqm=153 | empty weight lb=51616 | empty weight kg=23462 | gross weight lb=85844 | gross weight kg=39020 | max takeoff weight lb=93808 | max takeoff weight kg=42640 | eng1 number=4 | eng1 type=[[radial engine]]s | eng1 name=[[Wright R-3350 Duplex-Cyclone|Wright R-3350]]-13 | eng1 hp=2200 | eng1 kw=1600 | max speed mph=382 | max speed kmh=615 | range miles=5,333 | range km=8,045 | ceiling ft=17832 | ceiling m=5,440 | wing loading lb/sqft=52 | wing loading kg/m2=255 |power/mass=0.10 hp/lb (170 W/kg) | guns=<br /> ** 8Γ .50 in (12.7 mm) [[machine gun]]s in four fuselage turrets ** 2Γ .50 in (12.7 mm) machine guns ''and'' ** 1Γ [[20 mm caliber|20 mm]] [[autocannon|cannon]] in remotely aimed tail turret | bombs=16,000 lb }}
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