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Lockheed P-2 Neptune specs
Country: United States of America
ICAO Type designator:P2
First flight:17 May 1945
Production ended: 1962
Production total:1036
Series: Neptune MR.1: British designation of P2V-5
OP-2E: Fitted with terrain avoidance radar in nose, chaff dispensers, wing mounted gun pods and waist guns.
P2V-2: Initial production version with extended nose instead of turret
P2V-2N: P2V-2 modified for polar exploration with ski landing gear and provision for JATO rockets
P2V-3: P2V-2 with improved engines
P2V-4: Fitted with R-3350 turbo-compound engines and wingtip tanks
P2V-5: Export version
P2V-6: Reduced capability radar, improved defensive armament
P2V-7: J-34 jet engine wingtip pods, new cockpit, MAD tail boom
RB-69A: USAF Variant
SP-2E: New designation of previous P2V-series without defensive guns
SP-2H: Redesignation of P2V-7B and P2V-7S models
XP2V-1: Prototype model
Propulsion:2 piston engines
Maximum number of passengers:
Maximum take-off mass:35240 kg
ICAO Mass group:4

Lockheed P-2 Neptune photo

Lockheed P-2 Neptune file photo (photo: Bidgee (CC:by-sa))

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