This Military Service Page was created/owned by
AB Raymond Guinn
to remember
Babcock, Leon W., Jr., Maj Gen USAF(Ret).
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Aircraft/Missile Information
Convair F-102A Delta Dagger Length 68.37 ft | 20.84 m Width 38.12 ft | 11.62 m Height 21.19 ft | 6.46 m Engine(s) 1 x Pratt & Whitney J57-P-25 turbojet engine delivering 17,200 lbs of thrust. Empty Weight 19,026 lbs | 8,630 kg MTOW 31,500 lbs | 14,288 kg Max Speed 825 mph | 1,328 km/h | 717 kts Max Range 1,350 miles | 2,173 km Ceiling 54,003 ft | 16,460 m | 10.2 miles Climb Rate 17,400 ft/min (5,304 m/min) Hardpoints 6 Armament 6 x air-to-air missiles 24 x 2.75in unguided rockets (pod x2)
Nuclear Capable Accommodations 1
Major Variants
? XF-92A - Experimental Test Study Aircraft from which the YF-102 is derived from. ? YF-102 - Prototype Model Designation (Model 8-80); fitted with 9,700lb Pratt & Whitney J57-P-11 turbojet engine. ? YF-102A - Redesigned "Whitcomb Area Ruled" airframe. ? F-102A - Initial Production Model Designation ? TF-102A - Tandem Seat Trainer Conversion Models ? F-102B - Improved Development on base F-102; redesignated and produced as the F-106 Delta Dart. ? YF-106A - F-106 Prototype Model Designation of which two were produced. ? F-106A - Single Seat Model Designation ? F-106B - Two-Seat Model Designation
