| Aircraft Maintenance |
|
| | |
| TWS Ribbon Bar |
|
|
| Service Photo |
Service Details |
|
|
|
|
|
What are you doing now:
Not Specified
|
| |
Other Comments:
Not Specified
|
| |
|
|
|
From Year
2003 |
To Year
2003 |
| |
Image
|
|
|
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
|
| |
|
