Convair F-102 A Delta Dagger , '61006' 431st Test and Evaluation Sqn. USAF , Zaragoza Air Base Spain 1962.Hobby Master HA3105.
Convair F-102 A Delta Dagger , '61006' 431st Test and Evaluation Sqn. USAF , Zaragoza Air Base Spain 1962.Hobby Master HA3105.
Convair F-102 A Delta Dagger , '61006' 431st Test and Evaluation Sqn. USAF , Zaragoza Air Base Spain 1962.Hobby Master HA3105.

Hobby Master – Convair F-102 A Delta Dagger , ‘61006’ 431st Test and Evaluation Sqn. USAF , Zaragoza Air Base Spain 1962

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                      Convair F-102 Delta Dagger

Convair F-102 Delta Dagger byl americký přepadový stíhací letoun, určený pro každé počasí. Vyvinut byl z pokusného letounu XF-92. Letoun byl navržen tak, aby výkonnostně překonal tehdejší sovětské bombardéry, ale vývoj motoru Wright J67 a avioniky se opozdil a tak vznikl provizorní letoun, který však ve vodorovném letu nebyl schopen překonat nadzvukovou rychlost. Stroj musel být přepracován a dostal nové motory Pratt & Whitney J57.

The Convair F-102 Delta Dagger was an American interceptor aircraft that was built as part of the backbone of the United States Air Force’s air defenses in the late 1950s. Entering service in 1956, its main purpose was to intercept invading Soviet strategic bomber fleets (primarily the Tupolev Tu-95) during the Cold War. Designed and manufactured by Convair, 1,000 F-102s were built.

Role Interceptor aircraft
Manufacturer Convair
First flight 24 October 1953
Introduction April 1956
Retired 1979
Primary users United States Air Force
Greece
Turkey
Number built 1,000
Unit cost
US$1.2 million
Developed from Convair XF-92
Developed into F-106 Delta Dart

General characteristics

  • Crew: 1
  • Length: 68 ft 4 in (20.83 m)
  • Wingspan: 38 ft 1 in (11.61 m)
  • Height: 21 ft 2 in (6.45 m)
  • Wing area: 661.5ft2/61.52m2 (Original Wing) or 695 ft2/64.57m2 (Conically-Cambered Wing) ()
  • Airfoil: NACA 0004-65 mod root and tip
  • Empty weight: 19,350 lb (8,777 kg)
  • Loaded weight: 24,500 lb (11,100 kg)
  • Max. takeoff weight: 31,500 lb (14,300 kg)
  • Internal fuel capacity: 1,085 U.S. gal (4,107 l)
  • External fuel capacity: 2 × 215 U.S. gal (815 l) drop tanks
  • Powerplant: 1 × Pratt & Whitney J57-P-25 afterburning turbojet
    • Dry thrust: 11,700 lbf (52.0 kN)
    • Thrust with afterburner: 17,200 lbf (76.5 kN)
United States Air Force
Founded 1 August 1907
(112 years)
18 September 1947
(71 years, 11 months) (as independent service)
Country United States of America
Type Air and space force
Role Air, space, and cyberspace warfare
Size 321,444 active duty airmen
141,880 civilians
69,200 reserve airmen
105,700 air national guard airmen
5,047 manned aircraft
406 ICBMs
170 satellites
Insignia
Flag
Seal of the Department of the Air Force
Roundel
USAF “Hap” Arnold Symbol
Symbol
Aircraft flown
Attack A-10, AC-130, MQ-9
Bomber B-1B, B-2, B-52H
Electronic
warfare		 E-2 , E-3, E-4, E-8, EA-18 ,  EC-130 , E-767
Fighter F-14 , F-15C, F-15E, F-16, F/A-18 , F-22, F-35A
Helicopter HH-60, UH-1N
Reconnaissance MC-12, RC-135, RQ-4, RQ-170, U-2, U-28
Trainer T-1, T-6, T-38, T-41, T-51, T-53, TG-16
Transport C-5M, C-12, C-17, C-21, C-32, C-37, C-130, C-40, CV-22, VC-25
Tanker KC-10, KC-135, KC-46

The 431st Test and Evaluation Squadron is an inactive United States Air Force unit. Its last assignment was with the Tactical Air Command 57th Fighter Wing stationed at Nellis Air Force Base, Nevada. It was inactivated on 30 June 1992.

431st Test and Evaluation Squadron

Emblem of the 431st Test and Evaluation Squadron
Active 1943–1992
Country United States
Branch United States Air Force
Type Test and Evaluation

 

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