page_title: Pratt & Whitney TF30
section_title: Variants
hierarchical_section_title: Pratt & Whitney TF30 / Variants
caption_attribution_description: at Ailes Anciennes Armorique Vannes airport
context_page_description: The Pratt & Whitney TF30 is a military low-bypass turbofan engine originally designed by Pratt & Whitney for the subsonic F6D Missileer fleet defense fighter, but this project was cancelled. It was later adapted with an afterburner for supersonic designs, and in this form it was the world's first production afterburning turbofan, going on to power the F-111 and the F-14A Tomcat, as well as being used in early versions of the A-7 Corsair II without an afterburner. First flight of the TF30 was in 1964 and production continued until 1986.
context_section_description: XTF30-P-1
  8,250 lbf (36.70 kN) thrust.
  YTF30-P-1
  TF30-P-1
  8,500 lbf (37.81 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.
  TF30-P-1A
  Similar to -1 with a fuel filter-heater instead of a fuel filter, initially powered first two prototype F-111B.
  TF30-P-2
  10,200 lbf (45.37 kN) thrust, intended to power the F6D Missileer.
  TF30-P-3
  8,500 lbf (37.81 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.
  TF30-P-5
  TF30-P-6
  11,350 lbf (50.49 kN) thrust, powered the A-7A.
  TF30-P-6A
  TF30-P-6C
  TF30-P-6E
  TF30-P-7
  12,350 lbf (54.94 kN) thrust, 20,350 lbf (90.52 kN) with afterburner.
  TF30-P-8
  12,200 lbf (54.27 kN) thrust, initially powered the A-7B/C.
  TF30-P-9
  12,000 lbf (53.38 kN) thrust, 19,600 lbf (87.19 kN) with afterburner.
  TF30-P-12
  10,750 lbf (47.82 kN) thrust, 20,250 lbf (90.08 kN) with afterburner, powered the two pre-production F-111B.
  TF30-P-12A
  Similar to -12 with a fuel filter instead of a fuel filter-heater and deactivated wave-off feature, powered early production FB-111A.
  TF30-P-14
  TF30-P-16
  TF30-P-18
  YTF30-P-100
  TF30-P-100
  Redesigned engine, 14,560 lbf (64.77 kN) thrust, 25,100 lbf (111.65 kN) with afterburner, powered the F-111F.
  TF30-P-103
  Redesignated -3 upgraded with -100 components under the Pacer 30 program, 9,800 lbf (43.59 kN) thrust, 18,500 lbf (82.29 kN) with afterburner.
  TF30-P-107
  Redesignated -7 upgraded with -100 components under the Pacer 30 program, 10,800 lbf (48.04 kN) thrust, 20,350 lbf (90.52 kN) with afterburner.
  TF30-P-108
  Hybrid of -107 aft section and -109 fore section.
  TF30-P-108RA
  Redesignated -108 when in RAAF service, powered the F-111G.
  TF30-P-109
  Redesignated -9 upgraded with -100 components under the Pacer 30 program, 20,840 lbf (92.70 kN) thrust with afterburner.
  TF30-P-109RA
  Redesignated -109 when in RAAF service, powered the F-111C.
  TF30-P-408
  Similar to -8, 13,390 lbf (59.56 kN) thrust, powered the A-7B/C.
  TF30-P-412
  Similar to -12
  TF30-P-412A
  Similar to -12A, 10,800 lbf (48.04 kN) thrust, 20,900 lbf (92.97 kN) with afterburner, powered early production F-14A.
  TF30-P-414A
  Similar to -412A, powered later production F-14A.
  JTF10A
  Company designation for the TF30 family of engines
  JTF10A-1
  (XTF30-P-1) Intended to power the Douglas Model 2067.
  JTF10A-6
  Intended to power the Douglas Model 2086.
  JTF10A-7
  (TF30-P-2)
  JTF10A-8
  (TF30-P-6)
  JTF10A-9
  (TF30-P-8)
  JTF10A-10
  JTF10A-15
  (TF30-P-18)
  JTF10A-16
  (TF30-P-408)
  JTF10A-20
  (TF30-P-1)
  JTF10A-21
  (TF30-P-3)
  JTF10A-27A
  (TF30-P-12)
  JTF10A-27B
  (TF30-P-12A)
  JTF10A-27D
  (TF30-P-7)
  JTF10A-27F
  (TF30-P-412)
  JTF10A-32C
  (TF30-P-100)
  JTF10A-36
  (TF30-P-9)
  Pratt & Whitney/SNECMA TF104
  Subsonic TF30 derivative modified by SNECMA, installed in Mirage IIIT and Mirage IIIV-01.
  Pratt & Whitney/SNECMA TF106
  A derivative of the TF30 to power the Dassault Mirage IIIV VTOL fighter.
  Pratt & Whitney/SNECMA TF306C
  A derivative of the TF30 tested in the Dassault Mirage F2.
  Pratt & Whitney/SNECMA TF306E
caption: Pratt & Whitney/SNECMA TF106
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