What engine did the F 105 A. C. have and what was the thrust rating,full afterburner?
2007-01-07 08:41:19 · 3 answers · asked by section hand 6 in Cars & Transportation ➔ Aircraft
The YF-105A prototype first flew on 22 October 1955, with the second YF-105A following on 28 January 1956.[2] In spite of being powered by a less potent J57-P-25 engine with 15,000 pound-force (66.7 kN) of afterburning thrust (the J75 was expected to generate 24,500 pound-force (109.0 kN) with the afterburner), the first prototype attained the speed of Mach 1.2 on its maiden flight.
Production engine: Powerplant: 1× Pratt & Whitney J75-P-19W afterburning turbojet, 26,500 lbf (118 kN) with afterburning and water injection
2007-01-07 10:51:49 · answer #1 · answered by Anonymous · 1⤊ 0⤋
Mechanics may know the answer, but any Thud (F-105) driver can tell you. Readdress your question.
2007-01-07 09:51:48 · answer #2 · answered by RANDLE W 4 · 1⤊ 1⤋
http://www.globalaircraft.org/planes/f-105_thunderchief.pl
2007-01-07 15:54:27 · answer #3 · answered by eferrell01 7 · 0⤊ 0⤋