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To: NoClones
the f/a-18 was the loser in a light-fighter competition back in the 70's wasn't it?

The Northrop YF-17 Shrike, forerunner of the Navy/Marine F/A-18 Hornet, didn't really lose the 'flyoff' against the General Dynamics F-16. The flight charactaristics were very close. The competition was a 'push'. The F-16 was 'chosen' because the F-16 used an engine (the GE F-100) that was common with the F-15 Eagle which was already in production. The USAF wasn't ready to add another engine to the supply chain. Logistical concerns tipped the scale in favor of the F-16 Falcon.

Besides, this was the LWF (Lightweight Fighter) project. Single-engine makes a bit more sense from a readiness standpoint. 'Course the Navy takes the view that 2 engines increase survivability.

33 posted on 03/24/2005 11:22:38 AM PST by Tallguy
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To: Tallguy
Didn't USAF Col. John Boyd himself make the push for the General Dynamics single-engine design over the YF-17 two-engine design...? Primarily because he wanted to commit the USAF to a design that constrained gold-plating and adding gadgeteer-unessentials/mission-creep to an air-defense-specific plane?

The YF-17 had more room for junk to be piled on...hence to be avoided...

37 posted on 03/24/2005 11:32:46 AM PST by Paul Ross ("Nothing that is morally wrong can be politically right." -William Gladstone)
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