God Bless USA
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The Israeli Air Force (IAF) bought the F-16I with conformal fuel tanks. Why hasn't the USA used the conformal fuel tanks on there F-16's? Also can conformal fuel tanks be used on other fighter aircraft?
Conformal tanks cannot be jettisoned this is their biggest disadvantage. They give less drag than a normal fuel tank but they still give increased drag compared to a clean aircraft that has jettisoned its under wing tanks.The Israeli Air Force (IAF) bought the F-16I with conformal fuel tanks. Why hasn't the USA used the conformal fuel tanks on there F-16's? Also can conformal fuel tanks be used on other fighter aircraft?
The F-15E is the only other operational aircraft i can think of.Is there any current fighter aircraft other than the F-16I that has the conformal fuel tanks? If so where can see photos of it.
Israel? An original developer of the Hornet???Boeing is developing CFTs for the super hornet. Too bad that the original developers ie Israel never did CFTs for the hornet for the simple reason that it did not operate any.
I DID read it very carefully, several times in fact, hence my confusion!Read carefully pls.
Israel was the developer of CFTs. As they did not possess any F-18s, they did not develop CFTs for the F-18s. Hence, it is up to Boeing, as the original developer of the F-18s, to adapt the CFTs for the Hornet.
It seems to me that CFT's for the Hornet series would be desirable when it is in the tanker role, the more fuel it can carry the better.Then my apologies for the confusion and hopefully my subsequent post clears...
I believe the likely option is to position the hornet CFTs similar to the F-16.
I would even consider a design that covers the centre fuselage but I'm not sure if there are any electronics housed in that area. I'm no aeronautical engineer. I also believe there will be an added issue of how CFTs will affect carrier take-off/landings.
However, the business case for CFTs is appealing especially for earlier versions of the hornet. This is so for the RAAF where the extra range would be appreciated.
I think also there will some impetus to develop ejectable CFTs but that's merely speculation at this point.
IIRC the MiG 29M used a single CFT along the spine of the aircraft behind the cockpit. Perhaps this is the best place on the hornet familly?Then my apologies for the confusion and hopefully my subsequent post clears...
I believe the likely option is to position the hornet CFTs similar to the F-16.
I would even consider a design that covers the centre fuselage but I'm not sure if there are any electronics housed in that area. I'm no aeronautical engineer. I also believe there will be an added issue of how CFTs will affect carrier take-off/landings.
However, the business case for CFTs is appealing especially for earlier versions of the hornet. This is so for the RAAF where the extra range would be appreciated.
I think also there will some impetus to develop ejectable CFTs but that's merely speculation at this point.
This is conjecture but I would think they'd increase the RCS at the angles at which they're visible, yes. Just going by the additional bulky surfaces and so forth - if pylon carried payloads increase RCS I don't see why the CFTs wouldn't.Would the CFTs on the Block 50/52/60 F-16 increase the size of its RCS. It looks from pics that the CFTs give a different silhouetee to the aircraft with CFTs adding additional physical dimensions behind the cockpit. But perhaps the designers intended minimal radar reflection considering how important LO features are for the Americans. Inputs anyone
Thanks in advance