Well this is patently false as the Raptor also has this exact same limit its a function of distance and fuel not any inherent F119/EJ200 engine problems.Mr. Cook,
Tell yourself whatever you have to. Saying it's not time limited while in the same breath saying it's a function of distance from base and fuel reserves is what I've been trying to tell you since day one.
You are so nearly right.. well apart from being wrong.. you are directly contradicting what was in the Email and I'll repost it to aid in comprehensionNow, something you really should pay close attention to...
" This ability was not required by the customer, but the aerodynamic design
work of our engineers simply was so good that as a spin-off the capability
is there."
...a quote from your email. I'll help you to interpret that. The EJ200 is a conventional turbofan and really powerful for it's size. Because it is pushing a very efficient aeroshell. It is able to exceed M1.0 dry under some circumstances. However, this capability was not required and the technology and fuel necessary to sustain this performance is not in the Typhoon.
Please also note the question that was asked... "is the EJ200 time limited in supercruise, or will will it start spitting turbine blades after a while". and the answer was :-but the aerodynamic design work of our engineers simply was so good that as a spin-off the capability is there.
Supercruise (flying at supersonic speed without use of afterburner) is not directly time limited.
For a simple example :- Concordes engines were a development from the subsonic Vulcan olympus engines (via the TSR2) they were not 'purpose built' to a design philosophy.Technology that is a part of the F119 which was purpose built to do that. Fuel, 18,000 lbs worth or 26,000lbs with two drop tanks is in the F-22 which was designed to fight this way to give it huge advantages over traditional late model fighters of the cold war. Supersonic flight is not easy. Sustained supersonic flight is very demanding and has to be a part of the design philosophy because it poses specific challenges.
<sigh> you will no doubt try to wriggle out of this too, but remember the EJ200 is designed to be a supersonic engine, just as a spinoff it doesn't need reheat to get there, thats not too big a leap is it!!Bristol Aero engines developed the Olympus BE.10 as a high power (10000lb) two spool turbojet for the RAF V-bombers to meet spec TE.1/46. By various modifications, including adding a zero stage, thrust was raised to 20000lb. It entered service on the Vulcan bomber, but had such potential, it was further developed as a supersonic powerplant for the TSR2 strike aircraft.
The USAF thinks 3.5 to 7 minutes in a sortie is tactically useful, are you seriously suggesting that the Typhoon is incapable of this?.The Typhoon does not supercruise. By that I mean sustained supersonic flight without afterburners for durations that would be tactically useful.
what distance do you think is tactically useful for supercruise, not time supercruising, not speed supercruising, but actual distance in nautical miles??
Every time I post anything to support the Typhoon supercruising the counter argument never contains anything at all substantive just your assertions that your clever, trained, in the know etc etc, all the things which you have never accepted as 'credable evidence' from anyone else.
I have shown you official Eurofighters sites stating M1.5 supercruise, Independent observations of M1.2 in Singapore, An email from a Eurofighter spokesman saying the engines are capable of sustained supercruise... and you come back with I need something "a bit more substantive".
nfloorl:
IMHO If a whole squadron of Eurofighter Typhoons passed you supercruiseing, while singing the supercruising song, with me waving a supercruising banner, on a "looky here at the Eurofighter supercruising" background then you'd either miss it/claim they were F-22's in disguise/or need something a bit more substantive..
Cheers