Never??? is a long time, does that include next year?.:D
Hmmm
Royal Air Force Eurofighter Typhoons could be deployed to Afghanistan in the ground attack role to support British and allied forces operating there as early as next year.
Speaking at the stand-up ceremony of XI(Fighter) Squadron at RAF Coningsby on Thursday (29 March), the unit’s Commanding Officer Wing Commander Gavin Parker, said: “We are the second operational squadron, but we are the first multi-role squadron.
“We will be prepared and ready to deploy to Afghanistan next year. It has not been timetabled, but I expect that when we are prepared, we will go.”
As for the UK rules of engagement, they may appear too soft, but compare that to the sh1tfight the whole world could be in right now if those rules were not so tight. RoE are there for this reason.
Remember this, when the UK prevented WWIII
“I’m not going to start the third world war for you,” General Sir Mike Jackson, commander of the international KFOR peacekeeping force, is reported to have told Gen. Clark when he refused to accept an order to send assault troops to prevent Russian troops from taking over the airfield of Kosovo’s provincial capital
I doubt even the US wants to start anything big with Iran while were all busy bringing peace and harmony to Iraq.
Lets try diplomacy first, The UK can still nuke Teran if you feel thats an appropriate response a bit later. (you have to wonder how much of a deterrent nukes are?)
Just run through what would have happened if the 15 had actually started firing… likely outcome?, present situation?.
Cheers
OOOH I’m sorry Sauron.. I didn’t mean to upset you…
hello, Hope you all liked it, I’m devastated my hour or two on paintshop wasn’t absolutley perfect, I have no idea what the chinese actually says on the bottom of the screen, But I tried!!
BTW I didn’t even get a chance to follow up with the pilots name “Jai Row” who’s became a little unstable ;-).
Or another comment regarding it wasn’t a deliberate defection just another navigation error!!.
How about Jim Shu (gym shoe) with the “making a run for it” comment.
Happy April Fools day (well it has been here in Oz for hours)
Cheers
Bloody hell!! theres pictures of an f-22 being escorted into a chinese airbase, and news items coming from Chinese sources saying that a pilot and an F-22 has defected and the pilot is seeking asylum.
A chinese spokesperson from the PRC a PLAAF Major Hu Benadd stated the pilot of an F-22 has defected to Luqiao Airbase , and that the pilot is seeking asylum, and that the aircraft has been quarantined and may be returned “at sometime in the future”.
A Japanese correspondent Jim Shu said that during the USAF’s “Polar Foil” exercise the F-22 had made a run for it to the Chinese mainland in the Luqiao Airbase area, and the name and wereabouts of the Pilots is unknown.
Heres a picture I managed to grab taken from a chinese news item, take a look at the tail of the F-22 it looks like its been blurred out in this news item.

anyone got anything more?
cheers
Foolfoone Concorde! TWR
that usually keeps him quiet for a day or two..:diablo:
Jane’s is tipping the Typhoon to win the Japanese airforce’s next-generation fighter order.
its not tipping it to win! its probaly just there to get a good price form the US offers 😉
Wonder why the Rafale wasn’t offered or not considered if it was offered???:confused:
Cheers
Engines performances? dry Max mean the eurofighter lose speed by his mass only, as simple as that, the TWR under 1 mean your mama will never pass Mach 1 without AB! and a supercruise isn’t a plane stoping his AB the Dry at Mach 2 to claim supercruise!
supercruise is sustaining on dry output supersonic speed ,over Mach 1, not going there somes times, its taking off, going to top level 60.000 feets and accelerating till going to Mach 1, when a TW ratio is under 1, the plane don’t have enough acceleration to pass supersonic speed , its just basic physic!
Cheers
Thought you’d disappeared? maybe you missed this post ? I was keen for an answer
Can you please tell me how Concorde defies the laws of physics?
How does it manage to go at M2+,
Empty weight 173,500 lb (Typical TO weight 400,000lbs +)
Total dry thrust 128,000lbs
AB thrust 152,200lbsWhats it T/W ratio… Hmmmm time for humble pie I think.:dev2:
Cheers
Thats just a stupid error mixing up f-35 and F-22’s, You need to pick your sources better, like the USAF
Air Power Purchasing Process Continues to Improve
(Source: US Air Force; issued March 19, 2007)
(See note at bottom-Ed.)
LANGLEY AIR FORCE BASE, Va. — Air Combat Command’s award-winning acceptance team in Marietta, Ga., is setting the precedent on how the Air Force accepts airplanes.
Working alongside the manufacturer, Lockheed Martin Aeronautics Company, during production of the F-22A Raptor, ACC’s Raptor Acceptance Team is a geographically separated unit whose mission is to provide gaining units with “ready to fight” F-22s.
“The biggest benefit is that the gaining unit receives a pre-accepted aircraft,” said Master Sgt. Timothy Silkwood, superintendent of the Raptor Acceptance Team. “Lockheed Martin can now see the aircraft from our perspective while the aircraft is being produced.”
The team consists of 15 qualified specialists who inspect the aircraft as it’s being built and accept it before delivery. By integrating into the manufacturer’s quality inspection process, only the team can give the final “OK to close” on 257 inspection areas.
“The methodology and timing of the inspections is the cornerstone of our success,” said Master Sgt. Gregory Everhart, weapons superintendent for the team.
In the past, a newly delivered aircraft was sent directly to a maintenance hangar where it was disassembled and thoroughly inspected before it was deemed mission ready, a task that lasted about 30 days.
The team identified more than 20,000 defects on the last 24 aircraft before they were delivered. Under the previous system, these repairs would have been made by the gaining unit, costing both money and time. “Military aircraft do not come with a warranty,” Sergeant Everhart said.
Without this process, new Raptors would be unusable for a minimum of 30 days. Additionally, the Air Force would incur the cost, $500,000, to coat and restore the aircraft to operational condition, Sergeant Silkwood said.
It is estimated that the Air Force will save $119 million by pre-accepting the Raptor throughout the current contractual agreement.
Cost savings and innovative thinking earned the team the 2006 Chief of Staff Team Excellence Award. The Raptor Acceptance Team was one of five teams to earn such recognition.
“All of these teams are winners and deserve to bring trophies back to their respective units,” said Air Force Chief of Staff Gen. T. Michael Moseley, when he recognized the winners in September. “Undoubtedly, their innovations are helping our Air Force ensure global air, space and cyberspace dominance in the years ahead.”
The CSTEA recognizes outstanding team performance and shares best practices within the Air Force. It promotes a systematic approach for enhancing mission capability, improving operational performance, and achieving sustained results while maximizing efficiency.
“Because of CSTEA, many great ideas are generated by our Airmen working together as teams to accomplish our mission while conserving precious resources,” said Audrey Tudyk, CSTEA program manager.
According to Col. Ken Murphy, Fifth-Generation Fighter Division chief, the in-plant process template is being considered for use with the multi-service/multi-national F-35 Lightning II program.
“These extraordinary benefits have laid the groundwork for our military’s future on combat operational asset procurement,” Sergeant Everhart said. (ends)
(EDITOR’S NOTE: This article provides a remarkably candid insight into the effectiveness of the F-22 program’s quality controls.
The “more than 20,000 defects” identified before the last 24 aircraft were delivered average to more than 833 defects per aircraft, a truly remarkable figure given the low production rate.
The anticipated savings of $119 million mean that the US Air Force has paid almost $5 million to fix defects on each aircraft that has come off the production line, in addition to the $156.9 million contractual price tag.
It’s indeed a good thing that these problems are being fixed, although one wonders why they weren’t earlier in the production run.)
Cheers
I truly wonder whether the Captor can engage all six targets within its full FOV, or it, as is common to most mechanically slotted arrays, breaks it up into bars and slices..within which it can TWS and engage, and I know of the PR about fast motors etc- but I really dont buy it unless theres an explicit statement about the Captor able to do what an ESA can do..
As you mention its been stated that it fast enough to interleave functions:-
BAE Systems have indicated that the low inertia non-counterbalanced antenna coupled with four high torque, high precision samarium-cobalt drive motors allows extremely high scanning speeds. As a consequence of this the radar can interleave different operations such as air and ground mapping. This is quite an achievement for a non-phased array system.
As you say you can be skeptical, but isn’t this feature unique to a mechical scanned radar, so it deserves some Kudos. and captor has a much wider FOV than a AESA, so does it only have to engage 8 targets within an AESA’s FOV or engage 8 targets across its extended FOV?
An equally valid question is can an AESA target 2 targets at the limits of a Captors FOV at the same time?
Hmmm interesting – thanks
Cheers
I was under the impression that internal fuel was about 5000kg (4995kg is often quoted).
I had a picture of the cockpit of the Typhoon (one of the DA’s) with 4996kg displayed on the fuel gauge, and got the figure confirmed by a Typhoon pilot at the Paris air show, so its 4996kg at the minimum. its as near to 5000kg as to make no difference, I suppose the temperature has an effect on the load to some degree
Cheers
According to http://www.airpower.at the MMH/FH is expected to be only 4.85 hours.
You can look it up under:
Eurofighter -> Eurofighter Technik -> Wartung
Ah thanks Rob my info was getting a bit old re MMH..
Heres the rest of that page roughly translated.
Reliability and maintenance
* Reliability
o less than 400 defects per 1,000 flying hour.
o Mission availability (related to technical reliability) > 95%.
o An autonomous start must be possible in over 98% of the cases.
o One crash per 100,000 flying hours .
* Maintenance
o 4.85 maintenance manhours per flying hour specification in accordance with less than nine maintenance manhours
o 50 per cent of all errors are remediable within 45 minutes.
o 95 per cent of all errors are remediable within 180 minutes.
o An engine change <45 minutes.
o Major maintenance @400 flying hours -thats approx every 2 years.
* Examination
o < 5% of false system error messages .
o 100% of critical errors reported
* Inspection
o A pre-flight check completed by 2 men in less than 15 minutes.
o Turn-Around after intermediate stop completed 2 men < 15 minutes.
o The post-flight inspection completed wit 2 men < 45 minutes.
* Application engineering
o The preparation for air/air employment completed 6 men < 23 minutes.
o The preparation for air/ground employment by 6 men < 30 minutes.
o A role change between each configuration with 3 men < 45 minutes.
The Eurofighter Typhoon had most modern test and monitors like integrated error message and – isolation, automatic system-monitoring device as well as automatic error transmission to the basis still during the flight. The self check ability of the system indicates 100 per cent of all flight safety-relevant errors and ensures a maximum error rate of five per cent. That is in the comparison with other weapon systems an extremely small permissible error rate.
First u are comparing price of Non Aesa fighter with Aesa fighter. and than both deals are signed or executed in different time frame. and there is long list of weopons with Australlian deal. we havent defined fully what system price includes. still EF price is $130m with yesterday technology.
Hmmm.. I’d expect the an announcement soon re AESA and Typhoon, BTW Its not long before the first one is flying in a Typhoon.
The Typhoon Austria deal is helpfully broken down into ‘flyaway only’ price up to ‘Full system’ price, you just need to find a reference to a similar package from the US.(look at the US Foreign military sales announcements).
If the AESA/Non AESA price variation is bothering you, then add an appropriate amount to the Flyaway cost. (Note that the CAESAR upgrade is more expensive to purchase but its cheaper over the aircrafts lifetime due to longer MTBF and less maintainence), so if your comparing Total cost of ownership rather than flyaway then deduct an appropriate amount.
Cheers
yeah the Aussie deal for the Shornet surely makes even the EF2000 seem decently priced. But compare these birds to MiG 35s or even Su 35s/MKIs and y’know what I mean when I say that the cost of the EF2000 is a disadvantage.
Regards,
USS.
Your correct for flyaway price, and possibly flyaway + support equipment.
But thats why I said “total cost of ownership”, Do you agree the Russian designs are labour intensive?, and that their cost over a 30 years period is prohibitive.
Total it all up over the life of aircraft and the initial purchase price accounts for a fraction of the running and maintainance costs.
The Typhoon has exceptional MMH/FH < 9 hours as defined by contract and according to some about 6 hours in real life. (Subject to parts being available), bettered only by the Gripen and estimated equal to the JSF (a one engine design)
IIRC these are the ballpark figures, happy for anyone to correct them…
The Raptor is 15 Hours +
the F-15 is 18 +
F16 = 16+
what are the Russian designs???
To summarize:
Typhoon’s greatest strengths are its MMI and Sensors.
Its competitive strengths are in flying performance, TWR, RCS, uptimes
Its weaknesses lay mainly in its exorbitant cost.Overall a decent bird, but not err “2nd best after f22/JSF”
JMT.Regards,
USS.
Hmmm re the exorbitant cost, it is costly, but all fighter aircraft are!,
You really have to compare total cost of ownership or system price, here’s the figures from the Austrian deal.
Eurofighter costs:-
Flyaway cost of each Batch 2 Typhoon is :-
EUR 62,890,000
The flyaway Cost of each Typhoon with a 9 year finance deal is :-
EUR 74,280,000
The System Cost of each Typhoon without the 9 year finance deal, and including Logistics, Training, and Simulators is :-
EUR 92,610,000
The System Cost of each Typhoon including the 9 year finance deal, and including Logistics, Training, and Simulators is :-
EUR 109,380,000
This is for 18 Typhoon jets, compare this to whats been offered to Australia (24 Super Hornets for $4.7B USD), its cheaper!!.
but you have to compare apples with apples with any other deals you have in mind.
I think its competitively priced!
Cheers
No, I am sorry but TWR is not the end all single factor as to if an aircraft can super cruise or not, far be it, although, if I remember correctly didnt the Concorde have to use AB extensively to get on step??
No it could reach M2 without AB it was just more fuel efficent to do it with AB, not bad for an aircraft with a sub .4 T/W ratio.
wiki says:-
The aircraft used reheat (afterburners) at take-off and to pass through the transonic regime (i.e. “go supersonic”) and were typically switched off at all other times. The engines were just capable of reaching Mach 2 without reheat, but it was discovered operationally that it burnt more fuel that way, since the aircraft spent much longer flying in the high-drag transonic regime even though reheat is relatively inefficient.
I’m just using Concorde as an example for Foolfoone, firstly as its an Anglo-French aircraft:diablo:, and it has a very low T/W ratio, which proves beyond doubt that
TWR under 1 mean your mama will never pass Mach 1 without AB
is a load of bo11ocks.
I rest my case
BTW each of the four Concorde engines only produced ~10,000lbs of thrust while at M2, thats only ~40,000lbs for Mach 2 at 55-60,000ft … interesting T/W ratio huh!:D
Cheers