A bit OT but i know guys almost twice my weight, thats about 22 stone that can beat me in a sprint. just saying.
What i KNOW for sure is that this article is a total JOKE.
😎
Thumbs UP to everyone!!! 😀
A MiG-25 can take off and climb to an altitude of 35,000 meters (114,000 ft) in a little over four minutes.😎
http://www.globalsecurity.org/military/world/russia/mig-25.htm
I think i was about 20 years old i already knew it…
Barry Scott
and nothing more and only those who post in this forum, no names mentioned, are the real experts.
Experts are teachers or curently in service in whatever useful area of the trade they can work.
If you were thinking of me, i’m flatered but i regard myself as an advanced enthusiast only, although even a glider pilots would know tons more about it all by necessity than most of you.
And No i never flew jets by my main instructor DID he actualy WAS the HEAD of the Flight Test Centre of Bretigny a *** AdA AirCorps General Guy Fleury, BTW the kind of guy who thaught ME one sure thing; in this buziness if one doesn’t LEARN, one DIES, the faster the aircraft, the FASTER one dies.
Please, if your interest is showing off in forums, stay grounded for your own safety and that of others.
EELightning
Registered User Join Date: Jan 2009
Location: UK
Posts: 33Some of these threads would be interesting if they weren’t b*tch
Skip the bulls then and look at the quality posts, but you’re right, forumers are like young birds, they didn’t learn to keep bitching for bedtime…
Scorpion82;1349440]My point stands and that is what it was all about from MY side. But sure I don’t know what I’m talking about:rolleyes: (Rhetorical I know your answer…)
Yes Scorpion they STAND out as pure FANTASY and utter SPIN.
I doubt I will find anything on pratrical (I warned you my friend :p)
And as said I meant kinetic, was an error besides me… The contents of my statements remains the same, but that is obviously the least you care about.
No you didn’t you insisted it meant kinetic energy and was used commonly i still have this page saved care to see your own MANURE posted again?
Was that the question? No as usual not, but you are twisting around things not related to the topic. Your usual escape… I know why;)
No question here your diatrtibes on how bad they would perform at 50.000ft.
One of the few things I agree with you. Nonetheless it is usually comprehendable (at least for 99% of the people, surprisingly not for you).
We all agree you have NO clue what you’re talking about. 😀
I had my a$$ in quite a couple of real aircraft like F-16, Tornado, B-1B etc. As said you know a sh!t about me.:rolleyes:
I meant flying them BOY…😎
Why should I care if you are p!ssed or not? Do you care about that? NO you don’t so don’t expect others to treat you different than you treat them.
Am certainly NOT pissed by a guy who makes a total goof of himself in public and keep thinking no one notices, you amuse me to say the least. 😀
Nice and you pretended to know it is 9.1t when it was in fact not.
I posts what datas were available at the time YES and also provided them from official sources.
And surprisingly people like me believed those newer figures more rather than sticking with the wishful thinking which was your case. Funny you still try to find an excuse instead of admitting that you were wrong.
Newer figures weren’t available at the time, you were just agreeing with the Typhoon mafia claiming “superiority” by TWR.
LMAO. Who is “we“? They (Dassault/AdA) informed me as much as you.
Me and other French posters of course, naturaly Dassault and those who have to learn on their trade as for myself AND Dassault you have NO idea.
Aerodynamics yes, never dealt with that beyond some basics (I don’t have to to do my work or fly virtually).
Basics?
No mate you aren’t even at this BASIC level, you have NO clue what BASIC means since you haven’t learnt them.
And History and Procedures, and Flight mechanics and Structural design and Navigation, and Meteorology, FROM WHICH THE WORD CEILING is coming from. 😀
If you had known this, you would KNOW why WE employ CEILING as a mean to indicate an altitude, a plafond in French; and naturaly you would KNOW that since France was the quasy inventor of MOST basic international procedures including world’s FIRST flight licences, the translation in English today are sometimes a little sensless to people like YOU…:diablo:
Yawn.
As i say you’re IMUNE to knowledge and it SHOWS. 😀
You must be a superguy to load an AIM-9 and check functionality:rolleyes: Tell me with how much services has you worked and exercised?
We l it made ME a little less IGNORANT; “Super”, no i make no such claim but just this little more AWARE.
Reach for your painkiller now.:cool:
From an article by Ariel Cohen
Washington (UPI) Jan 14, 2009Wonder where he got that 57,000 foot number?
Could he have mistaken the loaded weight?
I think the USAF will be pleased to know this! 😀
F-22 factsheet.
Ceiling: Above 50,000 feet (15 kilometers)
http://www.af.mil/factsheets/factsheet.asp?fsID=199
General Characteristics
Primary Function: Air dominance, multi-role fighter
Contractor: Lockheed-Martin, Boeing
Power Plant: Two Pratt & Whitney F119-PW-100 turbofan engines with afterburners and two-dimensional thrust vectoring nozzles.
Thrust: 35,000-pound class (each engine)
Wingspan: 44 feet, 6 inches (13.6 meters)
Length: 62 feet, 1 inch (18.9 meters)
Height: 16 feet, 8 inches (5.1 meters)
Weight: 43,340 pounds (19,700 kilograms)
Maximum Takeoff Weight: 83,500 pounds (38,000 kilograms)
Fuel Capacity: Internal: 18,000 pounds (8,200 kilograms); with 2 external wing fuel tanks: 26,000 pounds (11,900 kilograms)
Payload: Same as armament air-to-air or air-to-ground loadouts; with or without 2 external wing fuel tanks.
Speed: Mach 2 class with supercruise capability
Range: More than 1,850 miles ferry range with 2 external wing fuel tanks (1,600 nautical miles)
Ceiling: Above 50,000 feet (15 kilometers)
Armament: One M61A2 20-millimeter cannon with 480 rounds, internal side weapon bays carriage of two AIM-9 infrared (heat seeking) air-to-air missiles and internal main weapon bays carriage of six AIM-120 radar-guided air-to-air missiles (air-to-air loadout) or two 1,000-pound GBU-32 JDAMs and two AIM-120 radar-guided air-to-air missiles (air-to-ground loadout)
Crew: One
Unit Cost: $142 million
Initial operating capability: December 2005
Inventory: Total force, 91
Point of Contact
Air Combat Command, Public Affairs Office; 130 Andrews St., Suite 202; Langley AFB, VA 23665-1987; DSN 574-5007 or 757-764-5007; e-mail: [email]accpa.operations@langley.af.mil[/email]
http://www.af.mil/factsheets/factsheet.asp?fsID=199
=Scorpion82;1349405]1.) Optimised doesn’t mean it can’t operate at higher altitudes. The Tornado is optimised for low level close to ground, but that doesn’t mean it can’t operate above 500 ft. Simple logic, you don’t grasp it!
YES DOES actualy. More precislely that it is a totral SLOUCH at anything above 40.000 ft.
2.) No it’s not practical for regulare missions i.e. flying patrols, escorts, fighter sweeps.
Search for the words: Pratrical and Cinematics in the handbook and you’ll have an idea. 😀
3.) Try to operate subsonic and manoeuver sufficiently there good luck Mr. Supersmart.
LOL! As you knew anything about it!
Look boy, i posted Mirage 2000 acceleration times from subsonic to M 1.98 or so as for the rest of its flight envelop as it was DESIGNED for this i don’t SEE where it would have a problem out-turning a F-16 or F-35 at 55.000 ft. 😀
I’d rather stick to lower alts in normal operations as the average performance is better there, who cares about achieve absolute max. speed at 55k ft if you are a sitting duck when operating subsonic there.
You’d rather stick behind your keyboard INVENTING stuff rather than learn them.
Oh excuse me to use common language to make people understand what it is all about. Your f*ckin word nitpicking is nothing else than a ridiculous bad excuse for your lack of true arguments.
Common language is NOT aerospacial language and is your way to INTERRET reality, everything remotly technical is “f*ckin word nitpicking”…
Operational altitude IS NOT max. altitude. Simple point.
Sure; it is writen on the box, you’re quiet a GENIUS here… 😎
BTW get yourself a dictionary and translate the word ceiling.
The dictionary doesn’t always apply to the way people speak in this buziness and there is a good old historic reason for this, but since the closest you ever came to get your ignorant @ss in the front seat of an aircrafft is Micropsoft Sim you couldn’t possibly know.
I was told it was considered or even tested, so for what do you think such a consideration has been for pitch up manoeuvers?:diablo: I meanwhile know that the canards are moving sysmetrical only, hence no roll. So what…?
AND IGNORANT ENOUGH NOT TO FIGURE SOMEONE WAS TAKING THE P!SS BIG TIME.
I well remember your hard battle pretending Rafale C’s empty weight is just 9.1t, while I said newer sources suggest at least 9.4t. Janes even said 9.85 t (but of course when it doesn’t suite your mind its crap, but if it suites your mind you take it for gospel, doesn’t matter if it is the very same source…).
It was at some point since the empty weights were given as developement progressed and avionic baies have enough room for more than the difference, when the C rolled out, it was weighted below 9.000 kg.
So you offended me of not being in the know and the usual bla bla and that Dassault know their stuff and that you have accurate first hand data (supposedly Dassault material).
This is still true, they know their stuff you don’t even know your basics.
Now a bit later we all no empty weight is 9.5 t so I was right you was wrong. But you just silently acknowledged it, because the mighty Sampaix is never wrong:rolleyes::p:D
And you’re lucky there we managed to dig the official sources to INFORM you because of course you still wont bother today.
Wow a flying license and loading weapons on a Mirage III (LOL) makes you an way above all expert in terms of military aviation and other related matters:rolleyes:
Precisley!
WAY more knowledgeable than you on these subjects by nature; to sumerise you would blow your b@alls trying to invent yourself a “better” way to box-test a par of AIM-9 loaded under a Mirage or get yourself stupidly killed very publicly applying your punny notions of aerodynamics and flight procedures. 😀
What I see is a crap load of nonsense besides you:diablo:
Whith the layer of this material you have pouring off your eyes you CANT see, this is WHY you DONT learn, boy…
According to F-15 pilots, they can WIN vs any aircraft as long as they fly within the best part of their flight envelop…
Higher and FASTER the Eagle is BETTER, the opposite applies lower and (relatively) slower…
Why do you only include graphics that support your assertions, but discard the ones where LM/USAF claim 400 percent A2A superiority over legacy aircraft? While the percentage may be debatable, I’d think that they’d know what the capabilities/requirements for the aircraft are. One of those was flight performance at least as good as F-16/F-18, combined with VLO and 5th Gen avionics.
SORRY, commercial bollock!ng designed to support a programme = not my cuppa.
You take it as godsend i analyse it, different approach.
And BTW this was writen by WHOM exactly?
According to AdA, 400% ratio also applies to Rafale vs Mirage 2000 which is no slouch in BOTH A2A and A2G.
=Scorpion82;1349307]The point is the 30-40k ft typical operating altitude band for the F-35 is not the same as the 55k ft operational ceiling of the Rafale. Simple point you refuse to recognise.

30-40k ft typical operating altitude band for the F-35 REALY?
You’re THE specialist here… Some more knowledgeable people actualy desagree no?
As DID the French AdA, Marine Nationale, Defense Ministry, Top Air Defense Squadron 1/2, Dassault -Aviation etc.
NO! YOU tried to IMPLY three different things previously mate:
1) F-35 has a 50.000 ft ceiling when in FACT it is clear it is OPTIMISED for a much lower one.
2) Operational ceiling of 55.000 ft weren’t “practical” as you put it wrongly…
3) Operational Ceiling wasn’t a good place to be performance-wise for “them”…
The word CEILING itself indicates it’s the upper limit.
No it doesn’t it does give a flight LEVEL in ft.
Upper isn’t even in use when it comes to Ceilling; Maxi IS.
That’s the maximum altitude at which the aircraft can be operated given the margins before reaching abosulte ceiling.
:D:D:D:D:D:D
Upper, Absolute, Cinematics.
We’re reaching the UPPER LIMITS OF THE ABSOLUTE REVISONISM….
Max. altitude to be achieved in a zoom climb is a different topic and has nothing to do with operational ceiling.
Max altitude of the Mirage III is 25.000 ft ABOVE its Operational ceiling of 50.000ft and the WAY you climb there doesn’t change this FACT a IOTA nor the FACT that you sitll dont know what you’re bubling about and are INVENTING IT.
You obviously don’t comprehend the word ceiling and draw wrong conclusions by that.
😀 Reverse phychology and spin at its best.
And that has what to do with the definition of operational ceiling?
NOTHING: I know what it realy means and take it for what it is since you got BOTH Maximum and Operational it’s made simple for you.
Here Ceiling values used to compute best climb rates at different flight levels.
By these guys who obviously have to be thaught some by Mr Scorpion82…
Has anyone said it wasn’t? NO! As usual you are bringing up points irrelevant for the discussion!
Everything you dont know or fail to comprehend is according to you “irrelevant“…:dev2:
bla bla bla. Much noise for nothing as usual for you…:rolleyes:
Go learn you basics boy.:rolleyes:
You pretty much know a damn sh!t about me, so stop pretending you do:mad: And BTW I don’t care about your so called education. It proves nothing!
Sure Scorpion, what i KNOW is; you’re the one who believed Typhoon’s canard were acting in the Roll axis aren’t you?
No need to ask how come you didn’t know your A (structural design chapter) from ABC as thaught in Airclubs around the world, as for Military matter it is pretty much the same and BTW, education is NOT meant to “prove” anything, only to comprehend some.
You SEE, those who know happens to be able to spot those who dont.:diablo:
=pfcem;1348879]I see you STILL fail to understand the basic concept of a KPP THRESHOLD…
SAY YOU. Perhaps to hide the FACT that you don’t KNOW what DESAIGNED MACH LIMIT, supersonic DASH and M 1.5 means?
Quite simply, if the F-35 did/does not MEET OR EXCEED an OPERATIONAL top speed of Mach 1.6 it would not have been selected or be accepted.
M 1.6 is NOT the KPP THRESHOLD as you imply but the DESIGNED Mach Limit.
Here on earth is was…
Legoland forum? 😀
No, the USAF is THE primary customer.
The USAF ONLY came second into the programme which was initiated more than TWO years previously by USMC and RAF/RN.
Expected to aquire the greatest number of aircraft & who’s requirements were the PRIMARY driving force behind the JSF with USN & USMC varients adapting the USAF design to their requirements.
FALSE: AGAIN; ONLY ADDING SUPERSONIC DASH ANDINTERNAL WEAPON BAIES.
Numbers doesn’t MEAN they wrote the specs in the first place and they didn’t, they just added Mid-Supersonic DASH and internal weapon baies to the already existing ones which included Operational ceilling similar to that of Harrier II+.
The USAF had a requirement to replace it’s F-16’s, the USN had a requirement to replace the F/A-18’s AND the USN/UK had a requirement to replace their Harriers. Three separate programs which it was decided in order to same developement costs were combined into a single program which became the JSF. You are FALSELY applying the PRE-JSF USN/UK Harrier replacement requirements to the F-35.
Blah-di-Blah the usual half-story of the whole thing.:dev2:
And this is NOT “FALSELY applying” it is programe and specification evolutions, primary role and specs didn’t CHANGE…
BUT if you want to play such childish games, the Typhoon’s origins can be traced back to a Jaguar replacement so by your convaluted thinking the Typhoon is LIMITED to Jaguar-like characteristics. 🙂
No “childish” games here simply my knowledge of the WHOLE of F-35 Politico-industrial history vs your cut-down internet version…:D
Replacing the F-16, F/A-18, AV-8 & A-10 (& if the incompetent DOD leadership has its way the F-15 as well)…and that is JUST in the US! How much more multi-role can you get?
The BAe Hawk 200?
LOL! In the strike role boy!!!
This doesn’t MEAN a LWF replacement, can YOU tell the difference between the TWO?
No, F-16/F/A-18 ‘like’ aero performance.
Which is the most imprecise way to fool newbies like yourself into thinking it was designed like one, obviously they perhaps need your $ to pay for the US part of the programme, not mine.
And you skiped the STRIKE role part of the F-16/F/A-18 ‘like’ aero performance, it’s in A2G confiruration that the F-35 is optimised not A2A as were the LWF designed and Optimised.
HERE> OPTIMISED FOR AIR-TO-GROUND LETHALITY.
Doesn’t look like LWF requiered specs to me.
http://i146.photobucket.com/albums/r279/sampaix/AFAORG-DATS.jpg
As for what specs means, ask the guy responsible for those of LWF and FX (F-16 and F-15)…
http://www.youtube.com/watch?v=oC6bF4f2iiU
Stop making a damned fool of yourself, it is quiet obvious that you are lacking SO MUCH elements on the programme that you hardly can comprehend its role and the meaning of the word OPTIMISED in the first place.
Aircraft performances are resulting from Requiered Specs and deisng features, not requiered numbers or the FACT that the original role of the aircraft they replaces have changed…
Please dont bother me any longer with Wilkipedia’s stories, i got enough of Jane’s yearbooks at my disposal and TONS of docs on the subject including the programme requierement of the time (go dig them on the internet for a laugh)….
Meaning i can tell who knows about it and who does not, you DONT.
As usual you still don’t get the point and I don’t care to try explaining this to you further as you are incapable to grab it or simply unwilled to do so due your sheer ignorance!
and what is “THE POINT” Scorpion82?
The FALSE one you were making in your recent comments?
The Rafale’s 55k+ ft figure (or take any max operational ceiling figure for any aircraft you want) is NOT equal to the 30k – 40k ft figure of the F-35, which is the regulare, normal, typical, usual (choose the word that best suits YOUR standards) figure. I tried to make you understand that simple fact, but you seem to be incapable to get the point for what ever reason.
It’s pretty obvious by now who is the IGNORANT.
“Upper” “Maximum” Operational ceiling anyone?
Just a CLUE. Operational have a MEANING, Ceiling too, when put together it means Operational Ceiling no more no less.
Where is it ANYWHERE specified “Upper” or Maximum” in the official links i posted?
Can you tell the difference between a “bleeding” turbojet and a turbofdan?
Was or wasn’t M-88 OPTIMISED for High-Altitude/High-speed interception responding to ACX requierements?
So basicaly you dont have enough of your sheer imagination and ignorance you also have this twisting and spinning tricks in your sleeve (as well as reverse psychology heading for copycating at a a HUGE rate)…
FAR remote from the realities of aviation.:diablo:
Cold war is over and MiG-25/31 doesn’t pose a threat any more!
The ceiling given for the F-35 (30k-40k ft) is the practical operational altitude.
The F-35s operational ceiling is for sure 50k ft or more, but the typical altitude band for operations is 30k-40k ft, as the performance/economics ratio is best here.
Neither of these aircraft is operated at altitudes of 50k ft plus on a “regular” base as you claim, though all of them are capable to fly at that altitudes.
The fact remains, aircraft like the F-16 or F/A-18 for example weren’t designed to operate at 50k ft on a regulare base either, yet the manufacturer and customers state 50k ft as its operational ceiling.
Most service ceilings given in publications are upper limits. Can the aircraft operate there? Yes it can! Does it operate there on a regulare base? No! And why doesn’t it operate there? Because the performance at such altitude would be insufficient!
SAY WHO?
Please DONT mystake ME for the image in the mirror boy, as i SAY YOU dont have ANY Aerospacial education; meaning the very basics of theorical flight as thaught to any Air Cadet or begginers in air-clubs the world’s over.
So unsuprisingly you keep missinterpreting and fail to comprehend most of it.
The SAME applies with your Military experience.
So when I READ your arrogant diatribes on other’s “ignorance“, knowing what was thaught to ME in BOTH Air Club and Air Force i can but only SMILE. 😀


Latest Rafale’s warpaint. (Literaly). 😎
the jet powered Raven is fully autonomous from take off to landing and is highly agile.
Link.
http://www.baesystems.com/Newsroom/NewsReleases/autoGen_1071513151.html
SURE! No one dispute this point…
As it became SO AFTER Corax first BAe’s UAV autonomous FIRST flight on 25th Jan 2005.
What YOU allege is that it FLEW fully autonomously on Sept 17th 2003 and this is NOT the case, the FIRST BAe UAV to fly FULLY autonomously was Corax on Jan 25th 2005 equiped with the SECOND Raven’s fuselage.
A full year after SAAB SHARC. 😀
The French won’t order more than 286.
So far so good. 😀
=aurcov;1349216] a B1, for example, will bring an insesisable penalty, vs a clean B1. But the EF/Rafale are not so much bigger than the F 16, so the penalty will be less, butnevetheless visible.
Stick with fighter-sized aircrafts and the difference becomes negligible.
As for the configuration of rafale in the picture, if those had to carry 8 tons of fuel and 6 missiles, as the F 35 will carry internally, I can bet the Rafale won’t supercruise and won’t go faster than 1.6 M, so it won’t offer nothing much over the F 35 . I said comparable configuration, remember?
Weapon load in A2G is mainly stricly subsonic, since USAF wanted F-35 to do better than F-16 in the strike role it requiered internal weapon loads.
Of course, a clean, or even slightly charged Rafale (1 x 1250 EFT) will supercruise.
Agreed.