A lot of claims being made here, would love to know your sources for the RCS of all these aircraft ?
X2
How about the other missile like r-27 , r-77m , r-37m , r-33 ,RVV-BD ,,,, ect all have much much longer range than aim-120d and meteor
You have been reading the APA site, right?
The R-27 is a vintage weapon, equivalent to a latest generation Sparrow or Aspide, its operational PK was dreadfull (and were did you get the idea that it has longer legs than a AIM-120D or an MBDA Meteor?), it doesnt belong in this discussion.
Whats a R-77M? If its the 1993 Ramjet R-77 project, it went frozen dead more than a decade ago. Vympel has been doing research on ramjet, but there´s no Russian operational ramjet aam, and there´s no sign that such a weapon enters service for the foreseable future. If we are talking of the RVV-SD, its an R-77 with an improved rocket engine, seeker and a new laser proximity fuse. Its an evolutionary improvement over the basic RVV-AE, an R-77″D”.
The R-33 is another vintage SARH weapon, a massive beast (an old one), no doubt that it can/could handle a B-52, now dealing with a recent fighter aircraft thats quite another story.
The R-37, a (much) updated R-33, its operational status is also a bit of a puzzle, the most probable being “operational with the Mig-31BM unit(s)”, its not in widespread use , and sure has hell its not available for “Flanker” use. The R-37 its the only (probably) operational weapon with a clear, useful range advantage over the latest western AAM´s. Its also massively big.
The R-37M, the R-37 with a detachable rocket booster, development status is unknown, its not operational. The program might have ended up in the technological pool for the RVV-BD (or it transformed itself into the RVV-BD).
RVV-BD, a new generation long range heavy weight AAM, in development, operational status “unknown”, for service “some day”, “some day, day unknown”.

If any of our Russian colegues have recent updates, feel free to correct me, recent news are always welcome.
Cheers
A combined deployment isn’t a simple “bring what you have” affair. There is significant pre-planning based on the mission set and limited physical space and logictics resources needed to support combat operations.
Bang-for-the-buck is key. No ally will be allowed to show up with a squadron of jets which cannot fly the primary missions, yet comsume valuable real estate and logistics, and require a circus of jammers and tankers to perform the mission.
Send them home. Let them fly airshows on sunny Saturdays and Holiday fly-bys for the Royal family.
Utter Tosh..
Yes, the fleets of Tornado´s, Rafale´s and Mirage´s have been entirely useless in the multiple “combined deployment´s” that western powers have been doing for the last two decades…
And off course that any non stealth jets will “sent home”… The massive numbers of Vipers, Eagles, SH´s and Warthog´s that the USAF, US Navy and USMC will field for the next… THREE DECADES, will be “sent home” every time that an out of area operation happens, right?
If i ever saw a lousy argument, well, thats it.
And dont get me started on the “Bang for the buck”…
If the primary use is airshow display and fly-by for Royal Holidays, then Gripen will be the correct choice.
And if the alternative is to acquire a handfull of airframes for doing nothing at the airbases because they are too dam expensive to actually fly them, well, Dave A will be a fine choice…
That’s not what I meant. Obviously the F-15 has a higher power-to-weight ratio.
What I am postulating (since the F-35’s specs are not public and testing is not complete) is that the transonic/supersonic drag penalty for the F-35 is less than an armed F-15C.
I was not speaking of Thrust/weight ratio, i was speaking of Drag/thrust ratio. While the F-35A numbers are classified i would be nothing short of astounded to discover that “the transonic/supersonic drag penalty for the F-35 is less than an armed F-15C”, at least if we are talking of four AIM-120´s and no external fuel tanks.
What is the combat radius of a clean F-15C with 4 AAMs and no CFT/EFT?
I’m willing to bet it is lower than the F-35’s 600nm.
Of course that is inferior, it carries a lot less internal fuel than “Dave”, its engines are more thirsty, and its a bigger and heavier airframe. Now stick identical fuel fractions on the two airframes… The point is that for an aircraft with such an extraordinary fuel fraction, equiped with the latest in engine technology, the F-35A range is nothing to write home about, why? I´ll try an educated guess, Drag?
It’s about the size of a T-50, meaning KAI and Lockheed hit the sweetspot 15 years ago.
Yes, because Boeing has (not) already disclosed the dimensions of that design, right?
And nevermind that the dimensions of a BAE Hawk 128 or a Dornier Alpha Jet, etc, are similar to a T-50… BAE and Dornier/Dassault got it right first.
@Sintra:
I did not say that it did not happen, just that it was not the job of the Govt to do it. Besides, those were loans not contracts to buy products. Those loans were (or are in the process of being) paid back.
I understand your point, and in theory i would completely agree with it. But i think Swerve hit the nail on the head, unless LM´s offer is absolutely head and shoulder´s above the rest i am not seeing the USAF delivering this contract to them. I have this idea that “monopoly” is quite a dirty word in the Pentagon (yeaah, i know, Northrop Grumman Ingalls cames to mind, but…).
Cheers
IIRC, The F-15 with only 4 AIM-120s is still draggier than a clean F-35
Is it?
The F-15 eagle with 4 AIM-120´s has a worse ThrustDrag ratio than the F-35A?
If so, an F-35A will outrun and outclimb an almost clean Eagle…
Can you prove it?
Because i am having a really, really, really hard time to believe thats true.
It’s not the government’s (read the people’s) job to keep certain companies in business. If they want to stay in business, then they need to produce a good product at the right price.
G-E-N-E-R-A-L M-O-T-O-R-S
C-H-R-Y-S-L-E-R
Etc, etc, etc
It’s a 350 unit deal, a rarity in today’s defense budget austerity world. Everyone in the business wants to take his chances, such that even a Chinese company wanted to get in.
They had no other foreign trainer vendor to partner with. Maybe Northrop would have gone with Saab if Saab disclosed its intentions sooner.
Oh, right, except those Italian chaps, that are (forcibly) going alone after Boeing snubed a certain “Master”…
Yes, it didn’t specify the supersonic capability. Doing so would have made it a single vendor qualifying program(Before the Saab’s plan to enter the T-X contest, that is).
Since (at least) 2009, no one was expecting a KPP mentioning supersonic dash capabilities.
At 15000 feet, drop 5000 feet, and the turn gets quicker and the g gets higher.
Look at the KPP: “altitude block of 10,000 to 20,000 feet MSL”
And by the way, Boeing its still very much looking at the T-X requirement (with a clean sheet design) and SAAB might make a go at it with a Gripen variant, but its far from certain.
I did some reading on each T-X bidder’s spec and only the T-50 meets the KPP as i t stands. The KPP requires 6.5 G sustained turn, and only the T-50 has this. M-346’s figure is 5.5 G max, and Hawk would be lower than M-346’s figure.
In other word, the M-346 requires an airframe modification while the T-50(The USAF proposed model is actually said to be a customized F/A-50 with an F414 engine) can meet the requirements as is.
Edit : I forgot about the Gripen trainer. The Gripen too would meet this requirement, making this a T-50 vs Gripen showdown.
Maximum sustained load factor at 15,000ft and M0.6-0.8 is +6g and turn rate 14.5°/s – performance that exceeds many fighters and all trainers in either dry power or reheat. Only above M0.8 at this altitude does the KAI T-50 in reheat start to better the turn rate of the M-346. Maximum angle of attack is 40°, which matches or exceeds the limits of most modern fighters and allows the M-346 to undertake post-stall manoeuvres. Maximum roll rate is 230°/s and can be sustained up to 6g.
And the KPP says precisely this:
KPP #2 Sustained G 6.2.2
Aircraft shall be able to sustain 6.5 Gs for no less than 15 seconds (Conditions: 80% fuel weight, drag index = 0, sub-sonic airspeed, altitude block of 10,000 to 20,000 feet MSL) using no more than 15 degrees nose low attitude
I would imagine that the “normal” M-346 would be very, very, very close to this KPP.
How much do all of Typhoons put together weigh… 😉
Never crossed my mind 😀
Compared to Russian industries, BAe did not face any huge financial difficulties or face chaotic period that disrupted supply chains. BAe is a well managed company with good financial weight and still they well managed to send rusted parts along with the costly Hawk jet trainers to India.
I agree but if we speak with our British forúm colegues around here they are going to tell us that BAE is run by a bunch of incompetents :diablo:
why did BAE agreed intially for lower price if manufacturing was not its control. now it has become a saga. only 24 aircraft standard aircraft after 6 years. and those aircrafts are not of the standard that BAE wants price increase for next batches.
Simple, they didnt. The signed contract covered the cost for the original batch built in good old GB, the costs for tranche 2 and 3 were always dependent on future negotiations. And thats whats happening now.
The Gorshokv saga was a sorry affair of “yeah, we´ve signed a contract, but either you pay more or we dont deliver the goods, if you are not happy, tough luck”…
Gorshokv airwing is already delivered and fully operational.
“Fully Operational”?!
No, far from it. But its pretty irrelevant, you have compared the Typhoon acquisition by Saudi Arabia with the Carrier deal, not with its airwing, so…
1500 Indian workers trained on carrier construction and operations. there is no price increase in further 29 MIG-29K. The aircraft deliverd to IN is much more capable from the start.. infact price is increas is only $1.5b on the carrier which is very modest for such thing.
Modest?! They´ve tripled its price after riping a signed contract!
I am quite aware that you live in a very particular world of yours (RUSSIA STROOOONG, YEEEEEEEEEEEEEEAH), but “Modest”?!!!!!!!!!!
Let me guess, Commodore Sukhjinder Singh repeated “modest” twenty times a day?
Its Saudi or BAE responsiblity to setup Typhoon production?.
BAE has been in that country for 30 years. It has 6000 employees there. It knows the technical skills and production cost in that country. so why did it agreed in 2006 and now backed out of it 2010 for seting up production.
It seems to me like Gorskhov saga of not doing due diligence on amount of work and cost estimation. and its not some special version of Typhoon.
Unlike the Gorshokv saga, the first tranche of 24 Typhoon´s were delivered on time and on the exact contractualized delivery dates, and are flying with active units. Unlike the Gorshkov saga the first 24 Typhoon´s were delivered on the originaly agreed and contractualized price…
The responsability of setting up a production plant was first and foremost on the feet of Alsalam, the Saudi company that was indicated by the Saudi MOD, wich by the way is a Boeing subsidiary… It was never going to be a BAE plant built in Saudi.