Sean,
Yep Indians right the French Porte Avions 2 is a CTOL adaptation of the Thales CVF design. There are some pictures of the proposed design on the Royal Navy board over at warships1.
WRONG on both side.
France hasn’t decided which design will be used
The design of the british carrier hasn’t been freeeze yet.
With the problem of the CVF and the fact that France need to launch the program really soon, the possibility of an improve CdG (even with classic engines) is not out of order.
I’ve checked the air and cosmos you talked about.
They said 90% of the parts were completed, not the prototype.
Ouch, you’re right.
But in my mind it was more or less the same thing. Perhaps I overestimated the importance of the program
in that article it is said the demonstrator to be built will be not an m88-3 with more thrust but rather a m88-2 based on m88-3(with the same parts,here’s the interest of the word “parts”) with better lifetime rather than more thrust.
Oups, sorry again.
Since South Koeran rejected the RAfale, the only customer for the M88-3 was the french AF who never hide that between a M88-3 with muscles and an economic M88-3, only the latter was considered.
So, like you, i’m not that optimist for that programm.
unfortunately.
I hope that the SAgem-Snecma entity will be able to resume the programm.
On the other hand, SAGEM-SNECMA isn’t in the business to make us happy.
Perhaps (as we discussed on check-six) the rafale with more powerful engine is quite an improvement over the “basic” flavor but I must say that if lots of potentiel upgrade for the Rafale, gripen or even chinese plane speak of newer version of M88-3 but never of real orders.
NOt at all.
Not a very good news according to me.
That and the M88-3 datas dropped from their website, I begin to wonder is it’s alright for that project.
No inews since then but a “the first engine should be completly built at the end of 2003” months ago.
The MiG-29 and the Mirage 2000 also has claims of 10G for emergency maneuvers. So that’s not impossible
13 or 14G for the mirage
it would be nice if France would join the Pak-FA. but traditionally they have always gone their own way and I suspect after some disagreements they might just walk out.
Things change and Dassault really feel the heat of F-35 already.
I suppose that can be a sweet manner from dassault to add another “cheap” plane to gain exports deals.
A way to hedge against that risk is to develop 3 versions like JSF, one to russian specs, one to french and one for whoever else wants to join in – if they have a different vision.
Only the avionics then, never at the same scale with the JSF.
france doesnt have a Raptor class engine. the M88-3 is too small. Russia has the Al41 which can be further developed into a more refined form.
You’re right.
Internal bays means high volume so high price for the plane …. until UAV.
Anyway, Dassault is working with Sukhoi and Snecma with SAturn.
Officially, it has never to do with a new fighter but ….. that could be so cool :dev2:
BRING IT ON
Yep, even Russia + France + India + China cannot fund a fighter at the class of the F-22 in a near future.
Ogami
IIRC, A&C stated that at the end of the Korean competition, the prototype was ready at 80%
The first question is WHO is working on the PAK-FA ?
Russia, ok.
But next ? China ? India ? France ?
Indian
Yes. It is said that blabla human machine interface blabla a single pilot can do all jobs all alone blabla
But as said Ogami, it’s cheaper :d
As Nirav said, nthing official about it.
In Fact, the problem is that an engineer from Thales said a word about it and Thales refused to said anything more AND after that interview has never spoken of that feature so that some “experts” thought that it was the sign that Thales decide to stay quiet about it because they fear to leak important information and to avoid attracting attention.
That how I see the whole story.
The specifications have been dropped from the SNECMA website.
Here is a copy
M88-2b
A/B thrust 75 kN (17 000 lb)
Dry engine thrust 50 kN (11 250 lb)
A/B specific fuel consumption 1,7 kg/daN.h
Dry engine thrust specific fuel consumption 0,8 kg/daN.h
Air flow rate 65 kg/s
TIT (Turbine Inlet Temperature) 1 850 K (1 577°C)
Pressure ratio 24,5
Bypass ratio 0,3
M88-3
A/B thrust 90 kN
Dry engine thrust 60 kN
A/B specific fuel consumption 1,7 kg/daN.h
Dry engine thrust specific fuel consumption 0,8 kg/daN.h
Air flow rate 72 kg/s
TIT (Turbine Inlet Temperature) 1 850 K (1 577°C)
Pressure ratio 27
Bypass ratio 0,3
why not, weren’t they offering it to Singapore?
Only the radar technologies
DAssault and France would be glad to give lots of technologies related to a massive deal about mirage 2000-5 but don’t dream of the rafale.
besides the europeans aren’t going to need a 150-ton-payload strategic airlifter anytime soon. french and germans have lived with nothing more than Transalls and C-130s, and with few expeditionary ops likely in the forseeable future it’s nothing that can’t be handled by some cheap rental An-124s.
Good point.
but I know that the French AF dream of pure french assets instead of rented Ukrainian An-124.
Should the french economy rise several years, with a better budget, the An-124 or C-17 would be considered.