I attached the pictures with the obvious RCS reduction measures once more.
Oops. Here they are.
I attached the pictures with the obvious RCS reduction measures once more.
European industry types must be rubbing their hands with glee at the prospect of taking one of those apart and bouncing numerous radar combinations at it as it flies across our skies.
Perhaps someone who's intimate with the indian airforce could write down whats the requirements they really need in order of importance, then the aircraft that fits best is a lot easier to see.
On to low RCS. The aussieairpower link says the intakes on the SH are all thats worth doing on a non stealth aircraft to try and lower RCS. They look nice and angular but the big LERX (?) extension, wing leading edges, pylons etc all must bounce back a lot of energy. Would that count for much if an AWACS was angled off in the distance or a ground or ship based radar off at the side?
massively reduced? There are a lot of things you can't see just by looking at a super hornet vs typhoon. For example, the radar dispersion of the canopy coating, active cancellation system, jamming of the opposing radar, effects of having vastly higher composite ratio. And if you get both fighters to put on 4 AMRAAM and 2 SRAAM and a fuel tank, how much RCS advantage do you have left? Also, Typhoon can probably achieve the same range as a super hornet without the external fuel tank.Er, don't forget me. One thing the SH definitely has over the Typhoon is a massively reduced "front on" RCS advantage. Combined with the APG-79 AESA radar systems advantage, it should provide a significantly increased detection range advantage over the Typhoon.
Given they are both using AMRAAM and will be for some time (though RAF only uses AIM-120B IIRC) it's pretty hard to argue the Typhoon's likely advantages even in BVR combat, apart from it's superior (though questionable exactly how much) aerodynamic performance.
massively reduced? There are a lot of things you can't see just by looking at a super hornet vs typhoon. For example, the radar dispersion of the canopy coating, active cancellation system, jamming of the opposing radar, effects of having vastly higher composite ratio. And if you get both fighters to put on 4 AMRAAM and 2 SRAAM and a fuel tank, how much RCS advantage do you have left? Also, Typhoon can probably achieve the same range as a super hornet without the external fuel tank.
None of the RCS reduction features employed in the F/A-18E/F are visible on any of the three Eurocanards
The Navy's justification for the E/F is the improvements it brings over the C/D in range (approximate 20% improvement, up to about 450 nautical miles [NM])
When carrying four 2,000-pound bombs and two AIM-9 Sidewinders, the F-18E/F has a combat radius of 520 nm unrefueled, compared to 341nm for the F-18C (Source:Jane’s Defense Weekly)
Ground attack : hi-lo-hi 750 nm (1389 km)
...
page 9 look at the stealth chart for the evolved legacy fighter (F18E is my guess).. ...
source :- http://www.navy.mil/navydata/people/flags/johnson_j/speeches/usni0423.txtThe “Super Hornet” combines the very best technology
currently available with a 40% increase in range and, almost as
importantly, an increase in endurance, which, to me, translates
into what I call "time over troops," supporting the land
campaign. You have one-tenth the radar signature of its
predecessor.
Perhaps someone who's intimate with the indian airforce could write down whats the requirements they really need in order of importance, then the aircraft that fits best is a lot easier to see, Didn't mean to thread creep,.
my apologies.
cheers
Here is a detailed article by Air Marshal B.K.Pandey (Retd) , Former C-in C Training command, IAF about what is expected of MRCA and his evaluation of various contenders.
Please note that 20 T limit has been dropped from the requirement.
Hope this answers some of your questions.
Selection of MRCA for the IAF
Thanks Kams.
It seems to me that this article is out of date (Jan-Mar 2005) and that requirements have since changed. For example the F/A-18 was specifically ruled out by Air Marshal B.K.Pandey and as you say the 20 tonne limit has now been dropped. As a result aircraft like the F/A-18E/F are now under consideration.
A March 2006 report in Defense Industry Daily listed the contenders as Dassault (Mirage 2000-5 and Rafale), BAE/Saab (JAS-39 Gripen), EADS/BAE (Eurofighter Typhoon), Lockheed (F-16 Block 70) and Boeing (F/A-18 E/F Super Hornet), together with the Russian MiG-29OVT with thrust vectoring (aka. MiG-35).
The article also indicated that the Mirage 2000 was subsequently withdrawn by Dassault.
http://www.defenseindustrydaily.com...as-mrca-fighter-competition-changes/index.php
Cheers