Both Willard and Westy are basically raising the same points, so I'll answer in one for handiness.
Radar Cross Section
VLO/LO AIAA papers call it one and the same.
Anywayz, dealing with what is on the airframes.
-> The S-H has ducts angled along with tailplanes, and also co-alignment of most other detail surfaces to reduce reflectivity to certain planes.
So does the Rafale. Indeed, some major elements of its substructure have been shaped with reflectivity in mind. The S-H's has not.
-> The S-H has a screw within the duct to prevent radar hitting the compressor face.
The Rafale has a serpentine duct
-> The S-H has RAM incorporated onto various panels.
So does the Rafale.
There is nothing with regards radar treatment that the S-H has that Rafale does not.
Maneuverability
The S-H bleeds energy worse than pretty much any fighter designed since the 50s, it also regains energy slower than any contemporary fighter. In an
era of matured energy maneuverability doctrines in ACM, the S-H is crap. Your own government's oversight committee lambasted the SH for being crap in
maneuvering!
The official report on the decision for the YF-22 has not been published. But its common knowledge within the industry the YF-22 won on three key
points:
1. Maneuverability
2. Lower technological risk
3. Confidence in manufacturer
Passive acquisition
The F-22 relies mainly on passive acquisition to achieve the kill rates it does, why should that be any different for any other platform? Everyone
knows it is easier to see an active radar than be seen by an active radar.
[Don't anyone reply with that LPI pish - there are even books published on how to detect the damn things - check amazon if you don't believe me!]
Weapons
We are comparing aircraft here - since the Rafale can use AIM-120s, the point that the aircraft has inferior weapons to the Hornet is null and void as
it can use the same weapons.
(BTW - the AIM-120D is not in service, so is void as well - unless we want to start going down fantasy lane)
[edit on 27/2/08 by kilcoo316]