IF ONLY NavAv was so simple. The links to info in the forum above will likely have info in those threads to explain further.
Arrestor gear has a limit of not only weight but wheelspeed/groundspeed at arrest (add on WOD to have approach airspeed which will always be the Optimum Angle of Attack for that aircraft weight). So at any given weight under the maximum allowed landing weight to engage the arrestor gear (without breaking either it or the aircraft) is one limit that is crucial. For example the F-35C has a KPP max. landing weight (for max. bring back) with an upper limit on approach airspeed KIAS which is 145 knots. This has been explained quite a few times now.
So we have CdeG with some kind of arresting equipment which will have limits not only for maximum airspeed/engage weight but also runout distance on the angle deck. This distance limit will be when the last wire is engaged at max. weight / max. KIAS - what that might be for the RAFALE or an F-35C I have no idea (nor do I care). However using the weight of a prop aircraft approaching at Opt AoA is not the same as the KIAS is likely to be much lower compared to the JET aircraft. You can tell me what the Opt AoA / Weight is for the Prop.
Then there is the catapult. One of the URLs above points to the type of catapult. That catapult will have a maximum ability to shift a given weight to flying speed in the length of the catapult stroke. What that is again I do not give a damn. IF THE F-35C cannot land on the CdeG no point in finding out if it can be catapulted - correctez vu? Probably other websites will have info on the capacity of the arrestor equipment. Several times on this forum a graphic showing the capacity of USN current or recent arrestor gear has been attached.
Charles De Gaulle http://www.naval-technology.com/projects/gaulle/ '...The main deck consists of a main runway angled at 8.5° to the ship's axis and an aircraft launch area forward of the island. These are each equipped with a USN Type C13 catapult, capable of launching one aircraft a minute. The runway is 195m long and the whole deck measures 260m x 64m.
&
Propulsion and power plant The Charles De
Gaulle is equipped with two nuclear pressure water reactors, PWR Type K15, which provide a speed of 27kt...."
I have no reason to doubt this claim - so - IF the other newspaper/online claims above are true it looks to me as though the runout distance for the F-35C aircraft after engaging the arrestor gear is not sufficient (or the arrestor gear has been modified to decrease capacity?). Next to find is the landing area details.... OR the actual deck strength is not good enough in the landing area to take the KIAS/weight at arrest of the F-35C....
“European Security and the Revolution in Military Affairs”20 Jun 2002 Carl C. Hodge"...France’s new nuclear-powered aircraft carrier, Charles de
Gaulle, is designed to be compatible with U.S. Navy F/A 18s and has the same catapult and arresting gear as American Nimitz-class carriers...."
Source: http://www.nato.int/acad/fellow/99-01/hodge.pdf (240Kb)
This USN LSO info is a bit dated at 2010 but useful for ball park figures. For sure the KPP at MCLW Max. Carrier Landing Weight (defined in the KPP) is 145 knots MAXIMUM.
After searching for a while WickedPedia looks appealing so here goes:
French aircraft carrier Charles de Gaulle (R91)"The ship [CdeG] carries a complement of Dassault-Breguet Super Étendard, Dassault Rafale M and E‑2C Hawkeye aircraft, EC725 Caracal and AS532 Cougar helicopter for combat search and rescue, as well as modern electronics and Aster missiles. It is a CATOBAR-type carrier that uses
two 75 m C13‑3 steam catapults of a shorter version of the catapult system installed on the U.S. Nimitz-class aircraft carriers, one catapult at the bow and one across the front of the landing area.[4] ([4] Charles de
Gaulle". GlobalSecurity.org. 10 June 2013. Retrieved 7 November 2014.)"
Source: http://en.wikipedia.org/wiki/French_air ... aulle_(R91)
Charles de Gaulle"...
Trials and technical problemsCharles de
Gaulle entered sea trials in 1999. These identified the
need to extend the flight deck to safely operate the E-2C Hawkeye. This operation sparked negative publicity, however, as the same tests had been conducted on both Foch and Clemenceau when the F‑8E(FN) Crusader fighter had been introduced. The 5 million francs for the extension was 0.025% of the total budget for the Charles de
Gaulle project.
...Two catapults accelerate aircraft (Rafales, Hawkeyes, and modernized Super Étendards) to over 300 km/h in just
75 meters...."
Source: http://www.globalsecurity.org/military/ ... pe/cdg.htm
http://3.bp.blogspot.com/_f_TiAqdkqU4/S ... e+Deck.jpg & from erehwon on the internet a CTOL carrier ROUGH comparison size deck wize.
A4G Skyhawk: www.faaaa.asn.au/spazsinbad-a4g/ & www.youtube.com/channel/UCwqC_s6gcCVvG7NOge3qfAQ/videos?view_as=subscriber