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You do have to careful with the drop tank thing.
as an illustration because I don't have the Hurricane numbers look at the P-40E.
The Hurricane may very well be able to do it after it gets the Merlin XX engine, but drop tanks and earlier versions of the Merlin may be a bit doubtful. Using Merlin VIII or Merlin 30 engines (Fulmar engines) may get you off the deck but then saddles your Sea Hurricane with one of the same problem as the Fulmar, crap performance over 16,000ft (or a bit higher in the lighter Hurricane).
I think the max weight for the take-off runs listed were max clean, that is condition (a) 7,015lbs.
American carriers were a lot bigger than RN carriers. All the arguments I've seen against the storing of Glycol, including space, are unconvincing.
The Fulmar II could carry a 60 gallon auxiliary tank. The pilot's notes describe it as such and the fuel system diagram represents the tank in broken lines with the qualification 'if fitted'. It was a self sealing tank and, according to the notes, it was possible to jettison this tank in an emergency. It was NOT a drop tank, and there was no need to store a supply of these tanks on the carrier. The tank, if fitted, was part of the aircraft.
In any case you'll struggle to find a picture of a Fulmar carrying the auxiliary tank. It had 4+ hours endurance on internal fuel and the extra that the auxiliary supply would give doesn't often seem to have been deemed necessary. I've never seen a picture of a Fulmar carrying an extra tank in the Mediterranean, but will happily be corrected.
Cheers
Steve
Hopefully the CAM ship turned into the wind and tried to wind up to full speed before the plane was launched?
Ground test might have been a worst case scenario?
You'd hope so! The 'Hurricats' were very seldom launched. They did destroy six or seven enemy aircraft in the roughly two years they were operated.
I have absolutely zero data on the ground test that was filmed, weight, type or condition of aircraft, let alone the prevailing conditions.
Cheers
Steve
You might want to add self sealing tanks..........and so starts the Weight spiral
Engine in the F2A-2 added at least 100lbs and required a new propeller. The F2A-1 used an engine without reduction gear to the prop. F2A-2 used a reduction gear and a larger slower turning prop.