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A monoplane carrier-borne aircraft were looking as an oddball, until the people really tried it. So did the 2-engined jobs, until tried. Heck, all aircraft were looked upon as oddballs prior ww1, let alone naval A/C.
Yep, the production of the P-38s only really hit the stride after there was no that much need for them, like in 1944/45.
The proposal was dated as of 1937. Should be tested by 1939 if the Navy wants it?
For a take off weight of 32000 lbs, the B-25 was supposed to use 1400 ft of runaway at 40 mph headwind, 0 deg C; at 28000 lbs, it was 1000 ft. The Doolittle raiders weighted 31000 lbs, yet managed to take off at under 500 ft of the deck space. No assist used.
Less said about P-39 and P-40 production in 1944 the better
Stretching things a wee bit???
The twin engine carrier planes weren't really tried until carriers and carrier decks got much bigger than they were in the late 30s and very early 40s.
same could be said for a number of US aircraft. Like 3130 F4Fs built in 1944 out of 7904 for the entire war. Less said about P-39 and P-40 production in 1944 the better
Using what for engines? The navy did test the Airabonita : Bell XFL Airabonita - Wikipedia, the free encyclopedia
But a 1939 version would use the C series engines at best with turbo operation being somewhat problematic?
Service version would happen when using what for engines?
What you can pull off for a one shot, special mission with specially trained crews is not what is acceptable for day in, day out service. Trying to time the take-off for maximum upward pitch of the carrier deck when the plane crosses the bow so you can trade the most altitude for airspeed (sort of like the ski jump flight deck used for harriers) was not a good idea for day in, day out operations in all weathers/climates.
BiffF15 said:
The P-38 didn't have problems flying on one engine. Fly around until you've used up the fuel and then land.
Tomo,
On all twins I have flown so far engine out approaches are flown at a lesser flap setting and higher speed (greater stall margin / power reserve). Also fighters, unlike airliners, generally land sooner rather than later (engines inside the plane vice out / less redundancy of systems) with the mentality that the problem will continue to grow. Both of those situations drive getting on the deck sooner rather than later, and the higher trap speed will introduce the need for stronger cables, and or the boat to move faster through the water to generate a lower approach speed for the plane.
Cheers,
Biff
I don't believe that the Airabonita is a good example of the US Navy showing interest in an inline fighter, to be frank.
If the navy was to invest in an earlier fighter, wouldn't a purpose built naval aircraft be a better bet, rather than disrupt army contracts to build a derivative of an existing design? Boils down to that typical argument of this kind of what if scenario, doesn't it; go with what you've got or go for an entirely new design. Surely, the time taken in modifying an existing design would/could be as much as starting from scratch.
I dunno, Tomo, based on what Shortround and the others are saying, can it really? I don't believe that the Airabonita is a good example of the US Navy showing interest in an inline fighter, to be frank. If the navy was to invest in an earlier fighter, wouldn't a purpose built naval aircraft be a better bet, rather than disrupt army contracts to build a derivative of an existing design? Boils down to that typical argument of this kind of what if scenario, doesn't it; go with what you've got or go for an entirely new design. Surely, the time taken in modifying an existing design would/could be as much as starting from scratch.
I don't believe that the Airabonita is a good example of the US Navy showing interest in an inline fighter, to be frank.
I agree that a purpose-built CV fighter with a V-12 should do better than a quick fix of the ground-based fighter. The USN was probably hoping they would have the Airabointa in service in shorter time, than it would be possible for a brand new design.
For a take off weight of 32000 lbs, the B-25 was supposed to use 1400 ft of runaway at 40 mph headwind, 0 deg C; at 28000 lbs, it was 1000 ft. The Doolittle raiders weighted 31000 lbs, yet managed to take off at under 500 ft of the deck space. No assist used.
Forget folding wings, installation of a hook etc. The only thing that's going to get a P-38 serving on a US Navy carrier deck was if it had radial engines. Besides, what could the P-38 offer that the F6F and F4U within the time frame did not have that the US Navy needed, apart from two engines, and even then, they were the wrong kind.
Exactly what problem did the USN have with liquid cooled engines? The RN had no issues at all it seems. The P-40 likely would have made a good carrier fighter early in the war, possibly better than the wildcat.