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The P 51H was of course a new plane but based on the earlier models, I was wondering if there were any parts of its design that could have been improved.I think you can look at what they did with the later models and see the answer. Also the twin mustang for very long range escort. That's as about as far as propellers were going to take them.
It was designed in early 1940.If the P51 was designed from the start as an escort fighter is there anything that would be changed?
If the P51 was designed from the start as an escort fighter is there anything that would be changed?
I was just wondering if the P51D had any fundamental flaws in service which could have been avoided with 20/20 hindsight
If the P51 was designed from the start as an escort fighter is there anything that would be changed?
By 8th AF definition, an escort fighter had to have long range and adequate fighter vs fighter maneuverability and speed at bomber altitudes.
The P 51H was of course a new plane but based on the earlier models, I was wondering if there were any parts of its design that could have been improved.
The Sabre engine should have been shot, stabbed and strangled while still in the crib. And the remains disposed of well out to sea. The Griffon was effectively a 2000hp engine. Considering that a single stage Griffon was 700lbs lighter than a Sabre and a two stage griffon was still 500lbs lighter.
Hello
PR Spits were able to cover Berlin, at least, from GB.
Longest Spitfire escort mission in ETO I'm aware was that made by 131 Sqn on 11 Aug 44 to La Pallice, 690mls and took 3 hours 50 min. They were flying Spit VIIs.
Juha
The XP-51F early test flights in February/March, 1944 with the 1650-3 highlighted the continued lack of yaw stability experienced with the P-51B/C following introduction of Merlin 61/four blade prop system. Ditto the XP-51G and J later. It should be noted that the NA-105 contracts began at the same time the XP-51B emerged and ran parallel to the introduction of the P-51B/C and D. The dimensions were very similar to the P-51B/C/D.
Given the experiences of the yaw stability noted in the very early RAF/RR testing, first the DFF was introduced as a retro fit kit, then installed in production beginning with P-51D-5-NA 44-13903 and P-51C-10-NT 44-107253, then the tall tail was tested on P-51D-5 at both NACA and NAA, then both were introduced in the NA-105 XP51G in middle of flight tests.
The experiences of Mustang X in 1942 through February 1944 with P-51B/C/D and XP-51F led to major P-51H design changes including extending the fuselage length , reducing the fuse tank volume and size, moving the engine CG slightly forward and increasing the empennage area by ~20%,to make substantial improvements in yaw stability.
Interestingly, the AAF did not buy the XP-51G as the projected range of the XP-51G without fuselage fuel tank was only 70 mile combat radius more than a conventional P-51B-1 before kit inst'l. That said it made with combat load, 45,000 feet ceiling (limited by no cabin pressurization), 495mph level flight speed and climbed 7,500 feet per minute. It would have matched any interceptor in the world in 1944
By 8th AF definition, an escort fighter had to have long range and adequate fighter vs fighter maneuverability and speed at bomber altitudes.
When I see claims for the speed of the P-51 on long range missions I am reminded of an anecdote told by Leon 'Woodie' Spears, who surely needs no introduction here.
"I had an air combat encounter in Kitten when my flight of about five aircraft escorted a... I believe it was a British Mosquito reconnaissance plane over a target area. He led us while we kept him in sight. We escorted him to the Munich area to this German ball bearing factory. As soon as he started his photo run, we backed off a little so he could do his work. He had to fly straight and level. The Mosquito was a very fast plane. When we came back from the target area he just out ran us. We could not keep up with him because of his speed. We heard him say on the radio "Ta, ta, chaps!""
Cheers
Steve