In July of 1943, U.S. Army approved a contract with North American Aviation to
design and build a lightweight P-51. Designated NA-105, 5 aircraft were to be
built and tested. Edgar Schmued, chief of design at NAA, began this design
early in 1943. He, in February of 1943, left the U.S. on a two month trip
to England. He was to
visit the Supermarine factory and the Rolls Royce factory to work on his
lightweight project.
Rolls Royce had designed a new version of the Merlin, the RM.14.SM, which was
proposed to increase the manifold pressure to 120 (from 67 max) and thus
improve horsepower to 2,200. Schmued was very eager to use this powerplant.
The new Merlin was not heavier than the earlier models. Schmued visited with
the engineers at Rolls Royce and they answered his many questions. Schmued left
the Rolls Royce factory very satisfied with their cooperation.
British fighters were lighter than U.S. fighters. Schmued ask for
detailed weight statements from Supermarine on the Spitfire. Schmued wanted
to know why the Spitfires were so much lighter than the P-51. Supermairne did
not have such data on the Spitfire, so they started weighing all the parts they
could get a hold of and made a report for Schmued. The British had design
standards that were not as strict in some areas of design as the U.S. Landing
gear, angle of attack and side engine design loads were higher in the U.S.
When Schmued returned, they began a new design of the P-51 Mustang that used
British design loads. They shaved weight on any part that could yield. They were
able to reduce the empty weight of the P-51 by 600 pounds. This would translate
into more performance.
The lightweight prototypes were designated XP-51F, XP-51G and XP-51J. After
testing of these prototypes, the production version, NA-126 P-51H, was
closest to the XP-51F. The project began in April of 1944 and the contract for
1,000 P-51Hs was approved on June 30, 1944.
The H model was a completely new design. Yes it looks like a P-51, but you can
tell there is something not the same. I remember as a teenager when I saw my
first P-51H in person. I asked my dad, "that's a Mustang ... isn't it?" as I
looked at it and tilted my head slightly. He
looked and my uncle looked, and then they paused and decided that yes it
was a mustang and it must be the later H model (they were seldom stumped when
I asked them aircraft ID questions).
Almost all the parts from the D line were not usable in the P-51H. This was
the first production P-51 with a complete overhaul. The wing did not have that
famous leading edge kink in it. The landing gear was visibly smaller. The profile shows
new lines with a taller tail (later versions). The fuselage was a bit more slender
and the length was increased to 33.33 feet. The wingspan stayed the same.
The belly scoop inlet profile was not angled any longer but was now square
again like the first P-51s. The chin scoop for the engine was decreased in size.
The wheels now had disk brakes. The oil cooler was moved from inside the
belly scoop to in front of the oil tank ahead of the firewall. This
eliminated the oil lines that ran from the engine to the old location in the
scoop. The oil was now cooled by a heat exhanger mounted next to the engine
intercooler.
The engine mounts were incorporated into the structural engine cradle,
thus saving weight. The engine would not be the newer RS.14.SM Merlin as
in some of the lightweight prototypes. The Rolls Royce Merlin
V-1650-9 was chosen. Take-off horsepower was actually down from the -7 series
to 1,380. But, the new -9 Merlin used water/alcohol injection and was able
to up the war emergency power to 2,200 at 10,200 feet. This was the fastest
production P-51 clocking 487 mph at 25,000 feet.
The propeller of the P-51H was the Aeroproducts 11'1" 4-blade Unimatic
otherwise know as the "H prop".
This prop is even lighter than the K model Aeroproducts but it looks much
different. The blades are wider and keep approx. the same width almost the
whole blade. The tips are rounded.
Armament was the same as in the P-51D. Removable ammo boxes and a
redesign of the ammo doors were added.
This saved time reloading and must have eased up on the laminar flow
killing scratches and scuffs on the wings. The earlier models had to be
loaded by hand out of portable ammo boxes. The top surfaces of the wings
were taking a huge beating and disrupting the true laminar flow of the wing
surface. I honestly doubt the crews in the field either knew or cared much
about that.
Fuel in the fuselage tank was decreased to 55 gallons max. The fuselage
skins were lighter and thinner, made from a new alloy. The cockpit panel was
improved and simplified. The canopy was redesigned and the "hump" moved further
forward. The pilot sat higher for a better angle using the gunsight.
The first P-51H
flew on Feb 3, 1945 with Bob Chilton at the controls. This P-51H-1NA, 44-64160
was wrecked three days later when the prop failed. The USAAF flew test flights on P-51H 44-64161 from Apr 4-14, 1945 by pilot Major J. D. Onerem.
Production continued and 221 P-51Hs were delivered by July 30 and 370 by VJ Day in early September.
Contrary to what many believe, the P-51H did not start out as "the tall tail Mustang".
The first 20 P-51H-1NA were built with the lower D model height tail. These
units were later retrofitted with the taller tail. The taller tail and smaller
fuselage fuel tank of 55 gallons, rid the P-51 of the annoying directional
stability problem.
Production was cut short by the end of the war. All P-51H versions were built
at Inglewood, Ca. The Dallas, Tx version of the P-51H, NA-129 P-51L with the
newest Merlin, the V-1650-11, would not finish any models. The last P-51 off
the Texas production line was an NA-124 order which included the newer
P-51M which was an improved P-51D-30 with the V-1650-9A Merlin and a
Hamilton Standard Prop. The -9A Merlin did not have water injection. One
production M model was completed. The 63 partially built units were scrapped.
The last P-15H-10NA rolled out of the Inglewood factory in November of 1945.
In all, a total of 555 P-51H models were completed: 20 P-51H-1NA,
280 P-51H-5NA and 255 P-51H-10NA were finished and accepted in the USAAF.
Even though some units in the pacific received the P-51H before VJ Day, they
did not see any action. Ironically, when the start of the the
Korea War broke out, the earlier version of the P-51, the P-51D was chosen
to do the fighting, not the P-51H. In the years to follow, the H was used
in many Air National Guard units around the U.S.
Only 5 P-51Hs survived, 2 are display quality only, 2 are airworthy and the last
is in restoration to be airworthy. One of the XP-51G prototypes does exist and
is in a long term restoration with John Morgan in California. This G model
was saved by chance and fast action while on its way to the scrapper.
Model | P-51H | |
Production | 555 | |
Length | 33.33 | |
Height | 13.67 | |
Wingspan | 37.04 | |
Weight - empty | 7040 | |
Weight - normal T.O. | 9,500 | |
Weight - max G.W. | 11,500 | |
Powerplant | Packard (Rolls Royce) V-1650-9 | |
Horsepower | 1,490 | |
Propeller | - | Aeroproducts 4-blade |
Max Speed | 490 at 25k | |
Service Ceiling | 41,320 feet | |
Fuel Capacity | 255 | |
Drop Tanks | 2x 75 or 2x 108 | |
Range | 855 and 1,200 w/DT | |
Armament | 6x .50 cal. - 1880 rounds (2) 1,000 lb bombs or rockets |