The Curtiss P-40 was undoubtedly one of the most controversial fighters
to serve in quantity during the Second World War. It was praised and abused,
lauded and vilified, but the fact remains that, as the first American
single-seat fighter to be manufactured on a mass-production basis, it bore
much of the brunt of the air warfare over several battle fronts. Its
performance was inferior to the performances of the majority of its
antagonists, but this shortcoming was partly compensated for by its
tractability and its sturdiness which enabled it to withstand a considerable
amount of punishment. It was amenable to adaptation and it was available when
most sorely needed.
Not particularly good technically or in performance, though very durable,
P-40s continued to be produced until the end of 1944, serving also with air
force units of Turkey, South Africa, Canada, Australia and New Zealand. Later
versions were known as Kittyhawks to the RAF and its Allies. Not usually
realized is that the name Warhawk applied only to the United States Army Air
Force P-40s starting with the P-40F version, a much improved plane with a
license built version of the British Rolls-Royce Merlin engine installed.
The belief in the "ascendancy of bombardment over pursuit" was rife in 1937
when the Curtiss P-40 was first envisaged, and it is a sobering thought that,
with the Bell P-39
Airacobra this product of such a school of thought constituted more than
half the strength of all USAAF fighters until July 1943. Prior to September of
that year the P-39 and P-40 also comprised more than half the
USAAF fighters committed overseas. However, by July 1945 only one P-40 group
remained operational.
The prototype P-40 took to the air in the autumn of 1938, and production was
initiated in the following year. Performance of the first version of this
single-seat fighter had not really come up to expectations, but as several air
forces were desperate for new aircraft, the type was welcomed into service.
The US had delayed modernizing its Army Air Service until the last minute, so
P-40s made up a large part of their equipment during the first years of war.
Britain and France also ordered P-40s to contend with the German Luftwaffe,
but in the case of France, deliveries came too late and their P-40s were
diverted to the Royal Air Force - to be known as Tomahawks. Similarly, the
Soviet Union's outdated air force had fared badly at the hands of the Germans,
and P-40s were also sent there.
The P-40 was initially designed around the Allison V-1710 liquid-cooled inline
engine which offered better streamlining, more power per unit of frontal area,
and better specific fuel consumption than did air-cooled radials of comparable
power. Unfortunately, the rated altitude of the Allison engine was only some
12,000 feet, rendering combat above 15,000 feet a completely impracticable
proposition. The P-40's ancestry dated back as far as 1924; the famed Curtiss
Hawk fighters being in the forefront of all US warplanes. But its development
was hindered from the start. The overall limitations of its design were such
that the addition of multi-speed superchargers was considered inadvisable in
view of the pending production of superior fighter designs. The achievements
of the P-40 were therefore all the more creditable.
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The Curtiss
P-40 served during most of the Second World War with one air force or
another, and under several different names including Tomahawk and
Kittyhawk in Britain and Warhawk in the United States. |
The prototype XP-40, the Curtiss Hawk Model 81, owed its origin to the
earlier Model 75 of 1935 vintage. With the standardization of the Allison
V-1710 , the P-36 design was reworked to incorporate this engine, becoming the
XP-37 which was equipped with a General Electric turbo-supercharger, and
featured numerous other modifications, including a rearward positioned
cockpit. Thirteen YP-37s were built for service evaluation; but, with
increasingly ominous signs of an approaching war, development of this fighter
was abandoned in favor of a less complex and more direct conversion of the
P-36 for the Allison engine, the XP-40. This was, in fact, the tenth
production P-36A with an integrally-supercharged 1,160 h.p. Allison V-1710-19
(C13) engine, and first flew with its new power plant in the autumn of 1938.
Successful in a US Army Pursuit Contest staged at Wright Field, in May 1939 it
was awarded what was at that time the largest-ever production order for a US
fighter, totaling nearly thirteen million dollars.
The P-40 was a relatively clean design, and was unusual for its time in having
a fully retractable tail wheel. One hundred and ninety-seven P-40s were built
in 1939-40 for the USAAF, and many more were sold abroad to Britain and
France. In the RAF, which service purchased 140 outright, it was known as the
Tomahawk Mk. I, IA, and IB, and carried two .303 in. Browning machine-guns in
place of the 0.30in.-calibre guns fitted in USAAF machines. It retained the
standard synchronized armament of two 0.5 in.-calibre machine-guns in the top
nose decking.
Many US volunteer pilots flew on behalf of Britain, the Soviet Union and China
before the United States entered the war. A group of them, equipped with
P-40s, went to help the Chinese in their struggle against the Japanese in
1942, where they became known as the 'Flying Tigers' because of their uniquely
painted aircraft. This group later became part of the USAAF proper, and P-40s
were thereafter used widely in the Pacific.
In the middle of 1941 General Claire Chennault began recruiting for his
Volunteer Group--better known as the Flying Tigers--to fight the Japanese from
China, for which 100 P40s were ordered for purchase through a loan from the US
Government. Ninety aircraft, mostly P-40Bs, were actually delivered,
sufficient for three squadrons, plus a few spares. At the time of the USA's
entry into the war there were eighty American pilots in the Volunteer Group,
and shortly after arriving at Kunming the P-40s drew first blood, six out of
ten attacking Japanese bombers being destroyed by two of the AVG squadrons on
December 20. There were no American casualties on this occasion, but the third
squadron, left behind at Mingaladon, Burma, was less fortunate, and lost two
pilots on their first interception, on December 23,1941. The American pilots
had underestimated the maneuverability of the lightly built Japanese Zero
fighters, and failed to utilize their superior speed and diving ability to
advantage. It was soon the cardinal rule that a P-40 should always avoid
mixing it individually with a Japanese fighter, owing to the Curtiss machine's
inferior climb rate and maneuverability, but the P-40 substantiated a
reputation for ruggedness that it was already acquiring with the RAF in the
Middle East, and its armor protection saved many AVG pilots in subsequent
combat.
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Click on Picture to enlarge |
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Many US
volunteer pilots equipped with P-40s, went to help the Chinese in their
struggle against the Japanese in 1942, where they became known as the
'Flying Tigers'. |
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Both the Flying Tigers in China and the RAF squadrons in the Middle East
had their P-40Bs replaced by P-40Es. The AVG after continuous operation, was
down to some twenty P-40Bs by March 1942, when some thirty P-40Es were ferried
to China by air from Accra, in Africa. The improved performance offered by
these more potent P-40s was found to be extremely valuable against the
Mitsubishi A6M Zero-Sen fighters which, first introduced in the
Chinese theatre in 1940, were becoming increasingly numerous. The
ground-attack potential of the P-40E was also much superior. The AVG pilots
had resorted to carrying 30-lb. incendiary and fragmentation bombs in the
flare chutes of their P-40Bs, but it was questionable whether this was not
more hazardous to the attackers than to the attacked. But some indication of
the P-40's capabilities in resolute hands is given by the fact that from its
inception in December 1941 until July 4, 1942, when it was absorbed by the
USAAF, the AVG was officially credited with the destruction of 286 Japanese
aircraft for the loss of eight pilots killed in action, two pilots and one
crew chief killed during ground attack, and four pilots missing. The
top-scoring AVG pilot, Robert H. Neale, was credited with the destruction of
sixteen enemy aircraft while flying the P-40, and eight other pilots claimed
ten or more victories.
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Specifications: |
|
Curtiss P-40N-20/35-CU Warhawk |
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Dimensions: |
|
Wing span: |
37 ft. 4 in. (11.37 m) |
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Length:
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33 ft. 4 in.
(10.15 m) |
|
Height:
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12 ft. 4 in.
(3.75 m) |
|
Weights: |
| Empty: |
6,700 lb.
(3,039 kg) |
| Operational:
|
8,400 lb.
(3,810 kg) |
|
Performance: |
| Maximum Speed:
|
325 m.p.h.
(523 km/h) @ 25,000 ft. (7,620 m)
343 m.p.h. (552 km/h) @ 15,000 ft. (4,572 m)
308 m.p.h. (495 km/h) @ 5,000 ft.(1,524 m)
|
| Service Ceiling:
|
30,000 ft.
(9,144 m) |
| Range: |
750 miles
(1,207 km) @ 10,000 ft. ft. (3,048 m) |
| Max. Range:
|
2,800 miles
(4,506 km) @ 10,000 ft. (3,048 m) |
|
Powerplant: |
One Allison
V-1710-99 , Vee, 12 cylinder, liquid cooled engines.
Engine power developed 1,200 h.p. (894 kw) @ takeoff and
1,125 h.p. (838 kw) @ 17,300 ft. (5,273 m) with a single speed
supercharger. |
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Armament: |
Six 0.5-in. Browning machine-guns with 281 rpg with provision for
external bomb load of three 500-lb. bombs. |
One of the most significant steps in P-40 development came in 1941, when a
British-built Rolls-Royce Merlin 28 engine with a single-stage, two-speed
supercharger was installed in a Kittyhawk I airframe to improve its
high-altitude performance. The Curtiss H-87-D, or XP-40F, as the
Merlin-powered prototype became known, then had 1,300 hp available for
takeoff, and 1,120 hp at 18,500 feet, which offered vast improvements over
earlier models and endowed a maximum speed of 373 mph. This was reduced
slightly in the YP-40F, which, like later variants, had the Packard-built
Merlin V-1650-1 and revised cooling, the air intake above the cowling being
incorporated in the radiator scoop. Gross weight climbed to 9,870 lb.
Following experiments in cooling-drag reduction in 1943 with a P-40K-10-CU
which had its "beard" radiator removed to wing installations, and in rear
vision improvements by installing a "bubble" canopy on a standard P-40L, a
general " clean-up " program was initiated, resulting in the sole XP-40Q. With
a 1,425 hp Allison V-1710-121 engine, the XP-40Q was modified from the first
P-40K-I to have a "bubble" canopy and cut-down rear fuselage, wing radiators
and, eventually, clipped wing tips. A four-blade propeller was fitted, and
water injection installed. With a weight of only 9,000 lb, the XP40Q attained
a maximum speed of 422 mph. This was still less than the speed attained by
contemporary production Mustangs and
Thunderbolts , however, and the XP-40Q did not achieve production.
The
Aviation History On-Line Museum.
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Curtiss P-40
"Tomahawk" : One
of WW II’s Most Famous Fighters |
Robert Guttman

If the Curtiss P-40 Warhawk was not the best fighter in the arsenal of
the U.S. Army Air Corps (USAAC) when the United States entered the conflict,
it was the most numerous type available. The Lockheed P-38 Lightning could
outperform the P-40, especially at high altitude, but the P-40 was less
expensive, easier to build and maintain, and — most important — it was in
large-scale production at a critical period in the nation’s history when
fighter planes were needed in large numbers.
A total of 11,998 P-40s were built before production was finally
terminated in 1944. Warhawks constituted the principal armament of the U.S.
Army Air Forces (USAAF) fighter squadrons throughout 1942 and 1943. Even
after the appearance of newer types of fighter aircraft in the USAAF
rendered the P-40 obsolete, it continued to contribute to victory in a
variety of Allied air forces.
The P-40 was the product of a long development process that began when
the USAAC invited various aircraft companies to submit designs for its 1935
fighter competition. Curtiss and Boeing had dominated the U.S. Army and Navy
fighter plane business since the end of World War I. In 1933, however,
Boeing had beaten Curtiss in competition for a lucrative Army fighter
contract with its innovative P-26 Peashooter. The P-26 was a monoplane of
all-aluminum, stressed skin construction. Ralph Damon, the head of Curtiss,
was determined that his company’s next fighter should have the benefits of
the latest design and construction technology. In 1934, he hired Donovan R.
Berlin as Curtiss’ new chief engineer. Berlin had previously worked at
Douglas and Northrop, two firms that had been at the cutting edge of
aircraft design.
The four rival designs for the 1935 fighter competition, from Curtiss-Wright,
Seversky, Vought and Consolidated, were the first really modern fighters to
be evaluated by the Army. All four were low-wing monoplanes of all-metal,
stressed-skin construction with retractable landing gear and enclosed
cockpits.
Curtiss designated its entry the Model 75. Since all Curtiss fighter
aircraft had been called ‘Hawks’ since the mid-1920s, the new fighter became
known as the ‘Hawk 75.’ Powered by a 900-hp Wright air-cooled radial engine,
the Hawk 75 was first flown in May 1935 and demonstrated good
maneuverability and flying characteristics. Initially, however, the USAAC
rejected the Hawk 75 in favor of the Seversky P-35. It subsequently reversed
that decision, however, and in 1937 it ordered 210 of the Curtiss fighters —
the Air Corps’ largest order of a single type of fighter aircraft since the
end of World War I. Fitted with a more powerful Pratt and Whitney R-1830
Twin-Wasp radial engine, the new fighter was designated the P-36A.
Significant as the USAAC order was, it was small compared to the total
number of Hawk 75s sold overseas. Curtiss had been selling large numbers of
Hawk biplane fighters to various nations in Europe, Asia and Latin America
since the 1920s. With war clouds gathering throughout the world in the late
1930s, Curtiss had little difficulty finding foreign buyers for its new
monoplane.
By far the largest customer for the Curtiss fighters was France. At
the time of the 1938 Munich crisis, the French aircraft industry was having
difficulty meeting its air force’s demands for modern fighters. The French
government decided that the most expedient solution to the problem was to
order 730 Hawk 75s from Curtiss, in the neutral United States. H-75As, as
the French called them, were the most numerous fighters in the Armée de
l’Air’s inventory when WWII began, and they shot down more German planes
than any other French fighter aircraft. The Hawk 75s that had not yet been
delivered to France before the country surrendered to Germany in June 1940
were transferred to Britain’s Royal Air Force (RAF), which called them
Mohawks.
Some of the French H-75As were seized by the Germans after France’s
collapse and sold to the Finns for use against the Soviet Union. Others,
still in French hands, were transferred to North Africa, where they
continued to operate under the control of the Vichy French government. On at
least one occasion, during the Allied landings in Morocco in November 1942,
Vichy French H-75As tangled unsuccessfully with U.S. Navy Grumman F4F
Wildcats.
Since the end of World War I, domination of the world’s aviation
engines had been alternating between liquid-cooled in-line engines and
air-cooled radial engines. The liquid-cooled engines were generally more
powerful, but they were also heavier, more complex and vulnerable to damage
if the coolant leaked out. The radial engines were lighter and more compact,
but their larger frontal area created aerodynamic drag. As it happened, the
Hawk 75 was developed at a time when the liquid-cooled V-12 engine was just
beginning to come back into vogue, both in Europe and the United States. The
principal reason was the introduction of high-temperature cooling utilizing
Glycol rather than water, a development that made it possible to reduce
weight and drag by decreasing the size of the cooling radiator by as much as
75 percent.
In February 1937, while the USAAC was still evaluating the P-36 for
production, it contracted with Curtiss to re-engineer the fighter to test
the potential of a highly promising new liquid-cooled V-12 engine, the
turbosupercharged General Motors Allison V-1710. To save money, the factory
rebuilt the original Hawk 75 prototype to create the new prototype. First
flown in 1937, the XP-37, as the new fighter was called, was not an
unqualified success. Although its 1,150-hp Allison engine and aerodynamic
lines gave it far better performance than the P-36, it had a number of
serious drawbacks as a combat plane. The General Electric turbo-supercharger
boosted the engine’s critical operating altitude — i.e., the altitude at
which the supercharger would operate at peak efficiency — to 20,000 feet,
but it proved unreliable and likely to catch fire. In addition, the cockpit
had to be moved aft to balance the heavy engine and its bulky
turbo-supercharger, which reduced pilot visibility.
Despite the promising performance of the turbo-supercharged Allison
engine, the problems encountered with the XP-37 were rapidly reducing the
likelihood that the airplane ever would be placed in production. Therefore,
Don Berlin decided to take a different approach to a P-36 derivative
equipped with an Allison engine. On March 3, 1938, Curtiss submitted a
proposal to the Air Corps to modify a P-36 airframe to accept an Allison
engine fitted with a mechanically driven supercharger. The modifications to
the airframe were less extreme than those required for the XP-37, as they
did not require moving the cockpit aft. The engine also proved to be more
reliable than the turbo-supercharged Allison used in the XP-37, although its
critical operating altitude was reduced to 10,000 feet, with performance
falling off at higher altitudes up to its service ceiling of 32,750 feet. At
Curtiss the new fighter design was known as the Model 81, but the Air Corps
called it the XP-40.
The prototype XP-40 was first flown on October 14, 1938, only two
weeks after the settlement of the Munich crisis bought the world a one-year
reprieve from war. It was modified from the 10th production P-36A airframe.
The XP-40’s sharply pointed nose was longer than that of the P-36, though
not so long as that of the XP-37. Since the cockpit was not displaced aft,
the pilot’s view was better than in the XP-37. The radiator, which had been
buried in the fuselage between the engine and cockpit of the XP-37, was now
installed under the fuselage, aft of the wings.
Although Curtiss had guaranteed that the XP-40 would achieve 360 mph,
the prototype was not immediately able to do so. After a series of
modifications that took several more months, however, the fighter
demonstrated a top speed of 366 mph at 15,000 feet. The most conspicuous
change was the relocation of the radiator to a new position under the nose,
giving the P-40 its most characteristic feature.
The XP-40 won the Army’s 1939 fighter competition against the Lockheed
XP-38 Lightning, Bell XP-39 Airacobra, Republic AP-4, and Curtiss’ own XP-37
and Hawk 75R, the latter a turbo-supercharged version of the radial-engine
P-36. The XP-38 outperformed the XP-40, especially at high altitudes, and
was more heavily armed, but the XP-40 had the advantage of being based on an
existing fighter design that was already on the production line. That meant
that Curtiss could put the P-40 into production with a minimum of delay, and
at the highly competitive price of $24,566.60 apiece. On April 26, 1939,
Curtiss was awarded a contract for 524 P-40s — once again, the largest order
for fighter planes placed by the Army since 1918.
The P-40 prototype was armed with one .50- and one .30-caliber machine
gun — the standard USAAC fighter armament during the 1930s — but the
production model was armed with two .50-caliber machine guns. In keeping
with President Franklin D. Roosevelt’s policy of making the latest American
military hardware available to the Allies, 140 of the original batch of
P-40s were diverted to France. They were armed with one .50-caliber machine
gun in the fuselage and four 7.5mm guns in the wings. None of those P-40s
were delivered by the time France capitulated, however. Instead, the export
P-40s were delivered to the RAF and became known as Tomahawk Mk.Is.
The British were grateful for all the combat aircraft they could get
in 1940, but they did not regard the Tomahawk Mk.I as suitable for combat.
Many of the Tomahawk Mk.Is still had metric instruments and other French
equipment that were not compatible with RAF service, and their French
throttle control levers worked in reverse of the way British or American
ones did. More important, they lacked self-sealing fuel tanks and had
neither armor nor bulletproof windscreens to protect their pilots.
Consequently, the Tomahawk Mk.Is were relegated to tactical reconnaissance
duties.
As a result of European combat experience, Curtiss installed armor in
the P-40 and increased its armament, adding a .30-caliber machine gun in
each wing. The improved fighters were called P-40Bs by the Americans and
Tomahawk Mk.IIs by the British. The next model, known as the P-40C, also had
self-sealing fuel tanks and yet another .30-caliber machine gun in each
wing. The USAAC ordered a total of 324 P-40Bs and P-40Cs during 1941. At the
same time, the British ordered 930 P-40Cs. Those with British radio
equipment were called Tomahawk Mk.IIas, while the ones delivered to the RAF
with American radios were designated Tomahawk Mk.IIbs.
First flown in April 1941, the P-40C was considered the first truly
combat-ready version of the P-40 line. A price had been paid for the
necessary improvements, however. The aircraft’s gross weight had increased
from 7,215 to 8,058 pounds, an increase of 843 pounds or approximately 11
percent, with no increase in engine power. The P-40C’s rate of climb
suffered, it was less maneuverable, and its maximum speed fell to 340 mph.
By comparison, the Messerschmitt Me-109E used by the Luftwaffe in
1941 weighed only 6,100 pounds and had a top speed of 360 mph. Air Chief
Marshal Sir Kenneth Cross, who served in the RAF’s Desert Air Force,
recalled that ‘the Tomahawk was beautifully built, but…short on performance
compared to the (Messerschmitt) 109F and G.’
By the end of 1941 the USAAC had deployed P-40s overseas. Thirty were
flown to Iceland from the aircraft carrier Wasp, and 99 of them were
stationed in Hawaii. In addition, four squadrons of P-40s were deployed in
the Philippines. It was with the British that the Tomahawk Mk.IIs first saw
action, however, flying reconnaissance sorties and fighter sweeps across the
English Channel with the RAF and Royal Canadian Air Force (RCAF) in 1941. By
May 1941 Tomahawks were also operating in the Middle East, eventually
serving in that theater with Australian and South African fighter squadrons
as well as the RAF. In addition, the British sent 195 Tomahawks to the
Soviet Union after the Germans invaded that country on June 22, 1941.
The first serious use of the P-40 as a fighter occurred when Iraqi
forces led by Rashid Ali El-Ghailani rose against the British in Iraq on May
2, 1941. When the Germans and Italians sent aircraft to assist the revolt,
staging from Vichy French bases in Lebanon and Syria, the British sent three
Bristol Blenheims to bomb the air base at Palmyra on May 14, escorted by two
Tomahawks of No. 250 Squadron, RAF, flown by Flying Officers G.A. Wolsey and
F.J.S. Aldridge. The Iraqi revolt was crushed by May 30, but the British
decided that Vichy France’s violation of neutrality justified the invasion
and occupation of Lebanon and Syria. Tomahawks of No. 3 Squadron, Royal
Australian Air Force (RAAF), took part in the first attack on June 8,
helping to destroy a Dewoitine D.520 fighter and damage three others at
Rayak airfield. Elsewhere on that same day, two of No. 250 Squadron’s
Tomahawks drew first blood for the P-40 in the air when they shot down an
Italian Cant Z.1007bis reconnaissance plane five miles northwest of
Alexandria, Egypt. The Vichy French put up a spirited fight before finally
signing an armistice on July 14, but the Tomahawks of No. 3 Squadron RAAF
also acquitted themselves well, holding their own against France’s
top-of-the-line D.520s and shooting down two out of eight German Junkers
Ju-88As of II Gruppe, Lehrgeschwader 1, operating from Crete, that
tried to interfere with British landings on the Levantine coast on June 12.
During the summer of 1941, No. 112 Squadron RAF, which had lost all
its Gloster Gladiators in Greece the previous spring, was re-equipped with
Tomahawks. Its pilots took one look at their sleek new mounts and decided
that the P-40’s cowling would make an ideal place to paint the squadron
badge, a black cat. The results, however, looked more fishlike than feline,
and soon a variety of shark mouths were being applied to the Tomahawks and,
later, to the deeper-jowled Kittyhawks. For some reason, British authorities
did not discourage No. 112 Squadron’s flamboyant liveries. The P-40 shark
mouth would soon be adopted in other units and other air forces.
David B. Brown, who flew Kittyhawks in No. 112 in 1942 and later
Supermarine Spitfires, recalled: ‘The Kittyhawk, while offering a more roomy
and comfortable cockpit than the Spitfire, with a bonus of improved
visibility, was more sluggish on controls and inferior in performance when
compared with the Spitfire V. Furthermore, even though we could cope with
moderate aerobatics and mock dogfights, there was still a feeling of
‘touchiness’ about the P-40 so that you wanted plenty of altitude before you
could relax….’
Me-109F aces such as Hans-Joachim Marseille took a grisly toll of
P-40s, but some of the more talented Commonwealth pilots rang up their own
fair tallies of Axis planes while flying the Curtiss fighters. Australian
ace of aces Clive R. Caldwell, flying Tomahawks in No. 250 Squadron and
later Kittyhawks as commander of No. 112 Squadron, was credited with 18
German and Italian aircraft, plus two to four shared, six probable and 15
damaged over the Western Desert, later adding seven Japanese planes to his
score while flying Spitfires over the South Pacific.
American P-40s first saw action at Pearl Harbor on December 7, 1941.
Of the 99 P-40Bs stationed in Hawaii that day, only seven managed to get
airborne during the attack. They shot down five Japanese planes, including
four — two Nakajima B5N2 torpedo bombers, a Mitsubishi A6M2 Zero fighter and
an Aichi D3A1 dive bomber — by 2nd Lt. George S. Welch of the 47th Squadron,
15th Pursuit Group. By the end of the day, however, only 25 P-40s remained
operational. Three had been shot down, and the rest were destroyed on the
ground.
In the Philippines, as in Hawaii, attrition was high — 26 P-40s were
destroyed on December 8, 1941, mostly because they were caught on the
ground. Although initially shocked by the startling performance of the Zero
fighters that faced them, the four squadrons of P-40s put up a gallant
struggle against the Japanese invaders.
The first USAAC ace of World War II was 1st Lt. Boyd D. Wagner, a
P-40E pilot of the 17th Squadron, 24th Pursuit Group, in the Philippines.
During a surprise attack on the Japanese army’s 50th Sentai, newly arrived
at Aparri airfield on December 12, Wagner was attacked by four Nakajima
Ki.27 fighters. He evaded two, then suddenly cut his throttle to make the
other two overshoot him and shot down both. After strafing five to seven
Japanese planes on the ground, Wagner was attacked by three more Ki.27s but
managed to shoot down two of them and then escaped. He was subsequently
awarded the Distinguished Service Cross, as was 1st Lt. Russell M. Church,
Jr., who was shot down in flames and killed by anti-aircraft fire in the
course of the raid. Wagner repeated his performance at Vigan field on
December 16, hitting eight enemy planes on the ground and shooting down a
Ki.27 that managed to take off, for his fifth victory in as many days. By
then, however, there were too few of the Curtiss fighters available to do
more than delay the inevitable. Lacking spare parts and replacement
aircraft, the Americans were overwhelmed by May 1942.
Thomas L. Hayes, who flew P-40Es with the 35th Pursuit Group, was
originally supposed to go to Mindanao, but when his squadron was unable to
reach the Philippines it was diverted to Java in mid-January 1942. ‘The
water-cooled Allison…moved the center of gravity forward,’ Hayes recalled.
‘The P-40 was much heavier than the P-36, and visibility was somewhat
restricted with that extended nose. The P-40 also had more difficult landing
characteristics than the P-36 — its greater weight, combined with the narrow
landing gear and long nose, gave it a greater tendency to ground loop.’
‘The most serious deficiency in my training was gunnery,’ he added.
‘The only time I had squeezed the trigger was strafing an oil slick dropped
in the Pacific. Tactics were a close second. We were indebted to our
veterans, who told us, ‘You’re not going to turn and fight with a Zero — you
won’t live to tell about it.’ Tactics were hit and run — if one had the
altitude on a Zero, one could dive and get him. But engagements usually
began with the Japanese above the P-40s — they threw the first punch.’
Hayes was shot down and wounded by a Zero on February 20, 1942,
crash-landing his P-40E in a rubber plantation. After escaping from the
Dutch East Indies, he went on to fly P-39s over New Guinea, and North
American P-51s over Europe with the 357th Fighter Group, Eighth Air Force,
finishing the war with credit for destroying 8 1/2 German aircraft.
By far the most renowned of all Curtiss fighters were the 100
dispatched to China for use by the American Volunteer Group (AVG), or
‘Flying Tigers.’ Usually referred to as P-40s, they were technically
Tomahawk Mk.IIbs that had originally been built for the British. The Flying
Tigers got the idea for their famous shark mouth marking from magazine
photographs of No. 112 Squadron’s colorful Tomahawks. The AVG’s exploits
made the shark mouth so famous, however, that P-40 units all over the world
began copying it from them.
The AVG never had more than three squadrons of 18 P-40s at any time.
Flying their first combat mission on December 20, 1941, the Flying Tigers
operated under extremely difficult conditions at the end of the world’s
longest supply line — and with the war’s lowest supply priority.
Nevertheless, by the time the group disbanded six months later, its pilots
had shot down 286 Japanese aircraft. During a period in the war when
everybody else in the Far East was being soundly defeated by the Japanese,
their achievements were truly phenomenal.
The AVG owed its success to the tactical doctrines developed by its
leader, Colonel Claire Lee Chennault. A former USAAC fighter pilot who had
carefully observed Japanese aircraft over China, Chennault understood the
strengths and weaknesses of both the Japanese and American fighters. Using
that knowledge, he established an advance warning system, which involved
Chinese observers relaying information to AVG air bases, giving his pilots
prior intelligence on what Japanese forces were coming and when they would
arrive. He also drilled three fundamental rules into his pilots. First,
never ever try to turn with a Japanese fighter in a dogfight, since it could
maneuver its way onto a P-40’s tail within two turns; instead, use the
P-40’s superior diving speed to escape, then climb and re-engage. Second,
Chennault advocated head-on passes, because the Curtiss, with its two .50-
and four .30-caliber machine guns, could outgun its Japanese army
counterparts, which were still armed with only two 7.7mm weapons. The third
rule was to harass the Japanese planes after they retired — since they
lacked self-sealing fuel tanks, a few holes in their tanks would probably
cause them to run out of fuel before they reached their home bases. These
rules were the secrets of the Flying Tigers’ success.
Technically, the AVG personnel were U.S. civilians employed by the
Nationalist Chinese government. Because of that, their P-40s were painted
with Chinese insignia. Their success, highly publicized in the United
States, was actually something of an embarrassment to the USAAC and its
successor, the USAAF. The AVG was disbanded when an agreement was reached
with the Chinese government to induct the Flying Tigers and their P-40s into
the USAAF on July 4, 1942.
Curtiss-Wright was well aware of the P-40C’s shortcomings. In 1940 it
developed a replacement fighter, mounting 10 machine guns and powered by an
improved version of the Allison engine. Known as the XP-46, the new fighter
did not enter production because Maj. Gen. H.H. Arnold, the Army Air Corps
chief of staff, insisted that P-40 production should not be interrupted.
Instead, Curtiss-Wright developed a new version of the P-40 incorporating
the same 1,150-hp Allison V-1710-39 engine intended for the XP-46. The new
P-40’s nose was considerably altered because the new engine was shorter and
had a higher thrust line, and the radiator air intake was enlarged. The
armament was changed to four .50-caliber guns in the wings. First flown in
May 1941, the improved fighter was called the P-40D Warhawk by the USAAC and
Kittyhawk Mk.I by the British. In April 1941, Curtiss built the first of
2,320 P-40Es, or Kittyhawk Mk.Ias, armed with six .50-caliber wing guns.
In an attempt to improve the P-40’s performance above 15,000 feet,
Curtiss installed a Rolls-Royce Merlin engine in a P-40D to produce the
XP-40F. The British were concerned that Rolls-Royce might not be able to
supply enough Merlin engines for their own and the Americans’ needs, and at
the same time, General Arnold was concerned that Allison could not supply
sufficient liquid-cooled engines to fulfill the Army Air Corps’
requirements. As a result, on September 13, 1940, the British contracted
Packard to build 6,000 Merlins for the RAF and 3,000 for the USAAC. The
production P-40F Warhawk, or Kittyhawk Mk.II, became the first American
fighter to use the 1,300-hp Packard Merlin and first flew in October 1941.
With a top speed of 364 mph, the P-40F was 10 mph faster than the P-40E. The
only external difference between the P-40E and F was the absence of the air
scoop on top of the P-40F’s cowling, due to the Merlin’s updraft carburetor.
A total of 1,311 P-40Fs were built, as well as 700 similar but
lighter-weight P-40Ls. When the supply of P-40F and L airframes outstripped
the supply of Packard Merlins early in 1943, 600 of them were completed with
Allison engines and designated P-40Rs.
Between 1942 and 1943 the P-40Es were superseded by 1,300 improved
aircraft with 1,325-hp Allison V-1710-73 engines, called P-40Ks. The P-40M
was a similar, but lighter version of the P-40K with a carburetor air bypass
grille on the cowling just forward of the exhausts. The aircraft’s tail was
also slightly lengthened to improve directional stability. Both models were
designated Kittyhawk M.IIIs by the RAF.
In order to further improve the P-40’s performance, Curtiss introduced
additional weight-saving measures, including reducing the amount of fuel and
eliminating two of the wing-mounted .50-caliber guns. At the same time, the
designers improved rear visibility by increasing the glazing behind the
cockpit. Called the Kittyhawk Mk.IV by the British, the lightweight P-40N
Warhawk was the most-produced P-40 variant. With a top speed of 378 mph, the
P-40N also had the best performance of the production-model P-40s. The
5,219th and last P-40N was completed on November 30, 1944. In addition to
the USAAF, P-40Ns were used by the Dutch, Australians and New Zealanders in
Europe and the South Pacific, and many were supplied to the Soviet Union.
In 1944, Curtiss-Wright made a final attempt to improve the P-40 by
installing an enhanced 1,425-hp Allison V-1710-121 engine equipped with a
two-stage supercharger in a P-40K. A new-style radiator was also built into
the wing center section. The XP-40K was rebuilt three times. In its final
form, with a shallow chin air scoop, clipped wings and a bubble canopy, the
Curtiss fighter’s appearance was somewhat reminiscent of a P-51D Mustang.
The XP-40Q, as the new version was redesignated, was the fastest of the
Warhawks, with a top speed of 422 mph at 20,000 feet. Unfortunately, by the
time the XP-40Q was built, the more capable P-51D was already available in
large numbers. Only three were built, and only one was evaluated — and
rejected — by the USAAF.
One XP-40Q turned up in Cleveland, Ohio, for the Thompson Trophy Race
on September 1, 1947. Flown by Joe Ziegler, the Warhawk was excluded from
the race because it qualified 13th, and only 12 planes were supposed to be
allowed to compete. Ziegler started the race anyway, but on the 13th lap the
XP-40Q’s engine stopped. Ziegler was forced to bail out, breaking one of his
legs, and a woman spectator was injured by the jettisoned canopy. Thus ended
the career of the ultimate P-40.
The P-40’s performance was always regarded as inferior to its German
contemporaries, the Me-109 and Focke Wulf Fw-190, especially at altitudes
above 15,000 feet. It could also be outmaneuvered and outclimbed by the
Japanese Mitsubishi Zero. The availability of better fighters, such as the
P-38 Lightning, P-47 Thunderbolt and P-51 Mustang, rendered the Warhawk
obsolete by 1944. Nevertheless, many continued to be used in the South
Pacific and China-Burma-India theaters right up until the end of World War
II. Some P-40Ns were retained after the war by the Dutch East Indies Air
Force and the Nationalist Chinese Air Force. The last known instance of
P-40Ns’ being used in action was by the Dutch against Indonesian insurgents
in 1948.
The P-40N was not only the last production model of the Warhawk family
but also the last production fighter from Curtiss-Wright. Curtiss produced
several fighter prototypes in an effort to supersede the P-40, but none were
accepted for production due to the availability of more suitable existing
models, such as the North American P-51. The last Curtiss fighter was the
XP-87 Blackhawk, a postwar four-engine jet night fighter that was rejected
by the U.S. Air Force in favor of Northrop’s F-89 Scorpion. The company
still had several important military aircraft in production after the P-40
program was terminated, including the C-46 Commando transport, the SB2C
Helldiver dive bomber and the SC-1 Navy scout seaplane. However, Curtiss-Wright’s
dominance of the American fighter business, which had lasted since the early
1920s, ended with the P-40.
Although the P-40 was not the best fighter plane of its era, it was
among the most ubiquitous. Few aircraft have seen combat in as many
theaters, under as wide a variety of climactic conditions, or with as many
different air arms as the Warhawk. P-40s were in action from the Arctic to
the tropics, from the desert to the jungle, and from sea level to the
Himalayas. In addition to the U.S. Army Air Forces, Warhawks were used by
British, Australian, New Zealand, South African, Canadian, Dutch, Free
French, Soviet, Chinese, Egyptian and Turkish fighter units. Whether it was
known as the P-40, the Tomahawk, the Kittyhawk or the Warhawk, Curtiss-Wright’s
fighter was one of the truly classic combat aircraft of World War II.
This article was written by
Robert Guttman and originally published in the November 2000 issue of
Aviation History.
The "Tomahawk" Files
|
XP-40, P-40A, P-40B, P-40C |
Joe Baugher's Tomahawk files
The P-40 was the best known Curtiss-Wright airplane of World War
II. It was also one of the most controversial fighters of the war. It
was vilified by many as being too slow, lacking in maneuverability,
having too low a climbing rate, and being largely obsolescent by
contemporary world standards even before it was placed in production.
The inadequacies of the P-40 were even the subject of a Congressional
investigation. It gets regularly included on lists of the worst combat
aircraft of World War 2.
All of these criticisms certainly had some degree of validity, but it is
also true that the P-40 served its country well during the first year of the
war in the Pacific when very little else was available. Along with the P-39
Airacobra, the P-40 was the only American fighter available in quantity to
confront the Japanese advance during the first year of the Pacific War. It
helped stem the speed of the Japanese advance until more modern types could be
made available in quantity. The P-40 had no serious vices and was a pleasant
aircraft to fly, and, when flown by an experienced pilot who was fully aware
of its strengths and weaknesses, was able to give a good account of itself in
aerial combat. The P-40 continued in production long after later types were
readily available, the numbers manufactured reaching the third highest total
of American World War II fighters, after the Republic P-47 and the North
American P-51.
The P-40 was obsolete by European standards even
before the first prototype flew, and it never did catch up. Its initial
inadequacies in the form of low firepower and lack of self-sealing fuel tanks
or armor were a reflection of mid-'thirties USAAC requirements which were
outmoded. The P-40 had been developed as basically a low-altitude
close-support fighter under mid-1930s US tactical concepts which envisaged
more need for low-level ground support operations than for high-altitude
interceptions. The military doctrine of the "ascendancy of
bombardment over pursuit" was dominant in 1937 when the P-40 first appeared.
This doctrine assumed that the prospect of high-altitude enemy air attack on
the USA was extremely remote, with coastal defense and ground attack in the
defense of US territory being seen as the the main tasks for any future
fighter aircraft. Low-altitude performance and rugged construction received
priority over high-altitude capabilities.
During the war, the Senate Special Committee to Investigate the National
Defense Program (usually known as the "Truman Committee", after its chairman,
Senator Harry Truman of Missouri) criticized the P-40 on several accounts,
particularly on the original volume purchase of an inadequate design and its
continued production long after later designs were readily available. However,
they finally concluded that this was not brought about by any undue favoritism
to Curtiss.
Some indication of the enormous P-40 production program undertaken by
Curtiss can be assessed by its claim on factory floor space and manpower.
During 1941, the Curtiss Airplane Division expanded its manufacturing area by
400 percent. The total work force was 45,000. This expansion included two new
plants, one at Buffalo, New York and the other at Columbus, Ohio, to
supplement the original Curtiss plant in St.Louis, Missouri. At the peak of
wartime production, the entire Curtiss Airplane Division complex of factories
was producing sixty aircraft A DAY!
The origin of the P-40 can be traced back to the
Curtiss P-36 (Model 75) fighter, which was powered by a radial, air-cooled
engine. A step in the direction toward what was eventually to
emerge as the P-40 was the XP-37, which was described in an earlier post. The
P-36 design was reworked to incorporate the Allison V-1710 liquid-cooled
V-type engine, resulting in the XP-37. The XP-37 was equipped with a General
Electrc turbosupercharger, and featured a cockpit pushed very far to the rear.
Thirteen YP-37 service-test aircraft were built, but problems with the
turbosupercharger caused the development of the P-37 to be abandoned in favor
of a less complex and more straightforward conversion of the P-36 for the
Allison V-1710 engine.
Realizing that the radial-engined P-36A was at the
limit of its development, Curtiss designer Donovan Berlin got USAAC permission
in July 1937 to install a 1150 hp Allison V-1710-19 liquid-cooled engine with
integral supercharging in the 10th P-36A (Serial No 38-10). This
project was given the company designation of Model 75P, and the USAAC gave the
project a new fighter designation, XP-40.
The XP-40 flew for the first time on October 14,
1938, with Edward Elliot at the controls. Armament was two 0.50-inch machine
guns located in the upper fuselage deck and synchronized to fire through the
propeller arc, standard armament for US pursuit aircraft at the time. Wing
racks could be fitted for six 20-pound bombs. A small oil cooler
was located beneath the pointed nose. The air intake for the single-stage
supercharger was mounted on top of the engine cowling between the two machine
guns, but during tests it was replaced by a long cowled intake duct which
became characteristic of all the early P-40 production models. Initially, the
coolant radiator was placed under the fuselage aft of the wing, but it was
gradually moved forward until it finally ended up located underneath the
extreme nose. The radiator intake was redesigned to include an oil cooler and
two coolers for the ethylene/glycol engine coolant. The initial XP-40 had a
single exhaust port on each side of the fuselage, but in its final form it had
six separate exhaust ports on each side. The initial XP-40 had inherited from
the P-36 a set of mainwheel fairing plates which covered the mainwheels when
they retracted into their wing wells, but these were eventually deleted and
replaced by two small doors which closed over the wheel struts upon
retraction.
The maximum speed of the XP-40 was 342 mph at 12,200 feet at a gross
weight of 6260 pounds. This was faster than the Hawker Hurricane, but slower
than the Spitfire or the Bf 109E. Empty weight was 5417 pounds, and
fully-loaded weight was 6870 pounds. Range was 460 miles at 299 mph with 100
gallons of fuel. With 159 gallons of fuel at 200 mph, a range of 1180 miles
was claimed, almost twice that of the contemporary Hurricane, Spitfire, and Bf
109E. Wingspan was 37 feet 4 inches, wing area was 236 square feet, length was
31 feet 1 inch, and height was 12 feet 4 inches. The wingspan and wing area
were to remain the same throughout the entire history of the P-40 production
run.
In the late 1930s, the USAAC was planning to expand its force, and on
January 25, 1939. manufacturers were invited to submit proposals for pursuit
aircraft. The Army was still thinking in terms of low-altitude, short-range
fighters. Among the contenders were the Lockheed XP-38, the Bell XP-39, the
Seversky/Republic XP-41 (AP-2) and XP-43 (AP-4), and no less than three planes
from Curtiss, the H75R, XP-37, and XP-42.
Although the XP-40 could not match the performance (especially at altitude) of
the turbosupercharged types, it was less expensive and could reach quantity
production fully a year ahead of the other machines. In
addition, the XP-40 was based on a already-proven airframe that had been been
in production for some years. Consequently, on April 26, 1939, the Army
adopted a conservative approach and ordered 524 production versions under the
designation P-40 (Curtiss Model 81). At that time, it was the largest-ever
production order for a US fighter, and dwarfed the service test orders placed
that same day for YP-38 and YP-39 fighters. A couple of weeks later, 13 YP-43s
were also ordered.
The P-40 was similar to the final XP-40
configuration except for 1040 hp V-1710-33 (C15) engines and provisions for
the mounting of one 0.30-inch machine gun in each wing. Flush
riveting was used to reduce drag. Armor, bulletproof windshields, and
leakproof fuel tanks were added in service. The P-40 was a relatively clean
design, and was unusual for the time in having a fully retractable tailwheel.
The first flight of a P-40 (Ser No 39-156) was on April 4, 1940. Maximum
speed was 357 mph at 15,000 feet, service ceiling was 32,750 feet, and initial
climb rate was 3080 feet per minute. An altitude of 15,000 feet could reached
in 5.2 minutes. The length of the P-40 was 31 feet 8 3/4 inches, which became
standard for all early models. Weights were 5376 pounds empty, 6787 pounds
gross, and 7215 pounds maximum.
Deliveries of the P-40 to Army units began in June of 1940. Three of the
P-40s were used for service testing, the USAAC contract making no provisions
for the standard practice of supplying YP models.
Foreign air forces were beginning to take notice of the P-40, and in May
of 1940, the Armee de l'Air of France placed an order for 140 H-81A (export
model of the P-40).
Only 200 of the initial P-40 order were actually completed as P-40s.
Serials were 39-156/280 and 40-292/357. The remaining 324 aircraft of the
order had their delivery deferred to enable Curtiss to expedite the delivery
of the 140 H-81As to France. However, none of these actually reached France
before the Armistice in June 1940, and the contract was taken over by the
Royal Air Force as Tomahawk I.
16 P-40s were sent to the Soviet Union after the German invasion.
The P-40 lacked such things as armor for the pilot, self-sealing fuel
tanks, and a bulletproof windshield, so it was not considered as being
suitable for combat. On October 22, 1942, the P-40s still in USAAF service
were ordered restricted from combat duty and were redesignated RP-40.
The P-40A designation was skipped in the initial designation
assignments. However, it was applied retroactively to P-40 Ser No 40-326 when
it was converted to a camera-carrying photographic reconnaissance model at
Bolling Field in March of 1942.
The P-40B (Model H81B) differed from the P-40 in
having an extra 0.30-inch machine gun in each wing. The engine
was still the V-1710-33. In September 1940, 131 P-40Bs were procured by the
Army to replace the deferred P-40s. Serials were 41-5205/5304 and
41-13297/13327. The first P-40B flew on March 13, 1941. The P-40B retained the
same dimensions of the P-40, but weight was
increased to 5590 pounds empty, 7326 pounds gross, and 7600 pounds maximum
loaded. Because of the additional weight, the P-40B had an inferior
performance to the P-40, maximum speed being 352 mph, service ceiling being
32,400 feet, and initial climb rate being 2860 feet per minute. Normal range
was 730 miles, but a maximum range of 1230 miles could be attained at the
minimum cruise settings.
The export equivalent of the P-40B was the Tomahawk IIA (Model H81-A2).
They differed from the American version by having the wing guns replaced by
0.303-inch Brownings. 110 were produced for the RAF. RAF serials were
AH881/990. 23 of these planes were transferred to the USSR, and one (AH938)
went to Canada as an instructional airframe.
The initial P-40 order was finally completed with 193 P-40Cs (company
designation H81-B). Serials were 41-13328/13520. The first flight of a P-40C
was made on April 10, 1941. The P-40C retained the 1150 hp Allison V-1710-33
engine, but was fitted with a new fuel system with 134 gallons in new tanks
with improved self sealing. In addition, provisions were made for a 52-gallon
drop tank below the fuselage. The P-40C had a SCR-247N radio instead of the
SCR-283. These additions produced yet another upward crawl in the weight ---
the weights for the P-40C were 5812 pounds empty, 7459 pounds gross, and 8058
pounds maximum loaded. Consequently, the performance continued to degrade.
Maximum speed was 345 mph at 15,000 feet. Normal and maximum ranges were 730
and 945 miles respectively. Service ceiling was 29,500 feet, and initial climb
rate was 2650 feet per minute. Dimensions were wingspan 27 feet 3 1/2 inches,
length 31 feet 8 1/2 inches, height 10 feet 7 inches, wing area 236 square
feet.
The export equivalent of the P-40C was the
Tomahawk IIB (Model H81-A2). A total of 930 were built. RAF serials were
AH991/999 (all to USSR), AK100/570 (36 to China), AM370/519 (64 to China), and
AN218/517. 100 of these planes, unofficially designated H81-A3, were
transferred to China where they were used by the American Volunteer Group ---
the famous "Flying Tigers". 23 went to the USSR, and unspecified
numbers went to Turkey and Egypt. The rest were used extensively by the RAF
and South African Air Force in the North African theatre.
 |
|
Much-rebuilt Tomahawk IIB, recovered
from Russia and painted in the colors of Bob Neale of the AVG. The plane
is on display at the Naval Aviation Museum, Pensacola. |
At a very early stage, the Curtiss P-40 attracted the attention of
foreign air forces. On May 10, 1939, the French ordered 140 export versions of
the P-40 for the Armee de l'Air. These aircraft were designated Hawk 81-A1 by
the manufacturer. The Hawk 81-A1s were identical to the US P-40 except that
they had French instruments and equipment and were equipped with
reverse-movement "French-fashion" throttles. The first of the French-ordered
H81-A1s flew on June 6, 1940, and a few were actually completed with French
markings. However, before any of their H81-A1s could be delivered, France
surrendered. Britain agreed to take over the
entirety of the French order, and gave the H81-A the name Tomahawk I in RAF
service. RAF serials were AH741/840 and AH841/880.
The USAAC had agreed to defer deliveries of their P-40s so that the
Tomahawk Is could be supplied to Britain as soon as possible. The first
Tomahawk Is reached England in September of 1940. The two 0.5-inch machine
guns in the nose were retained, but they were supplemented by four
wing-mounted 0.303-inch Browning machine guns in place of the 7.5-mm FN-Brownings
specified by the French. Such was the urgency of their delivery to Britain
that many of the 140 machines still had French instruments and bore cockpit
lettering in French when they arrived.
However, Britain quickly concluded that
these planes were not suitable for combat, since they lacked armor protection
for the pilot, armor-glass windshields, or self-sealing fuel tanks.
Nevertheless, since a German invasion was feared to be imminent, they were
actually issued to several operational squadrons.
However, the Hun never invaded England, and so the Tomahawk Is were used
only for training roles within Britain. Overseas, the first Desert Air Force
squadron to be equipped with Tomahawks was No. 112 which exchanged its Gloster
Gladiators for the Curtiss fighter. No 112 Squadron became famous for its
"shark's tooth" insignia on the engine cowling, and this scheme was later
adopted by the American Volunteer Group in China. AH774,793, and 840 were sold
to Canada for use as instructional airframes, but they retained their RAF
serials.
The Tomahawk IIA (Model H81-A2) was equivalent to the US P-40B. It had
protective armor and externally-covered self-sealing tanks. 110 were built for
the RAF under a direct-purchase contract. It carried two 0.30-inch machine
guns in the wings in addition to the two 0.50-in guns in the fuselage. A
British radio was fitted. RAF serials were AH881/990. AH938 was transferred to
Canada as an instructional airframe. 23 of these planes were transferred to
the USSR.
The Tomahawk IIB (Model H81-A2) was generally
equivalent to the US P-40C. It had four 0.303-inch Browning machine guns in
the wings in addition to the two nose-mounted 0.50-in guns.
[But see my and Erik Shilling's comments on this subject in the facsimile
Pilot's Notes on this
website. -- DF] Whereas the Tomahawk IIA had a British radio, the Tomahawk
IIB had US equipment. A total of 930 of these planes were produced in four
lots. RAF serials were AH991/999, AK100/570 (36 of this batch were shipped to
China and were selected at random with no particular sequence), AM370/519 (64
were shipped to China, selected at random), and AN218/517. They were used
extensively by the RAF and the South African Air Force in North Africa
starting on June 16, 1941.
After the German invasion of the USSR in June 1941, one hundred and
ninety-five Tomahawk IIBs were shipped to the USSR, some from the USA, others
selected from the reserve forced based in the United Kingdom in anticipation
of the German invasion which never came. These Russian Tomahawks went into
action on the Moscow and Leningrad fronts in October 1941, and were the first
US-built planes to be used by the Russians in the new battle area.
An unspecified number of Tomahawk IIBs were sent to bolster Turkish
neutrality in November 1941. Turkey was supplied with planes from both the
Allies and the Axis during World War II.
The Tomahawk IIs were active in the Middle East from October of 1941
onward. They shared in the strafing of the retreating Axis troops. The ability
of the Tomahawk to absorb an incredible amount of punishment became almost
legendary. They served with Nos 2, 26, 73, 112, 136, 168, 239, 241, 250, 403,
414, 430 and 616 Squadrons of the RAF. They also served with Nos 2 and 4
Squadrons of the South African Air Force and No 3 Squadron of the Royal
Australian Air Force. At low altitudes, the Tomahawk II was actually superior
to the Bf 109, but this advantage rapidly disappeared when combat took place
at altitudes above 15,000 feet. The weight which handicapped the performance
of the Tomahawk did have one tangible benefit --- the rugged structure could
absorb a terrific amount of battle damage and still allow the airplane to
return to base. Although generally outclassed by the Bf 109, the Tomahawk was
a capable fighter in the hands of experienced pilots such as Neville Duke.
Wing Commander Clive Caldwell of the RAAF scored more than twenty victories
while flying a Tomahawk in the Middle East. However, much of the opposition to
the Tomahawk was provided by obsolescent fighter biplanes (e.g. Fiat CR-42)
and underpowered, lightly armed fighter monoplanes such as the Fiat G-50 of
the Regia Aeronautica. It had difficulty with the more advanced Macchi C-202
Folgore.
100 of the RAF Tomahawk IIBs were released to
China and served with the American Volunteer Group (AVG) --- the famous
"Flying Tigers". Company records list them as Model H81-A3. The Tomahawk IIB
was more-or-less equivalent to the P-40C, but some sources list the Flying
Tiger Tomahawks as being equivalent to the P-40B. There is confusion on this
point.
It is with the Flying Tigers that the P-40 achieved immortality.
Newly-promoted to Brigadier General in the Chinese Army, Claire Chennault went
to the USA in November 1940 to recruit pilots for the AVG. The AVG came into
existence in August 1941. General Chennault ordered 100 P-40s through a loan
from the US government. By the time of Pearl Harbor, some 80 American pilots
were serving with the AVG based at Kunming and Mingaladon. Contrary to popular
understanding, the AVG did not actually enter combat until AFTER Pearl Harbor.
The famous "shark's teeth" marking did not originate with the Flying Tigers,
but was copied from the markings used by the Tomahawks of the RAF's No. 112
Squadron in North Africa.
The AVG drew first blood on December 20, destroying six out of ten
attacking Japanese bombers. When the AVG encountered the Japanese Zero for the
first time, they initially underestimated the maneuverability of their
opponent, and they lost two pilots on December 23. [Actually, the Dec. 20
encounter ended with three Kawasaki Ki-48 "Lily" bombers shot down and one
force-landed in Vietnam. The retractable-gear aircraft that fought the AVG
were Nakajima Ki-43 Hayabusa fighters, later called "Oscar" in the west. --
DF] It was soon learned that it was wise not to mix it up with the Zero on
a one-to-one basis because of the inferior maneuverability and climb rate of
the Curtiss, but instead to use the P-40's superior speed and diving ability
to advantage. The most effective tactic against the Zero was a diving pass
followed by a rapid departure from the scene. The P-40 gained a reputation for
ruggedness which enabled many an AVG pilot to return safely home after his
plane was damaged in combat.
by Joe Baugher