DS> Anyone out there have details and/or experience with the F-7
DS> Tigercat? I've seen a model of one but am having trouble finding any
DS> more information about this plane.
Daniel, here's some additional information I dragged out of the
basement for you regarding the F7F Tigercat, as well as the later F11F Tiger
and Supertiger
The Grumman F7F Tigercat
The F7F Tigercat was ordered by the Navy on the same day in June of
1941 that it ordered the F6F Hellcat. The Navy had been studying air combat
in Europe the previous two years, and concluded that the things that mattered
most were engine power, armament, protective armor and self-sealing tanks. At
a time when the average U.S. Navy fighter had 1,000 hp and two machine guns,
the Bureau of Aeronautics asked Grumman to build a fighter with more than
4,000 hp and a weight of fire more than 100 times as great.
The F6F project advanced quickly due to its more modest goals, resulting
in the introduction into battle of the war-winning Hellcat in early 1943. The
F7F project, being far more ambitious, meant that the first Tigercat
prototype
did not fly until December of 1943, and the first service deliveries did not
take place until October of 1944. Tigercats were deployed to Guam and Okinawa
in
May of 1945 and saw limited combat in the waning days of the war.
Had the invasion of Japan been necessary, the tremedous versatility of the
F7F design would probably have resulted in its becoming the Navy's single
most
effective and valuable aircraft. In 1945, the F7F Tigercat was the fastest
aircraft in the sky at low altitude, was almost as fast as the Mustang at
high altitude, had an absolutely devastating firepower of four 20-mm cannon
(200 rpg) and four .50 caliber machine guns (300 rpg), could outmaneuver a
P-38 or a Japanese "Nick" (two contempory twin-engine designs) and could
outclimb everything but an F8F Bearcat. As a fighter bomber, it could be
equipped with a torpedo, or two 1,000 lb bombs, or six rockets. The rugged,
battle-tested design of its two air-cooled 2,100 hp radial Pratt & Whitney
R-2800-22W Double Wasp engines and excellent protective armor meant that it
could sustain battle damage that no other fighter could withstand and still
get its pilot back home. In addition, the F7F was roomy enough to incorporate
a second seat and a radar operator, resulting in a night fighter as capable
as the newest and fastest USAAF model - the P-61C Black Widow. With the
veterans of Japanese airforce largely shot out the sky, the emphasis for
Naval air missions would have shifted from air-to-air combat to ground attack
sorties such as attacks on kamikazi aerodomes, interdiction of rail and
other ground transport facilities and strikes against coastal shipping, all
for which the F7F Tigercat was imminently suited.
As it turned out, of course, the Tigercat as an air-to-air fighter wound up
only a footnote in the history of aviation. Like so many other excellent
aircraft of its era, the Tigercat as an air superiority fighter was made
obsolete by the dawn of the age of jets. By the time the Navy found itself in
air-to-air combat five years later in the skies over Korea, it was meeting
that challenge with its first jets, most notably the Tigercat's (and
Bearcat's) direct successor, the Grumman F9F Panther. But the Tigercat lived
on in Korea as the Navy's and Marine's most advanced night-fighter until
replaced late in that war by the jet-powered F3D Skyknight. The Tigercat also
was used heavily by the shore-based Marines in Korea as a very capable
ighter
-bomber, supplementing the work of F4U Corsairs, AD-1 Skyraiders, F9F
Panthers
and F2H Banshees in critically important Naval and Marine close-air and
interdiction strikes against the North Korean and Chinese Communists.
e-mail: phartl@siopmag.ucsd.edu
Phone: 619-587-8878 (home)
619-534-6531 (office)
The Grumman F11F Tiger and F11F-F1 SuperTiger
The Grumman F11F Tiger's two greatest claims to fame were both results
of peacetime activities. To many of us "boomers" who grew up in the fifties
and sixties, the F11F Tiger was THE Blue Angels jet. The Angels flew the
Tiger from 1957 to 1969, the longest period for any aircraft, a period which
corresponded to the duration of conscious childhood for me. Indeed, when the
Angels finally changed over to F-4J Phantoms in 1969, I felt as if I'd lost
an old friend! The Tiger's other claim to fame is not nearly as glorious,
however, as it was the only U.S. military aircraft known to have shot itself
down! This decidedly inglorious incident occurred in September 1956 when
Grumman test pilot Tom Attridge was test firing the craft's 20-mm cannon in a
dive and somehow managed to catch up with his own projectiles! There were at
least three hits, one on the windshield, one on the nose cone and one on the
starboard intake which apparently was subsequently ingested by the engine.
Attridge managed to get out of the aircraft after a crash landing.
The F11F Tiger started out as a proposed design modification of the
F9F Cougar to incorporate the newly discovered "area rule" concept to reduce
transonic drag and push the jet through Mach 1. The plan soon evolved into a
completely new design, and by spring 1953, the F11F project had begun. The
area rule stated that the total frontal cross-sectional area of the aircraft
must be maintained down the length of the aircraft. Thus, where wings and
tail surfaces joined the fuselage, the fuselage cross section must be reduced
to allow for the increase in frontal area presented by those components. This
gave rise to the "coke bottle" fuselage shapes of this and other aircraft of
its era (most notably Republic's F-105 Thunderchief). The design worked. The
F11F exceeded Mach 1 in level flight soon into its test program in the fall
of 1954, even though the specified engine was not yet ready. When the F11F
finally was properly engined, it was with a 7,400/10,500 lb thrust
dry/afterburning J65-W-18, which gave it top speed of 754 mph and a rate of
climb about 10,000 ft/min.
However, rapid advances in jet engine design during this period made
this performance almost obsolete before the F11F could reach its destination
squadrons. Vought, McDonnell, Douglas and others were all vying for a shot
at becoming the Navy's number one fighter contractor, and this time Grumman
had taken a misstep. Grumman of course soon realized this, and quickly drew
up plans for a Super Tiger, designated F11F-1F, to be powered by a
9,600/15,000 lb thrust dry/afterburning General Electric YJ79-GE-3. This
version of the F11F first flew in May 1956 and attained a speed of Mach 2
and set an altitude record of 80,250 feet a year later. But it was too late.
Vought had in the meantime won the competition for first-line fighter with
its
excellent F8U Crusader, and McDonnell-Douglas sealed up all possible chances
for a Grumman comeback shortly thereafter with its superb F4 Phantom.
All in all, just 200 or so F11F Tigers served with the Navy as front-line
fighters from March 1957 to April 1961. If the F11F-1F Super Tiger had been
available a bit sooner, these would almost surely have seen action over
Vietnam in the middle and late sixties, but this was not to be. Grumman had
lost out, and for the first time in 28 years, since even before the F4F
Wildcats of Midway and Guadalcanal fame, no Grumman fighters were protecting
the fleet. Not until 1974 did Grumman make its fighter comeback with the
F-14A Tomcats. 20 years later, F-14 Tomcats still patrol the skies over the
fleet as its first-line fighter.
Specifications F11F-1 F11F-1F
Dimensions:
Span 31'7" 31'7"
Length 46'11" 48'9"
Height 13'3" 14'5"
Wing Area, sq. ft. 250 250
Weights (lb):
Empty 14,330 16,457
Loaded 21,280 23,360
Max 24,078 26,086
Performance:
Max speed, mph 754(s.l.) 1,325 (35K ft)
Cruise speed, mph 578 580
Climb rate, ft/min 10,000* 30,000*
Service Ceiling, ft. 42,000 50,300
Normal range, miles 1,275 1,136
Powerplant, type J65-W-18 YJ79-GE-8
Powerplant, lb. thrust 7,400/10,500 9,600/15,000 (dry/afterburning)
Armament: 4x 20mm cannon 4x 20mm cannon
Weapons load: 4,000 lb. 2,000 lb.
Weapons types: Bombs, 5-in HVAR or HPAG rockets, Sidewinder
(* Rene Francillon gives unrealistically low climb rates for both Tiger
versions, so I have put down estimates based on power/weight ratios and
comparisons with other similar aircraft such as the F3H Demon and F8U
Crusader. His numbers are 5,130 and 8,950 ft/min.)
Reference Source:
"Grumman Aircraft Since 1929" by Rene J. Francillon
e-mail: phartl@siopmag.ucsd.edu
Phone: 619-587-8878 (home)
619-534-6531 (office)
Have Fun,
Christopher
... "Do you suppose we've died and gone to the Army?" -- Trapper
___ Blue Wave/DOS v2.30 [NR]
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* Origin: Odyssey BBS (1:3603/73)
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