Grumman
F9F-5 Panther
The F9F-5
was numerically the most important of the Panther variants. It
had the longer fuselage and revised tail surfaces of the F9F-4,
but was powered by the Pratt & Whitney J48 turbojet, a license-built
version of the Rolls-Royce Tay.
The XF9F-5
prototype was the 100th production airframe (F9F-2 BuNo 123085),
modified and re-engined. It flew for the first time on December
21, 1949. It actually preceded the XF9F-4 into the air by almost
half a year.
616 F9F-5s
were delivered to the Navy and Marine Corps between November 1950
and January 1953. They were all powered by the Pratt & Whitney
J48-P-6 or P-6A, rated at 7000 lb.s.t. wet. The F9F-5 had four
external store pylons underneath each wing, with the three outboard
pylons being stressed to carry bombs of up to 500 pounds in weight.
Maximum external load was 3465 pounds.
During the
course of production, an anti-stall fence was added just outboard
of the wing roots to control the airflow and reduce landing speed.
Many of the F9F-4s were retrofitted with J48 engines and thus
became indistinguishable from F9F-5s.
The first F9F-5 deliveries took place on November 5, 1950. Most
squadrons which had been equipped with F9F-2s were re-equipped
with the later F9F-5.
In November
1951, the F9F-5 replaced the F9F-2s of the Blue Angels flight
demonstration team. This team began to convert to the swept-wing
F9F-6 Cougar in 1953, but it turned out that these Cougars were
urgently needed by the fleet and the team had to be hastily re-equipped
with overhauled F9F-5s. The F9F-5s served with the Blue Angels
until 1954, when they were finally replaced by F9F-8 Cougars.
The first
F9F-5s entered combat in Korea in October of 1952, serving aboard
the USS Oriskany (CVA-34) with the reserve squadrons VF-781 and
VF-783. They were also flown by VF-51, VF-52, VF-53, VF-111, VF-153,
and VF-154 during the latter stages of the Korean War. They provided
the backbone of the Navy's carrier-based jet-powered ground attack
capability during the last year of the Korean War.
One of the
more significant experiments carried out by the F9F-5 was the
performance of early midair refuelling tests. F9F-5 BuNo 125240
was fitted in 1952 with a refuelling probe in the nose for trials
with a North American XAJ-1 attack plane modified as a tanker.
These tests were so successful that the Navy eventually decided
in September of 1955 to require that all of its jet-powered fighters
and attack aircraft would henceforth be equipped for midair refuelling.
As the Panther
began to be replaced in active service by more advanced types,
surviving F9F-5s were modified as F9F-5K remotely-controlled drones
or as F9F-5KD drone directors. In the F9F-5KD, the nose guns were
removed and were replaced by radio control equipment. In 1962,
the Defense Department introduced the new Tri-Service designation
scheme under which the separate USAF/Navy designations were replaced
by a new unified designation system. This required that all existing
Navy aircraft be redesignated. By this time, the only Panthers
remaining in Navy service were the F9F-5KD drone directors, which
were redesignated DF-9E. The last DF-9Es were struck off charge
in the mid-1960s.
Serials
of Grumman F9F-5 Panther:
123085 Grumman XF9F-5 Panther
126000/126256 Grumman F9F-5 Panther
126627/126669 Grumman F9F-5 Panther
125080 Grumman F9F-5 Panther
125082 Grumman F9F-5 Panther
125228/125313 Grumman F9F-5 Panther
125414/125443 Grumman F9F-5 Panther
125489/125499 Grumman F9F-5 Panther
125533/125648 Grumman F9F-5 Panther
125893/125912 Grumman F9F-5 Panther
125949/125999 Grumman F9F-5 Panther
Specification
of the Grumman F9F-5 Panther:
Engine: One
Pratt & Whitney J48-P-4/P-6A turbojet rated at 6250 lb.s.t.
Performance: Maximum speed 604 mph at sea level, 579 mph at 5000
feet, 543 mph at 35,00 feet. Cruising speed 481 mph. Stalling
speed 132 mph . Initial climb rate 5090 feet per minute. Service
ceiling 42,800 feet. Range 1300 miles.
Dimensions:
wingspan 38 feet 0 inches, length 38 feet 10 1/2 inches, height
12 feet 4 inches, wing area 250 square feet. Weights: 10,147 pounds
empty, 17,766 pounds gross, 18,721 pounds maximum takeoff. Internal
fuel capacity 1003 US gallons. Armament: Four 20-mm cannon in
the nose. Eight underwing hardpoints which could accommodate a
total underwing load of up to 3465 pounds of bombs and rockets.
Sources:
1. United
States Navy Aircraft Since 1911, Gordon Swanborough and Peter
M. Bowers, Naval Institute Press, 1990.
2. The American Fighter, Enzo Angelucci and Peter Bowers, Orion,
1987.
3. Grumman Aircraft Since 1929, Rene J. Francillon, Naval Institute
Press, 1989.
4. American Combat Planes, 3rd Enlarged Edition, Ray Wagner, Doubleday,
1982.
Panther
in Service with US Navy and US Marine Corps
The F9F-2
and -3 initial production versions of the Panther were declared
service-ready in the spring of 1949. However, because of initially-slow
deliveries of the Pratt & Whitney J42, the Allison J33-powered
F9F-3 was actually the first to enter service. F9F-3s were first
delivered to VF-51 at NAS San Diego on May 8, 1949.
The F9F-2s
first went to the Blue Angels flight demonstration team based
at NAS Pensacola on August 20, 1949, and a few days later F9F-2s
went to VMF-115 at MCAS Cherry Point in North Carolina. The first
Navy squadron to get the F9F-2 was VF-11 at NAS San Diego, which
first received the machines in the early autumn of 1949.
When war came
to Korea on June 25, 1950, VF-51 and VF-52 loaded their F9F-2
Panthers aboard the USS Valley Forge (CV-45) and put to sea. Panthers
from VF-51 were first in action on July 3, 1950, providing escort
for a strike against an airfield at Pyongyang. Ens E. W. Brown
and Lt(jg) L. H. Plog shared credit for downing a Yak-9, scoring
the first kill credited to a Navy jet fighter.
In November
of 1950, the swept-wing MiG-15 began to appear over northern Korea.
Although powered by derivatives of the same Rolls-Royce Nene as
was the F9F-2, the MiG-15 had a much better performance because
of its swept wings and lighter weight. Nevertheless, the Panther
was able to defeat the MiGs in the few air-to-air encounters that
did take place. The first MiG-kill by a F9F Panther was by Cdr
W. T. Amen of VF-111 on November 9, 1950. Four more MiG-15s were
downed by Panthers before the Korean War ended, with no Panthers
being lost in air-to-air combat.
The first
Marine Corps Panthers appeared in combat in Korea in December
of 1950. These were F9F-2Bs serving with VMF-311, helping to support
the withdrawal of troops from the Chosin Reservoir.
Most Panthers
serving in Korea flew air-to-ground close-support missions, air-to-air
action being quite rare. The first Navy F9F-2Bs appeared in combat
on April 2, 1951, when VF-191 flew an attack on railway bridges
near Songjin.
The more capable
F9F-5 first appeared in Korea in October of 1952, flown initially
by VF-781 and VF-783 operating off the USS Oriskany (CVA-34).
F9F-5s also served with VF-51, VF-52, VF-53, VF-111, VF-153, and
VF-154.
The Marine
Corps flew F9F-2Bs, F9F-4s and F9F-5s in Korea, exclusively in
the ground support role. Active and reserve Marine Corps squadrons
that flew the Panther included VMF-115, VMF-122, VMF-211, VMF-213,
VMF-214, VMF-223, VMF-224, VMF-232, VMF-234, VMF-235, VMF-311,
VMF-312, VMF-314, VMF-324, VMF-334, and VMF-451, plus the training
squadrons VMFT-10 and VMFT-20.
F9F-2P unarmed reconnaissance aircraft were deployed by VC-62
aboard the USS Princeton in December of 1950. Two years later,
they were replaced by F9F-5Ps. Two Marine Corps reconnaissance
(VMJ-1 and VMJ-3) squadrons flew F9F-5Ps. VMJ-3 was still flying
F9F-5Ps when the squadron was redesignated VMCJ-3.
Throughout
the early 1950s, Panthers served extensively with active and reserve
units of both the Atlantic and Pacific Fleets. They provided the
mainstay of the Navy's jet-powered carrier-based air-to-ground
capability. The Panthers were phased out of active service with
the Navy in 1956, but they remained with training units until
1958. The last Marine Panther units were the two reserve squadrons
VMF-213 and VMF-234, which were based at Minneapolis. These Panthers
were retired in 1958.
Many of the
surplus Panthers were used as drones or as drone directors under
the designation F9F-5K or F9F-5KD. In 1962, the Defense Department
eliminated separate designations for Navy aircraft, and ordered
that all Navy planes be redesignated under the new Tri-Service
unified designation scheme. The Panther/Cougar was assigned the
designation F-9 under the new system. By this time, the only Panthers
left in service were the F9F-5KD drone directors. These were redesignated
DF-9E. The last of these DF-9Es was stuck off charge in the mid-1960s.
Sources:
1. United
States Navy Aircraft Since 1911, Gordon Swanborough and Peter
M. Bowers, Naval Institute Press, 1990.
2. The American Fighter, Enzo Angelucci and Peter Bowers, Orion,
1987.
3. Grumman Aircraft Since 1929, Rene J. Francillon, Naval Institute
Press, 1989.
4. American Combat Planes, 3rd Enlarged Edition, Ray Wagner, Doubleday,
1982.
5. E-mail from Ben Marselis
Grumman
F9F-5P Panther
The F9F-5P
was a specially built unarmed photographic reconnaissance version
of the F9F-5. Unlike the F9F-2Ps, which were modified from existing
F9F-2 airframes, the F9F-5Ps were built from scratch as unarmed
photo-reconnaissance aircraft. 36 were built. The modified nose
had the armament replaced by a housing for vertical and oblique
cameras. The overall length was 40 feet as compared to 38 feet
10 1/2 inches for the standard F9F-5.
The F9F-5P
was deployed with a detachment of VC-61 aboard the USS Princeton
during late 1952, supplanting the earlier F9F-2P.
F9F-5P BuNo
126275 is on display at the USN Pensacola Air Museum.
Grumman
F9F-5P Panther serials:
125314/125321 Grumman F9F-5P Panther
126265/126290 Grumman F9F-5P Panther
127471/127472 Grumman F9F-5P Panther
Grumman
F9F-4 Panther
The F9F-4 Panther (and the F9F-5 that was developed in parallel
with it) differed from the previous F9F-2/F9F-3 in having a 19.5-inch
longer forward fuselage that made it possible to increase the
internal fuel capacity from 923 to 1003 gallons. In addition,
the height and area of the vertical tail surfaces were increased.
The F9F-4 was powered by the uprated Allison J33-A-16, capable
of delivering 6250 pounds of thrust dry and 6950 lb.s.t. with
water injection.
The 99th and
101st production airframes (F9F-2s BuNos 123084 and 123086) were
modified as the XF9F-4 prototype and the static test airframe.
123084 flew for the first time on July 5, 1950, powered by a 6250
lb.s.t. Allison J33-A-16 turbojet.
The F9F-4
was equipped with four external store pylons underneath each wing.
The three outboard pylons were stressed to carry bombs of up to
500 pounds in weight, bringing maximum external load to 3465 pounds.
The J33-A-16
turbojet proved to be unreliable in service, and many F9F-4s were
delivered to the Navy as J48-powered F9F-5s, and most of the others
were re-engined with J48-P-6As once they entered service. They
thus became indistinguishable from F9F-5s.
In early 1954,
F9F-4 BuNo 125081 was modified as a test bed for a high-lift boundary
layer control system.
Serials
of F9F-4 Panther:
123084 Grumman XF9F-4 Panther
123086 Grumman XF9F-4 Panther
125081 Grumman F9F-4 Panther
125156/125227 Grumman F9F-4 Panther
125913/125948 Grumman F9F-4 Panther
Grumman
F9F-3 Panther
The F9F-3 was developed in parallel with the F9F-2. It differed
from the F9F-2 in being powered by the Allison J33 turbojet, which
was approximately the same size as the J42 but was somewhat less
powerful. The J33 had been planned as a second-source powerplant
for the Panther in case the program to produce the Nene under
license in the USA as the J42 proved unsuccessful. The first flight
of the XF9F-3 (BuNo 122476) took place on August 16, 1948. It
was powered by a 4600 lb.s.t. Allison J33-A-8 jet engine.
54 J33-powered
F9F-3s were delivered to the Navy by Grumman between August 1948
and November 1949. They came off the production line in parallel
with the J-42-powered F9F-2. Because of initially slow deliveries
of J42 engines for the F9F-2, the F9F-3 was actually the first
Panther version to enter service with the Navy, when F9F-3s replaced
the FJ-1 Furies of VF-51 in May of 1949.
However, the
J33 turned out in service to perform less well than the J42. In
October 1949 virtually all F9F-3s were re-engined with 5750 lb.s.t.
Pratt & Whitney J42 turbojets, and thereby became indistinguishable
from the F9F-2. No further F9F-3s would be built, and further
Navy contracts would be for the F9F-2 version.
In the summer
of 1950, a re-engined F9F-3 (BuNo 122562) was fitted with an experimental
electro-hydraulically driven Emerson Aero X17A roll-traverse turret
housing four 0.50-inch machine guns. The guns could be directed
at any angle from directly forward to 20 degrees aft, and the
gun mount could be rolled the full 360 degrees in either direction.
The turret could roll at a rate of 100 degrees per second, and
the guns could be traversed at up to 200 degrees per second.
Although the
tests with the turret went fairly well, delays in the development
of the associated radar and fire control system led to the project
being cancelled in early 1954.
Serials
of F9F-3:
122476 Grumman XF9F-3 Panther
122560/122562 Grumman F9F-3 Panther
122564/122566 Grumman F9F-3 Panther
122568 Grumman F9F-3 Panther
122571 Grumman F9F-3 Panther
122573/122585 Grumman F9F-3 Panther
123020/123043 Grumman F9F-3 Panther
123068/123076 Grumman F9F-3 Panther
Grumman
F9F-2 Panther
The first production F9F-2 flew in August 1949. The production
F9F-2 was externally similar to the XF9F-2 prototype but with
wingtip tanks. However, it was equipped with an armament of four
20-mm cannon with 190 rounds per gun and the cockpit was provided
with a Martin-Baker ejector seat. With the wingtip tanks, the
total fuel capacity was now 923 US gallons. Because of the additional
equipment and fuel, it was substantially heavier than the XF9F-2.
The first
F9F-2s began their trials powered by J42-P-4 turbojets, but initial
production F9F-2s were powered by J42-P-6s. Most F9F-2s were powered
by J42-P-8s with a modified ignition system. All of these engines
offered a maximum wet takeoff-thrust of 5750 pounds and a dry
take-off thrust of 5000 pounds.
The production
by Pratt & Whitney of the J42 adaptation of the Rolls-Royce
Nene proceeded on schedule and with relatively few snags. The
J42 engine was, in fact, so successful in service that the F9F-3
alternative J33-powered version was deemed not to be necessary
and the few F9F-3s that were built were retrofitted with J42 engines
and thus became indistinguishable from F9F-2s. A total of 564
Panthers were delivered as F9F-2.
A substantial
number of early production F9F-2s were modified as F9F-2B fighter
bombers by the addition of four bomb racks underneath each wing.
The inboard rack could carry either a 150-gallon drop tank or
a 1000-pound bomb, whereas the three outboard racks could carry
250-pound bombs or 5-inch HVAR rockets. Maximum load was 2000
pounds. Beginning with the 365th F9F-2 (BuNo 125083), these racks
were installed at the factory. After most F9F-2s had been brought
up to F9F-2B standards, the B suffix was usually dropped.
When the Korean
War began in June 1950, the Navy had no jet-powered reconnaissance
aircraft, since the McDonnell F2H-2P Banshee still had not undergone
its first flight trials. As a stopgap measure, a small number
of F9F-2s were modified as unarmed photographic reconnaissance
aircraft under the designation F9F-2P. The four 20-mm cannon were
removed and replaced by oblique and vertical cameras.
Following
the withdrawal of the F9F-2 from service, a few F9F-2s were modified
as unarmed radio-controlled drones under the designation F9F-2D.
A few F9F-2s were modified as drone controllers under the designation
F9F-2KD. F9F-2 BuNo 123050 is on display at the USN Pensacola
Air Museum.
Serials
of Grumman F9F-2 Panther:
122475 Grumman XF9F-2 Panther
122477 Grumman XF9F-2 Panther
122563 Grumman F9F-2 Panther
122567 Grumman F9F-2 Panther
122569 Grumman F9F-2 Panther
122570 Grumman F9F-2 Panther
122572 Grumman F9F-2 Panther
122586/122589 Grumman F9F-2 Panther
123016/123019 Grumman F9F-2 Panther
123044/123067 Grumman F9F-2 Panther
123077/123083 Grumman F9F-2 Panther
123397/123713 Grumman F9F-2 Panther
125083/125155 Grumman F9F-2 Panther
127086/127215 Grumman F9F-2 Panther
F-9 / F9F-2 Panther
The McDonnell Company of St. Louis built the Navy’s
first all jet aircraft and demonstrated that the jet engine was
adaptable to naval aviation, but it was Grumman’s F9F Panther
that became the first Navy jet fighter to shoot down another jet
fighter. Grumman’s departure from propeller driven fighters
was accompanied by abandoning the tradition of naming the Company’s
fighters "Cats." However, the feline connection lived
on with Panther and Cougar and eventually returned to original
policy with the F-14 Tomcat.
Grumman received a Navy contract on 16 December
1946 to produce a jet powered, straight wing, carried based fighter.
The aircraft Grumman proposed first flew on 21 November 1947 and
was eventually designated and named the F9F-2 Panther. It was
first delivered to Navy squadron in May 1949 and remained in service
until October 1958. The Navy accepted a total of 1,388 Panthers
with designations of F9F-2, F9F-3, F9F-4 and F9F-5.
With the Panther, Grumman maintained its position
into the jet age as a major supplier of Navy carrier fighter aircraft.
The Panther never enjoyed the recognition of Grumman's last piston
engine fighter, the F8F Bearcat, as a spectacular performer. However,
it did extend Grumman's reputation for building rugged, effective
fighter aircraft. The F9F series began when development was initiated
on the large two-place four-jet XF9F-1 night fighter. Before design
work was completed, the XF9F-1 was dropped and the project shifted
to the single-place, single-jet XF9F-2 day fighter.
The imported Rolls-Royce Nene jet engines of the
two XF9F-2 prototypes were replaced in production F9F-2s by Pratt
& Whitney-built J42 Nenes. In the XF9F-3 and production F9F-3s,
an Allison J33 replaced the Nene. Only engine installation details
differed between the -2 and -3 Panthers. Permanently attached
tip-mounted external fuel tanks were the most obvious change added
to all Panthers early in the program.
While the first aircraft to see squadron service
were the -3s, which VF-51 received in May 1949, the Nene-powered
-2 became the sole production version following early deliveries.
An increased thrust version of the Allison J33
led to the -4 with a longer fuselage and increased area vertical
tail. The same airframe with the P&W-produced J48 version
of the Rolls-Royce Tay engine became the F9F-5. The -5s joined
the -2s as the major production versions. Photo versions, the
Navy-modified -2P and Grumman-built -5P, also served in carrier
air groups of the early Fifties.
A total of 1,385 Panthers were delivered to the
Navy. The Panthers became a mainstay of Navy and Marine forces
in Korea. They were the first carrier jets to fly in combat, shooting
down two YAK-9s on their first mission in July 1950. Later, in
November, LCdr. W. T. Amen, C.O. of VF-111, was the first carrier
jet pilot to shoot down a MiG-15.
In 1954, flight tests of the first fly-by-wire
aircraft, a modified F9F Panther jet, were initiated at Langley.
The primary objective of the tests was to evaluate various automatic
control systems, including those based on rate- and normal-acceleration
feedback. However (as is the case in many research investigations),
the most valuable result of the flight test was related to secondary
objectives—in this case the introduction and evaluation
of fly by wire and a sidestick controller for pilot inputs.
In a serendipitous approach, Langley researchers
decided to avoid the relatively large expense and time required
to modify the existing hydraulic flight control system for the
F9F. Instead they chose to implement an auxiliary system based
on a fly-by-wire analog concept and a small (4 in.) sidestick
controller mounted at the end of the armrest at the side of the
pilot. The sidestick controller was used as the maneuvering flight
controller throughout the investigation. Rapid and precision maneuvers
such as air-to-air tracking, ground strafing runs, and precision
landings were evaluated.
The objectives of the flight program were completed
with great success, and the information on various types of automatic
control feedback was used for numerous aircraft development programs.
However, the very successful use of the rudimentary fly-by-wire
and sidestick controller concepts generated considerable excitement
within the research community, especially those visionaries that
anticipated the weight saving advantages for future aircraft.
Additional research was conducted at Langley on these systems,
including the use of a sidestick controller for the Apollo mission.
As the -4 and -5 Panthers replaced the -2s in
carrier squadrons, the -2s took over advanced training, drone/drone
control, reserve squadron and other duties, followed in turn by
the -4s and -5s as they were replaced by their swept-wing F9F-6
successors. The last Marine combat squadrons to use Panthers kept
their -5s until late 1957, and a few drone F9F- 5KDs remained
to be redesignated DF-9Fs under the 1962 DOD redesignations.