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McDonnell FH / FD Phantom


Carrierborne Single-Seat, Jet-Powered Fighter (1947)


Aviation / Aerospace

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Jump-to: Specifications

The McDonnell FH Phantom series became the first post-World War 2 jet-powered fighter of the United States Navy.



Authored By: Staff Writer | Last Edited: 10/23/2017 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.
The Allied victory in World War 2 (1939-1945) was not a foregone conclusion in 1943 as the war in Africa and Europe raged alongside an ever-growing commitment to the Pacific against the might of the Japanese Empire. Warship battles dotted the ocean landscape throughout the island-hopping campaigns and progress proved a slow bloody affair. This period gave rise to a new generation of airmen, aces and aircraft and forever solidified the placement of the aircraft carrier in naval warfare.

With this in mind, the United States Navy (USN) looked to grow its stable of fighters beyond its conventionally-arranged, piston-powered types. As many of the major defense industry players were tied to the production of much-needed aircraft for immediate service, the U.S. Navy Bureau of Aeronautics approached McDonnell in January of 1943 to partner on a new single-seat, jet-powered monoplane fighter project. The engine of choice was an equally-new turbojet development offered from Westinghouse. The aircraft was given the designation of "FD-1".

McDonnell had revealed itself to be a rather forward-thinking company with its previous XP-67 "Moonbat" heavy fighter / interceptor development. While not adopted into service form - and only one flyable prototype completed - the Moonbat made McDonnell stand out as an aircraft builder. Additionally it did not hold the production commitment to the ongoing war as its competitors did.

In the short span of two years, McDonnell engineers had readied the "XFD-1" prototype which first took to the air on January 26th, 1945. The aircraft proved a sleek design featuring a well-streamlined fuselage, straight wing appendages (with clipped tips) and a single-finned tail unit. A wholly-retractable tricycle undercarriage was fitted and the airframe was powered by two of the aforementioned jets buried in the wingroots, exhausting through rounded ports at the wingroot aft. Because the engines could be mounted at any point behind the pilot, vision out-of-the-cockpit was vastly improved for navy aviators (no forward-mounted engine or spinning propellers to contend with and therefore a shorter distance between the cockpit and nose of the aircraft). Standard, fixed armament centered on 4 x 0.50 caliber heavy machine guns, all fitted to the nose. There was also support for 8 x 5" (127mm) High Velocity Aircraft Rockets (HVARs) underwing intended to help bring down large, slow-moving targets like bombers.
World War 2 ended with the Japanese surrender of August 1945 but the Navy still pursued its new fighter - nicknamed the "Phantom" because of its promised performance of 500 miles per hour - the aircraft would come and go as "an apparition" to enemy forces facing it. On July 21st, 1946, the XFD-1 prototype became the first all-jet USN aircraft to take-off and land on an American carrier (USS Franklin D. Roosevelt).

With Douglas' post-war reentry into fighter development, the "D" initially allocated to the McDonnell FD-1 project was assigned back to Douglas which left McDonnell use of "H" - as such the FD-1 became the "FH-1". Once its testing and evaluation phase had successfully ended, the FH-1 "Phantom" was introduced for service in August of 1947. For the USN, the jet age had begun which would produce a whole slew of evermore powerful types still to come - and McDonnell benefitted from this early partnership with the service branch.

VF-17A fighter squadron was the first to employ FH-1 Phantoms when they arrived in number for August 1947. Totals were strengthened considerably over the next year. Also in 1947, the United States Marine Corps aviation section acquired the FH-1 which marked the Phantom as the first joint USN/USMC jet-powered combat aircraft.

The FH-1 in service became more of a technological stepping stone for the USN than a long-term fighter solution. The thirsty jets it relied on limited operational range and the machine-gun-only armament was lacking punch when compared to the all-cannon arrangements featured on competing fighter designs seen elsewhere. While the Phantom carried rockets for its attack role (rarely uses in actual service) it lacked a bomb-delivery capability ruling out any usefulness as a fighter-bomber. Straightline performance was, however, one of the best of the period and gave the carrier-based fighter an advantage over piston-powered enemies it could potentially face.

The operational life of the FD-1 series was extremely short nonetheless for the line was retired by the USN and USMC as soon as 1949 and reserve units followed in 1954. McDonnell then developed the F2H "Banshee" from its FH-1 experience and 895 of this design were completed with service introduction coming during August of 1949. The FH-1 was not exported to U.S. partners and, beyond the 60 production FD-1 models and the pair of XFD-1 prototypes, no other variants existed.

The "Phantom" name was resurrected by McDonnell for their classic F-4 "Phantom II" design.

Specifications



Service Year
1947

Origin
United States national flag graphic
United States

Status
RETIRED
Not in Service.
Crew
1

Production
62
UNITS


McDonnell Aircraft Corporation - USA
National flag of the United States United States
(OPERATORS list includes past, present, and future operators when applicable)
Air-to-Air Combat, Fighter
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
Maritime / Navy
Land-based or shipborne capability for operating over-water in various maritime-related roles while supported by allied naval surface elements.


Length
37.2 ft
(11.35 m)
Width/Span
40.7 ft
(12.42 m)
Height
14.2 ft
(4.32 m)
Empty Wgt
6,680 lb
(3,030 kg)
MTOW
12,037 lb
(5,460 kg)
Wgt Diff
+5,357 lb
(+2,430 kg)
(Showcased structural values pertain to the McDonnell FH-1 Phantom production variant)
Installed: 2 x Westinghouse J30-WE-20 turbojet engines developing 1,600 lb of thrust each.
Max Speed
478 mph
(770 kph | 416 kts)
Ceiling
41,093 ft
(12,525 m | 8 mi)
Range
696 mi
(1,120 km | 2,074 nm)
Rate-of-Climb
4,230 ft/min
(1,289 m/min)


♦ MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


(Showcased performance specifications pertain to the McDonnell FH-1 Phantom production variant. Compare this aircraft entry against any other in our database. View aircraft by powerplant type)
STANDARD, FIXED:
4 x 12.7mm machine guns mounted in the nose

OPTIONAL:
8 x High Velocity Aircraft Rockets (HVARs) underwing


Supported Types


Graphical image of an aircraft medium machine gun
Graphical image of an aircraft heavy machine gun
Graphical image of aircraft aerial rockets


(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 0


FD "Phantom" - Original Series Designation
FH "Phantom" - Revised Series Designation
XFD-1 - Prototype Model Designation; two examples completed.
FH-1 - Production Series Designation; 60 examples delivered.


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