MANUFACTURER(S): McDonnell Aircraft - United States
LENGTH: 44.95 feet (13.7 meters)
WIDTH: 30.35 feet (9.25 meters)
HEIGHT: 14.60 feet (4.45 meters)
WEIGHT (EMPTY): 14,330 pounds (6,500 kilograms)
WEIGHT (MTOW): 17,185 pounds (7,795 kilograms)
ENGINE: 1 x Westinghouse XJ40-WE-8 turbojet engine developing 7,500lb of thrust (estimated).
SPEED (MAX): 761 miles-per-hour (1225 kilometers-per-hour; 661 knots)
RANGE: 1,087 miles (1,750 kilometers; 945 nautical miles)
CEILING: 50,000 feet (15,240 meters; 9.47 miles)
RATE-OF-CLIMB: 30,450 feet-per-minute (9,281 meters-per-minute)
Detailing the development and operational history of the McDonnell Model 60 Carrier-based Fleet Defense Fighter / Interceptor Proposal.
Entry last updated on 5/5/2016.
Authored by Staff Writer. Content ©www.MilitaryFactory.com.
Before the close of World War 2 (1939-1945), and in the period immediately following, the United States Navy (USN) raced to field its first jet-powered, carrier-launched fighters. Many developments existed and even more proposals were witnessed during this chapter of American aviation history that were to lead the service to acquire a whole new generation of fighter types heading into the next decade. A May 1948 requirement called for a new carrier-based, short-ranged single-seat turbojet-powered fleet defender / interceptor and, while the service eventually selected two different designs for the role - the Douglas F4D Skyray and the McDonnell F3H Demon, there lay several other submissions of note including the McDonnell "Model 60".
As an interceptor, the design required excellent take-off and climbing capabilities to meet a given inbound threat in short order. Additionally, a dimensionally compact design was needed to keep the aircraft both lightweight and relatively small for storage and operation aboard space-strapped American carriers. McDonnell introduced two designs, the Model 59 and the Model 60, the former utilizing a more conventional swept-wing arrangement, very pointed nose cone assembly and traditional tail unit with single rudder fin. The Model 60, however, settled on a twin rudder approach with full delta wing configuration. The mainplanes ran against the sides of the cylindrical fuselage which sat the pilot at the front in the usual way, aft of a shallow nosecone assembly. A tricycle undercarriage would be used and excellent vision out-of-the-cockpit provided for by a largely unobstructed "teardrop-style" canopy.
The selection of a delta wing allowed for more internal volume in the wings to be had. This meant that the main undercarriage legs could share space with additional fuel stores and possible armament while freeing volume from within the fuselage proper. A blended wing-body was not used however which would have benefitted the design even more. Besides the more obvious benefits of the delta wing championed by McDonnell engineers, another selling point of the approach was in improved handling characteristics and diving speeds. The rudder fins were set along the midway mark of each wing's trailing edge.
The Model 60 borrowed some of the Model 58's design features - a sole Westinghouse XJ40-WE-8 turbojet engine would be used and this aspirated by an intake arrangement which contoured nicely about the rounded fuselage sides at the cockpit walls. The engine was to exhaust through a single, large port between the twin rudder fins so no wing surfaces would be exposed to jet wash. The same armament scheme seen in the Model 59 was also employed in the Model 60 and consisted of 24 x aerial rockets fitted into a retractable, ventrally-mounted launcher unit.
It was estimated that the Model 60 could reach near-supersonic speeds during level flight and would most certainly be able to attain Mach 1.0+ speeds in a dive. The rocket armament gave it a healthy frontal "punch" against any incoming enemy target - particularly large Soviet bombers. As drawn up, the Model 60 was given a length of 45 feet and a wingspan of 30.3 feet. As a carrier aircraft it would also have been completed with the usual carrier-qualities such as reinforced undercarriage, tail arrestor hook and folding wings (the wings were set to fold outboard of each vertical tailplane). Maximum speed was estimated to be 762 miles per hour with a rate-of-climb nearing 30,450 feet per minute.
At any rate the Model 60 was not selected for development and the design ended its days as nothing more than a "paper airplane". The USN certainly found its fighters in due time and went on to field some of the more classic of the Cold War carrier-based aircraft to see the light of day. McDonnell continued to design and sell the service on various aircraft for the remainder of its operating days - including the fabulous F-4 "Phantom II" multirole platform which turned into a global success.
Where applicable, the appearance of U.S. Department of Defense (DoD), Russian Ministry of Defense, Chinese Ministry of Defense or British Ministry of Defence visual information does not imply or constitute endorsement of this website (www.MilitaryFactory.com). Images marked with "www.MilitaryFactory.com" or featuring the Military Factory logo are copyrighted works exclusive to this site and not for reuse in any form.
Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed Rating
This entry's maximum listed speed (761mph).
Graph average of 750 miles-per-hour.
Graph showcases the McDonnell Model 60's operational range (on internal fuel) when compared to distances between major cities.
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units