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Grumman Sapphire Cougar

Jet-Powered Carrierbased Fighter Proposal

Grumman Sapphire Cougar

Jet-Powered Carrierbased Fighter Proposal

OVERVIEW
SPECIFICATIONS
ARMAMENT
VARIANTS
HISTORY
MEDIA
OVERVIEW



Proposed by Grumman though not taken up by the United States Navy, the Sapphire Cougar undoubtedly influenced the upcoming F11F Tiger swept-wing fighter for the company.
National Flag Graphic
ORIGIN: United States
YEAR: 1953
STATUS: Cancelled
MANUFACTURER(S): Grumman Aircraft - USA
PRODUCTION: 0
OPERATORS: United States
SPECIFICATIONS



Unless otherwise noted the presented statistics below pertain to the Grumman Sapphire Cougar model. Common measurements, and their respective conversions, are shown when possible.
CREW: 1
LENGTH: 41.24 feet (12.57 meters)
WIDTH: 31.66 feet (9.65 meters)
HEIGHT: 13.12 feet (4 meters)
WEIGHT (EMPTY): 12,787 pounds (5,800 kilograms)
WEIGHT (MTOW): 15,807 pounds (7,170 kilograms)
ENGINE: 1 x Wright J65-W-3 (Armstrong-Siddeley "Sapphire") afterburning turbojet engine developing an estimated 7,000lb dry thrust and 10,000lb with reheat.
SPEED (MAX): 637 miles-per-hour (1025 kilometers-per-hour; 553 knots)
RANGE: 652 miles (1,050 kilometers; 567 nautical miles)
CEILING: 51,001 feet (15,545 meters; 9.66 miles)
RATE-OF-CLIMB: 13,400 feet-per-minute (4,084 meters-per-minute)




ARMAMENT



PROPOSED:
4 x 20mm Colt Mk 12 cannons under the nose section.

Optional:
4 x AIM-9 "Sidewinder" short-ranged Air-to-Air Missiles (AAMs) OR Aerial rocket packs OR 2 x Jettisonable fuel stores.
VARIANTS



Series Model Variants
• "Sapphire Cougar" - Named Proposal; not selected by the United States Navy for development.


HISTORY



Detailing the development and operational history of the Grumman Sapphire Cougar Jet-Powered Carrierbased Fighter Proposal.  Entry last updated on 2/21/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
As the age of the jet fighter was getting its feet underneath, longtime fighter supplier Grumman approached the United States Navy (USN) with a concept for a new carrier-based solution which came to be known as the "Sapphire Cougar" for its lineage related to the earlier F9F "Cougar" and its choice of engine, the British Armstrong-Siddeley "Sapphire" turbojet. The engine was a local-license model from Curtiss-Wright which tagged it the "J65". The fighter was intended as a compact product to serve from the decks of the space-strapped Essex-class aircraft carriers then in USN service. As such it would have featured carrier-operation qualities like wing-folding, a reinforced under-structure, and arrestor hook equipment.

The aircraft certainly mimicked aspects of the F9F and the subsequent F11F "Tiger" developments put forth by the same company. A swept-back, high-mounted mainplane form was used as were side-mounted intakes. The pilot's position was well-forward in the design, positioned just over the nose. The tail section featured a single fin with a pair of horizontal planes - all featuring sweepback. A tricycle undercarriage rounded out the list of modern features.

It is assumed that the Sapphire Cougar would be outfitted with 4 x 20mm cannons to fulfill the fighter requirement. This would be consistent with carrier fighters of the late 1940s and early 1950s. The high-mounted wing mainplanes also opened the design to carrying underwing stores such as early-form Air-to-Air Missiles (AAMs), conventional drop bombs and rocket pods - the latter two offering an inherent strike capability and doubling the design's tactical usefulness.




The USN eventually showed little interest in the Sapphire Cougar concept and the design fell away to military aviation history in time. At least a wind tunnel model was completed for testing to go along with design drawings and this marked the Sapphire Cougar as a stepping point towards the upcoming F11F Tiger - which was adopted by the USN in useful numbers (200).

As the Sapphire Cougar was never built and flown, performance figures remained estimated by Grumman engineers as part of the USN proposal. This included a maximum speed of 725 miles per hour, a service ceiling up to 51,000 feet and a combat radius reaching 320 miles.




MEDIA









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.

Image of collection of graph types

Relative Maximum Speed Rating
Hi: 750mph
Lo: 375mph
    This entry's maximum listed speed (637mph).

    Graph average of 562.5 miles-per-hour.
City-to-City Ranges
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  NYC
Graph showcases the Grumman Sapphire Cougar's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
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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
0
0

  * Commercial Market High belongs to Cessna 172.

  ** Military Market High belongs to Ilyushin Il-2.


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Supported Roles
A2A
Interception
UAV
Ground Attack
CAS
Training
ASW
Anti-Ship
AEW
MEDEVAC
EW
Maritime/Navy
SAR
Aerial Tanker
Utility/Transport
VIP
Passenger
Business
Recon
SPECOPS
X-Plane/Development
A2A=Air-to-Air; UAV=Unmanned; CAS=Close Support; ASW=Anti-Submarine; AEW=Airborne Early Warning; MEDEVAC=Medical Evac; EW=Electronic Warfare; SAR=Search-Rescue
Supported Arsenal
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