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Caproni Vizzola F.5

Single-Seat, Single-Engine Monoplane Fighter

Caproni Vizzola F.5

Single-Seat, Single-Engine Monoplane Fighter

OVERVIEW
SPECIFICATIONS
ARMAMENT
VARIANTS
HISTORY
MEDIA
OVERVIEW



The Caproni Vizzola F.5 was developed in parallel with the F.4 of 1940 but both amounted to little more than footnotes of Italian military aviation for their time in the air.
National Flag Graphic
ORIGIN: Kingdom of Italy
YEAR: 1940
STATUS: Retired, Out-of-Service
MANUFACTURER(S): Caproni - Kingdom of Italy
PRODUCTION: 14
OPERATORS: Kingdom of Italy (retired)
SPECIFICATIONS



Unless otherwise noted the presented statistics below pertain to the Caproni Vizzola F.5 model. Common measurements, and their respective conversions, are shown when possible.
CREW: 1
LENGTH: 25.92 feet (7.9 meters)
WIDTH: 37.07 feet (11.3 meters)
HEIGHT: 9.84 feet (3 meters)
WEIGHT (EMPTY): 4,079 pounds (1,850 kilograms)
WEIGHT (MTOW): 4,938 pounds (2,240 kilograms)
ENGINE: 1 x Fiat A.74 R.C.38 14-cylinder air-cooled radial piston engine developing 870 horsepower and driving a three-bladed propeller unit at the nose.
SPEED (MAX): 317 miles-per-hour (510 kilometers-per-hour; 275 knots)
RANGE: 478 miles (770 kilometers; 416 nautical miles)
CEILING: 31,168 feet (9,500 meters; 5.90 miles)




ARMAMENT



2 x 12.7mm Breda-SAFAT fixed, forward-firing machine guns.
VARIANTS



Series Model Variants
• F.5 - Base Series Designation.
• F.5bis - F.4 airframe with DB601A inline engine built from final F.5 pre-series aircraft.
• F.5 "Gamma" - Proposed two-seat trainer with Isotta-Fraschini R.C.35 IS radial engine; not furthered.


HISTORY



Detailing the development and operational history of the Caproni Vizzola F.5 Single-Seat, Single-Engine Monoplane Fighter.  Entry last updated on 6/8/2018. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
In the pre-World War 2 period, F. Fabrizi of Italy led a design team that engineered several lesser-known fighter prototypes for the Kingdom of Italy. This work netted the "F.4", an all-modern monoplane seating one in an enclosed cockpit, offering a wholly retractable undercarriage, and armed with twin machine guns. Engine decisions meant that this model was passed on in favor of another fighter being designed in parallel - the "F.5'.

While the F.4 was intended to fit an Isotta-Fraschini liquid-cooled inline, the F.5 was to feature the Fiat A.74 R.C.38 twin-row, 14-cylinder air-cooled radial piston engine of 870 horsepower. This was used to drive a three-bladed propeller unit at the nose. Both aircraft used the same low-wing monoplane layout and both were designed to carry 2 x 12.7mm Breda-SAFAT heavy machine guns as primary armament. The availability of the German Daimler-Benz DB601 inline engine for Italy in the summer of 1939 changed the fortunes of the F.4 some but this model, slated to become the "F.5bis" prototype, managed little before being given up for good in 1942.

The F.5 itself flew in prototype form on February 19th, 1939 with its Fiat powerplant in place. It was showcased to Italian authorities who were sold enough on the type to order a second flyable prototype for further evaluation and this was followed by a contract for twelve pre-series airframes (subsequent events then led to the final pre-series F.5 airframe being used to develop the F.4/F.5bis mentioned earlier as that program was revitalized by the arrival of the German inline engines).

The eleven pre-series F.5 were delivered to 300 Squadriglia and, by 1942, were formed as part of the night-fighting contingent of 167 Gruppo. Beyond this, it appears that little more was had with the F.5. Like the F.4, the F.5 ended its days most likely in 1942.

The F.5 "Gamma" was a proposed two-seat trainer being planned for the series. It was to be powered by an Isotta-Fraschini "Gamma" R.C.35 IS air-cooled radial piston engine instead. A single 7.7mm Breda-SAFAT machine gun was to make up its armament load for gunnery training. Little was realized of this project.

As flown, the F.5 managed a maximum speed of 317 miles per hour with a range out to 480 miles. Its service ceiling reached 31,200 feet.




MEDIA







General Assessment (BETA)
Firepower  
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Performance  
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Survivability  
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Versatility  
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Impact  
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Rating: 44 (of 100)
The rating is an internal assessment derived from forty factors pertaining to this entry.
Relative Maximum Speed Rating
Hi: 400mph
Lo: 200mph
    This entry's maximum listed speed (317mph).

    Graph average of 300 miles-per-hour.
City-to-City Ranges
NYC
 
  LDN
LDN
 
  PAR
PAR
 
  BER
BER
 
  MSK
MSK
 
  TKY
TKY
 
  SYD
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  LAX
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  NYC
Graph showcases the Caproni Vizzola F.5's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Pie graph section
Pie graph section
Pie graph section
Pie graph section
Pie graph section
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
14
14

  * Commercial Market High belongs to Cessna 172.

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


Altitude Visualization
Small airplane graphic
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