The Caproni Vizzola line of "F" fighters was led by the late-1937 initiative "F.4" model. This was an all-modern monoplane fighter seating one and armed with twin heavy machine guns while powered by an inline piston engine. The subsequent "F.5" utilized the same airframe and armament but went the route of an air-cooled radial piston engine for its power. The former only lasted as a single prototype tested into 1942 while the latter achieved pre-series production but, itself, only totaled fourteen aircraft in all (including two prototypes). These were, however, fielded as night-fighters with an Italian squadron during the middle of World War 2 (1939-1945) for their part in the conflict.
All of this work led the company to establish the "F.6", a similarly-minded fighting monoplane. It shifted to a liquid-cooled inline engine once the German DB605's became available to Italy but was more or less a continuation of both the F.4 and F.5 lines. The F.5 made up its airframe and the powerplant of choice became the DB605A V-12 inverted piston engine of 1,474 horsepower driving a three-bladed propeller unit at the nose. The wing mainplanes were redesigned and completed as all-metal members for added strength, unlike the wooden ones used in the F.5. Again, armament was a modest load-out of just 2 x 12.7mm Breda-SAFAT heavy machine guns, these fitted to the nose, while a pair of guns could be added to the wings (one per wing).
The revised aircraft was designated as "F.6M" and, in prototype form, the product achieved a first-flight in September of 1941. Its chin-mounted radiator was found to generate significant drag during flight so this structure was modified and repositioned closer to midships (at the belly, aft of the cockpit floor). This prototype was actively tested until a collision at Bresso and given up for good thereafter - Caproni looking to further the promising F.7 fighter instead (detailed elsewhere on this site).
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Specifications
Caproni Vizzola - Kingdom of Italy Manufacturer(s)
AIR-TO-AIR COMBAT
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
INTERCEPTION
Ability to intercept inbound aerial threats by way of high-performance, typically speed and rate-of-climb.
X-PLANE
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.
30.0 ft (9.15 meters) Length
37.2 ft (11.35 meters) Width/Span
9.9 ft (3.02 meters) Height
4,993 lb (2,265 kilograms) Empty Weight
6,360 lb (2,885 kilograms) Maximum Take-Off Weight
+1,367 lb (+620 kg) Weight Difference
1 x Daimler-Benz DB605A inverted V-12 liquid-cooled piston engine developing 1,474 horsepower and driving a three-bladed propeller unit at the nose. Propulsion
PROPOSED (F.6M):
2 x 12.7mm Breda-SAFAT heavy machine guns in forward fuselage.
2 x 12.7mm Breda-SAFAT heavy machine guns in wings (one per wing) (optional).
PROPOSED (F.6Z):
1 x 12.7mm Breda-SAFAT heavy machine gun in forward fuselage.
2 x 12.7mm Breda-SAFAT heavy machine guns in wings (one per wing).
0 Hardpoints
F.6 - Base Series Designation
F.6M - Fitted with Daimler-Benz DB605A V12 engine; 2 x 12.7mm HMG armament with optional 2 x 12.7mm wing guns; damaged in collision and ultimately abandoned.
F.6Z - Fitted with Isotta-Fraschini Zeta R.C.25/60 24cyl X-type engine; armament of 1 x 12.7mm fuselage gun and 2 x 12.7mm wing guns; abandoned development.
General Assessment
Firepower
Performance
Survivability
Versatility
Impact
Values are derrived from a variety of categories related to the design, overall function, and historical influence of this aircraft in aviation history.
Overall Rating
The overall rating takes into account over 60 individual factors related to this aircraft entry.
24
Rating is out of a possible 100 points.
Relative Maximum Speed
Hi: 400mph
Lo: 200mph
This entry's maximum listed speed (354mph).
Graph average of 300 miles-per-hour.
City-to-City Ranges
NYC
LON
LON
PAR
PAR
BER
BER
MOS
MOS
TOK
TOK
SYD
SYD
LAX
LAX
NYC
Operational range when compared to distances between major cities (in KM).
Max Altitude Visualization
Design Balance
The three qualities reflected above are altitude, speed, and range.
Aviation Era Span
Showcasing era cross-over of this aircraft design.
Unit Production (2)
2
36183
44000
Compared against Ilyushin IL-2 (military) and Cessna 172 (civilian).
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