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Aviation / Aerospace

Caproni-Campini N1 (CC.2)

Technology Demonstrator Aircraft [ 1940 ]

The Caproni-Campini N1 was anything but an advancement for jet-powered flight, often refered to as a technological dead end.

Authored By: Staff Writer | Last Edited: 05/31/2017 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

GO TO SPECIFICATIONS [+]

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With the introduction of the N1 (may also be known as the CC.2), Italy became only the second nation in the world to achieve jet-powered flight (Germany being the first), though the development of this particular aircraft did little to further the arrival of the jet age and help a nation stuck on the losing end of a World War. Engine designer Secondo Campini joined forces with the Caproni aircraft firm to try and produce fruit for his labor in reaction propulsion technology. The product would become an interesting mix of the old and the new, for the N1 would feature a basic piston engine driving a fan compressor system with ignited fuel for added propulsion - in effect becoming an engine with afterburn characteristics to an extent. Though not a true turbojet, the N1 was nonetheless a practice aircraft and would prove the engine design possible but effectively become a design that could not be furthered to become something more.

The N1 became a large aircraft design piloted by two personnel. It was a low-wing monoplane with a traditionally-designed empennage and a single vertical tail surface. The intake was open at the extreme forward position and exhaust jettisoned at the extreme rear of the aircraft. The first flight was achieved in 1940 and several more controlled flights followed soon after. As this was mostly a technology demonstrator than a viable fighter design, no armament was fitted the to the system. Landing gear was powered and fully retractable. Keeping with early "jet" designs of the time, wings were straight-wings and featured the distinct smooth curves of piston engine fighter designs. The N1 would achieve a top speed of only 233 miles per hour.©MilitaryFactory.com

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The Caproni-Campini N1 (CC.2) neither a true piston engine aircraft or a full-blown turbojet design. As a result, development of this type of technology proved to be a dead end for the most part and the failing war effort at home put priorities for Italy mostly on the defensive. The N1 would never truly achieve much beyond proving a design concept and bringing Italy one step closer to the jet age. The N1 would go on to survive through the end of the war, becoming a museum set piece.©MilitaryFactory.com

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Specifications

Service Year

1940

Origin

Kingdom of Italy

Crew

2

Production

1
UNITS

Caproni-Campini - Italy

(View other Aviaton-Related Manufacturers)

Kingdom of Italy

(OPERATORS list includes past, present, and future operators when applicable)

✓ X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.

Length

43.0 ft
(13.10 m)

Width/Span

52.0 ft
(15.85 m)

Empty Wgt

8,025 lb
(3,640 kg)

MTOW

9,248 lb
(4,195 kg)

Wgt Diff

+1,224 lb
(+555 kg)

(Showcased structural values pertain to the base Caproni-Campini N1 (CC.2) production variant)

Installed: 1 x Isotta-Fraschini radial piston engine generating 900 horsepower driving a three-stage, ducted-fan compressor system.

Max Speed

233 mph
(375 kph | 202 kts)

Ceiling

13,123 ft
(4,000 m | 2 mi)

♦ MACH Regime (Sonic)

Sub

Trans

Super

Hyper

HiHyper

ReEntry

♦

(Showcased performance specifications pertain to the base Caproni-Campini N1 (CC.2) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)

None.

Supported Types

(Not all ordnance types may be represented in the showcase above)

None.

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