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SNCAC NC.1070


Carrier-based Strike Aircraft Prototype


France | 1948



"The SNCAC NC.1070 was a failed French development of a carrier-based strike platform - one prototype was completed and flown."

Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the SNCAC NC.1070 Carrier-based Strike Aircraft Prototype.
2 x Gnome-Rhone (SNECMA) 14R R-25 14-cylinder twin-row, air-cooled radial piston engine developing 1,500 to 1,600 horsepower each and driving three-bladed propeller units.
Propulsion
360 mph
580 kph | 313 kts
Max Speed
32,808 ft
10,000 m | 6 miles
Service Ceiling
2,113 miles
3,400 km | 1,836 nm
Operational Range
Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the SNCAC NC.1070 Carrier-based Strike Aircraft Prototype.
3
(MANNED)
Crew
33.5 ft
10.20 m
O/A Length
65.6 ft
(20.00 m)
O/A Width
15.1 ft
(4.60 m)
O/A Height
17,306 lb
(7,850 kg)
Empty Weight
23,589 lb
(10,700 kg)
MTOW
Armament
Available supported armament and special-mission equipment featured in the design of the SNCAC NC.1070 Carrier-based Strike Aircraft Prototype .
PROPOSED (Standard):
2 x 20mm MG151 autocannons in nose.
2 x 20mm MG151 autocannons in rear powered turret.

PROPOSED (Optional):
Support for up to 4,410lb of drop bombs or aerial torpedoes.
Variants
Notable series variants as part of the SNCAC NC.1070 family line.
NC.1070 - Base Prototype Designation..
NC.1071 - Second version fitted with 2 x Rolls-Royce Nene turbojets.
NC.10
Authored By: Staff Writer | Last Edited: 02/25/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.

The French Navy's quest to reestablish its legitimacy following the close of World War 2 in 1945 led the service to, at first, take on many surplus equipment types from the United States and Britain. In time, indigenous programs ultimately went on to satisfy standing local requirements and, one such attempt, became the SNCAC "NC.1070". This initiative sought to satisfy a French Navy need for a carrier-based, torpedo-or-bomb-carrying, anti-ship strike platform. Three prototypes were contracted for and up to 100 production-quality aircraft were envisioned.

The aircraft would feature a crew of three and was given a twin-engine, twin-boom design arrangement with a centralized fuselage straddled by the straight-lined wing mainplanes. Each mainplane carried a Gnome-Rhone (SNECMA) 14 series R-25 14-cylinder air-cooled radial piston engine of 1,500 horsepower and these were used to drive three-bladed propelled units. The booms emanated from the engine nacelles in traditional fashion, terminating at the rear of the aircraft where there was fitted a twin-vertical fin configuration. Atop these two structures was placed the horizontal stabilizer and this sat over a fixed horizontal plane. A conventional tricycle undercarriage (retractable) would be used for ground-running.

Structurally, the aircraft carried a running length of 33.5 feet and a wingspan of 65.6 feet with a height of 15 feet. Empty weight was 17,305lb against an MTOW of 23,600lb. Size was of particular importance for the aircraft would have to be cleanly stowed away on a space-strapped aircraft carrier of the period.

For armament, it was proposed that the aircraft would field 2 x 20mm MG151 autocannons in fixed, forward-firing mounts and 2 x20mm MG151 autocannons in a SAMM AB211 series powered turret (the latter primarily for self-defense). Up to 4,410lb of stores could be carried, these made up of either conventional drop bombs or aerial torpedoes.

The first of the scheduled prototypes made its first-flight on May 25th, 1947. Further testing revealed the aircraft to be largely underpowered despite its twin-engine arrangement - even without the rear turret or primary, fixed armament having been fitted. After suffering damage during a landing action in March of 1948, the aircraft was not repaired nor furthered.

As tested, the NC.1070 recorded a maximum speed of 360 miles per hour, reaching a range out to 1,835 miles and a service ceiling up to 32,640 feet.

Instead, the focus now shifted to the same design now powered by 2 x Rolls-Royce "Nene" turbojet engines - the "NC.1071". This specimen flew for the first time on October 12th, 1948, but did not produce the expended performance gains and the program was shelved in full.

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Operators
Global customers who have evaluated and/or operated the SNCAC NC.1070. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 1 Units

Contractor(s): Societe Nationale de Constructions Aeronautiques du Centre (SNCAC) - France


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