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1402

France

Gerfaut

First flight

1954

In service

1954

info

Total in database

Crashed

info

info

Displays

info

Land Leased

Airplane.png
cockpit.png
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Variant
First Flight
Max Speed
Max Range
Max Weght
Max Celling:
Wing Span
length
height
1402B
1000
125
10000
50000
~18.9
~36.0
~21.3
1402A
1000
125
10000
50000
~18.9
~36.0
~21.3
1405
01/01/1953
1000
125
11000
50000
~18.9
~36.0
~21.3

The SNCASO (Société Nationale de Constructions Aéronautiques du Sud-Ouest) 1402B Gerfaut 1B was a French experimental interceptor of the early 1950s. Developed to explore the aerodynamic potential of tailless delta-wing configurations combined with turbojet power, it marked an important step in France’s postwar effort to build indigenous supersonic fighters. Its intended role was to serve as a prototype Mach 1+ interceptor, paving the way for operational aircraft that could counter fast, high-flying bombers in the emerging Cold War era.


Development and Role
The Gerfaut program began in the late 1940s as part of France’s ambitious push to catch up in aviation technology after World War II. The original 1402 prototype (Gerfaut I) first flew in 1953, demonstrating promising performance with a tailless delta design. The 1402B Gerfaut 1B was an improved variant that incorporated refinements to improve supersonic handling and test compatibility with future weapons systems.

The aircraft was built to evaluate aerodynamic efficiency, climb rate, and high-speed stability rather than to serve as an armed fighter itself. However, its development paralleled the growing need for a supersonic interceptor in French service, ultimately informing designs like the Dassault Mirage I/III series.


Powerplant and Enhancements
The Gerfaut 1B was powered by a SNECMA Atar 101D axial-flow turbojet, rated at about 7,700 lb thrust with afterburner. Enhancements in the 1B included:

  • A refined thin delta wing with a sharper leading edge for better supersonic aerodynamics.

  • Improved air intake geometry to ensure stable airflow at higher Mach numbers.

  • Reinforced fuselage structure to handle higher stress loads in transonic and supersonic flight.

  • Provisions for testing radar and armament systems (though these were mostly conceptual at this stage).

Configuration and Equipment
The Gerfaut 1B retained the single-seat, tailless delta-wing configuration of the earlier prototype, with notable refinements:

  • No horizontal stabilizers, with pitch control provided by elevons.

  • A large nose intake feeding the Atar turbojet.

  • A pressurized cockpit with an ejection seat.

  • Flight test instrumentation to record aerodynamic and engine data.

Although envisioned as a supersonic interceptor, the 1B was never armed. However, proposals suggested fitting it with air-to-air missiles or cannon for future operational development.


Operational Use
The Gerfaut 1B’s first flight took place in 1954, and it quickly became one of the first European aircraft to demonstrate sustained supersonic flight in level flight without afterburner assistance—a milestone that placed France alongside the United States and Soviet Union in cutting-edge jet technology.

Key performance highlights included:

  • Reaching Mach 1.13 in level flight.

  • Demonstrating exceptional climb rates, with time-to-altitude figures competitive with American prototypes of the same era.

  • Stable handling characteristics at both subsonic and supersonic speeds, proving the viability of delta-wing interceptors.

Despite its promise, the Gerfaut 1B remained a test aircraft. By the late 1950s, French military priorities shifted toward the Dassault Mirage program, which offered greater development potential and production readiness.


Crew Experience
Test pilots praised the Gerfaut 1B for its smooth handling and relatively forgiving delta-wing aerodynamics, though landings required precision due to higher approach speeds. Visibility from the cockpit was excellent thanks to the forward placement of the canopy over the nose intake. Pilots noted strong acceleration with the Atar engine and impressive performance at high altitude, but also limited endurance because of the engine’s high fuel consumption.


Conclusion
The SNCASO 1402B Gerfaut 1B played a vital transitional role in French aviation, bridging the gap between early postwar jet fighters and the supersonic interceptors that would dominate the Cold War era. While it never entered service, its successful test flights validated key concepts in delta-wing aerodynamics and supersonic propulsion, directly influencing the design of the Mirage series. In this way, the Gerfaut 1B secured its place as one of the essential stepping stones in France’s rise to prominence in high-speed aircraft design.

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