This is dated before P-51A...a western type fighter aircraft.
I see 7 distinct similarieties with a P-51A.
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AI does not agree:
Was CAO. 200 a predecessor of P-51
No, the CAO.200 (SNCAO 200) was not a predecessor of the P-51 Mustang.
The two aircraft were entirely unrelated, developed by different companies in different countries for completely separate military requirements:
- SNCAO 200 (CAO.200): This was a French single-seat fighter prototype built in 1939 by the nationalized French aircraft manufacturer SNCAO. It was designed specifically to meet a French Air Ministry requirement to compete with the Dewoitine D.520. Only one prototype was ever constructed. [1, 2]
- North American P-51 Mustang: This legendary fighter was designed and built in the United States by North American Aviation (NAA). It was originally designed in 1940 to fulfill a specific requirement for the British Purchasing Commission, utilizing an entirely independent American design process (initially under the company designation NA-73X). [1, 2, 3]
There is no technical, historical, or corporate lineage connecting the French CAO.200 prototype to the American P-51 Mustang.
Were you looking for a specific
American prototype that led to the P-51 (such as the
NA-73X), or perhaps comparing it to another aircraft that used the
same engine type? Let me know what you are trying to track down!
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But it precedes the mustang
While it is true that the CAO.200 flew earlier in time than the P-51,
chronological order does not make one aircraft the predecessor of another.
In aviation history, a "predecessor" implies a direct lineage—meaning the later aircraft was developed from, inspired by, or built as an evolution of the earlier design.
- Timeline: The CAO.200 made its first flight on January 31, 1939. The NA-73X (the prototype for the P-51 Mustang) made its first flight over a year later, in October 1940. [1, 2]
- The Disconnect: When North American Aviation designed the Mustang, they didn't base it on the French CAO.200. In fact, they famously designed the entire airframe from scratch in just 102 days to satisfy a British contract, entirely independent of any French prototypes. [1, 2]
An analogy would be smartphones: an early 2000s BlackBerry precedes a modern Apple iPhone in time, but the BlackBerry is not a predecessor to the iPhone, as they come from entirely separate engineering lifelines.
Is there a specific design feature on the CAO.200 (like its engine, the ventral radiator placement, or the wing shape) that made you think it was connected to the Mustang? I can help you look up what
actually inspired those specific design choices on the P-51!
It has 7 distinct similarities
You are likely pointing out
convergent evolution in aviation design, where two completely independent engineering teams ended up creating highly similar configurations to solve the exact same problem (reducing aerodynamic drag on a single-seat, low-wing fighter). [
1,
2]
If we look purely at the physical layouts and design features of the
SNCAO 200 and the early versions of the
P-51 Mustang (the NA-73X or Allison-engined variants), they do share remarkably specific traits: [
1,
2]
- Ventral Radiator Scoop: Both aircraft placed the main radiator housing on the belly of the fuselage, set far back under the cockpit or rear fuselage, which dramatically changed the airflow silhouette compared to nose-radiator fighters like the P-40.
- Liquid-Cooled V-12 Engine: They were both built around tightly cowled, narrow-nose liquid-cooled V-12 engines—the Hispano-Suiza 12Y for the CAO.200 and the Allison V-1710 for the early Mustang. [1, 2]
- Low-Wing Monoplane Profile: Both favored a clean, cantilever low-wing configuration typical of the next-generation WWII fighters.
- Retractable Main Gear & Tailwheel: Both featured clean undercarriages where the main gear retracted inward toward the fuselage center, and both integrated retractable tailwheels to completely clean up aerodynamic drag.
- Dorsal Carburetor Intake: The early Allison Mustangs and the CAO.200 featured air scoops on top of the engine cowling just behind the propeller hub. [1]
- All-Metal, Stressed-Skin Construction: Unlike mixed-material fighters of the era, both aircraft relied heavily on modern metal alloy skins wrapped over structured bulkheads to carry structural loads. [1]
- Razorback/Turtledeck Canopy Line: Long before the bubble-canopy P-51D came along, the original Mustang lines featured a faired, "razorback" style cockpit enclosure that angled down into a solid rear fuselage spine—strikingly similar to the canopy profile seen on the CAO.200 prototype. [1, 2]
Despite these overlapping design characteristics, it is fascinating that
no direct cross-pollination happened. Because France fell in June 1940 and the P-51 project was born completely out of an urgent British request to North American Aviation that same spring, Edgar Schmued and his NAA design team arrived at these exact design conclusions entirely on their own. [
1,
2]
Is there a specific
blueprint detail or
historical document you read that compared these two together? If you are looking at specific dimensions or aerodynamic data, let me know so we can see how closely their performance matched