So was the Rolls Royce R and look what that led to!The Fiat engine was a race engine so not comparable at all nor usable in anything else but racing
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So was the Rolls Royce R and look what that led to!The Fiat engine was a race engine so not comparable at all nor usable in anything else but racing
A rather unfair comparison.
Maybe it was politics.
Isotta-Fraschini managed to sell a fair number of V-12s to the Italian military in the mid to late 30s. At least in comparison to the total number of engines built, however the Isotta-Fraschini V-12 never seemed to crack the 1000hp barrier in production form and so never made any real impact on the aviation scene. Perhaps Fiat backed the wrong people in government?
The 1938 Jane's does say that at some point Fiat was told by the Italian government to simplify their range of liquid cooled engines, in the late 20s they had five different V-12 engines not including minor variations and/or race engines. This might not have been an unreasonable request. Fiat did trim the lineup to 3 engines.
I would note that NONE of these engines had superchargers and ALL were in operation before 1930. That leaves the AS-6 race engine as the last Fiat V-12 to try to develop a service engine from and yet it could be traced back to the AS.5 of 1929 (unsupercharged).
Please note that a racing engine at sea level is operating quite differently than an engine at 15,000ft. These old Fiat engines were delivering a much higher percentage of power developed in the cylinders to the propeller, the only loss being power to friction (pumps are included in this catagory) while a supercharged engine operating at 15,000ft could be devoting several hundred horsepower to driving the supercharger which means a higher thermal load and more pressure/stress inside the cylinders.
Perhaps the Fiat company decided on their own to go for the air-cooled market? Or perhaps, with their eye on Africa, the Italian government issued a requirement (or more than one) that favored air cooled engines? The consumption of water by liquid cooled engines in the dessert would be minuscule in comparison to the consumption of water by hundreds of ground crew but sometimes logic wasn't a strong point in armchair air marshals (or like the US Navy, experiences in the 1920s with leaky liquid systems soured them on liquid cooled engines?)
A chronic disease of ideologues. Evidence that disagrees is just a [insert etnic group or nationality of choice] conspiracy. Alas, not a defunct position.I found it curious that both Piaggio and Isotta-Fraschini licensed the Gnome-Rhone 14K. In hindsight this probably wasn't the best choice given the limited development potential of the basic design. Furthermore, the latter company carried out little development and production of the K14 engine. Perhaps they would have been better off developing a monobloc version of their V12s or licensing the DB engines.
The Fascist government seems to have made many bad decisions, such as giving priority to the production of light tanks of minimal usefulness, to say nothing of jumping into a war it was badly prepared for. It seems that the decision makers heard only what they wanted to hear.
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The failures of the Fascists is inherent to the regime. Mussolini was acutely aware of Italian economic weakness. Having said that, the fascist regime was a highly centralised regime, in which nearly all power, but no responsibility was vested in the hands of one man. This one man needed lieutenants to pay the bills, switch the lights on and off, but ultimately were beholden to the Duce for their status. Mussolini was more about style and looks than substance. He was after all, a newspaper journo in which facts were secondary to sensation. He wanted more tanks than anybody, but Italy couldn't afford real tanks, it couldn't even afford to research tanks properly. Results were that Italy went to war with poor AFV park, many tanks were referred to as "sardine tins". They really were rather poorly designed tankettes, on, or below par with a bren gun carrier. The true tanks were a mixture of obsolete types dates back to the late 20s, or a few exceptionally bad types epitomised in the M-13/39.Break down rates were exceptionally high.
Italy boasted that she could raise an army of "8 million rifles". Maybe, but they never did. Closer to 2 million really, including training and militia units. Something like 11 different calibers of rifle spread over 20 something models. Artillery was atrocious and short supply.
Naval units were slow to reach front line units, cruisers were designed to win pre-war trial speed rercords more than anything, carrier aviation was ignored. The design of guns were generally poor with huge dispersal issues, a lack of strength to allow full salvo fire, poor sustained sea speeds, slow rates of fire for most weapons, and fatally a lack of realistic training for night operations. Italy as a whole was short of fuel, but the navy in particular suffered from this shortage.
The RA was the darling child of the Fascists and in the 1930's it had give impressive displays of its power and technology all over Europe, indeed the world. In the early 1930s it was impressive, but as the decade wore on, the italians began to lag. It was in this environment of all show and no substance that the Ba88 was born. It was an aircraft designed and built for show, not a practical response in any sense. designed to grab headlines and not much else.
The question I think that is relevant is whether, with the tools and equipment at hand if there was anything that could have been done to rescue the Ba-88. Certainly engines of higher power and further engines that didn't lose power in desert conditions. This is a bit of a mystery to me, since other Italian aircraft used exactly the same engine and did not suffer the same catastrophic losses in performance as the Ba-88. Makes me think something else was wrong with this aircraft. Im thinking fuel management.
A comparison with the Z1007, another aircraft with the same engine, albeit 3 attached, allowed that aircraft, at slightly over 30000 lb fully loaded to achieve deent levls of performance. The published figures (probably not carrying any great amounts of weight) enabled the z 1007 to reach respectable speeds of 285 mph. The z 1007 had an empty weight of 20718 lbs. I would hazard a guess and claim the z 1007 was less aerodynamic than the BA 88.The BA 88 in comparison had an empty weight of (10,251 lb) and a fully loaded weight of 14,881 lb. Comparatively the BA 88 had significantly greater amounts of power per lb of weight to the Z 1007, yet was barely able to get off the ground. What caused this?
Did the prototype had any means of protection, either for crew or fuel, or both? For oil system? Radios, batteries, antennea masts, how many crew on board? Top crop of the pilot(s) for the prototype vs. run on the mill pilot(s) for the military-viable ones?
We know well how the P-36C become the P-39D, or how the P-40 (no suffix) became P-40E, or how A6M5 became A6M5c - performers turned into turkeys once protection, better/more radios and firepower was added for almost no increase of engine power. Neither of whom featured 'double construction' methods applied on the Ba.88.