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Behold the Aerfer XS.1, much cited but never shown last Stefanutti's project for Aerfer, 1959. It was a further evolution of the Leone formula (turbojets plus rocket engine) taken to its logical consequences, a zero-lenght takeoff point defence interceptor tailored to the European theater of operations during the early cold war: prospective menace by high-flying Mach 2 Soviet bombers, few minutes of warning time, lot of possible targets, first of all airports. The XS-1 intended modus operandi was different from that of the preceding Stefanutti's mixed propulsion machines. The rocket, unspecified, has a thrust of 3000 Kgs and burns kerosene with nitric acid as an oxidant. Some sources say that it is a Napier Scorpion, but I beg to differ for two reasons: first, the Scorpion did 3650 Kgs of thrust, and, second, the Scorpion used HTP (High Test Peroxide) as an oxidant, not nitric acid. The rocket was to be used to take-off and accelerate, complementing the turbojets (two Rolls Royce RB.145R, 1700 Kgs thrust each with a/b), until reaching Mach 2 at 11.000 mts in level flight (2' 30 " after take-off). The attack, either level or with a final climb to the max height of 21.000 mts was to be under jets alone (see graphic), after discarding the empy rocket fuel tank (nitric acid). The launcher was mobile, mounted on a standard truck (Italians will recognize a well known '50s lorry) and meant to be dispersed in case of war. The XS.1 was to be integrated in a two layer air defense system, with short range missiles as last resort. The early warning and control system (radar, fighter control, missile launch, etc) had to be integrated (a tall order in late '50s Italy, I fear) and commander were to be able to use the weapons based on the tactical situation. Naturally, the project was never pursued. First, there was no money: the preceding Stefanutti's planes had been funded by US money, and, second, by 1959 Aeronautica Militare had already chosen the F-104G for a primarily fighter-bomber role, using Nike-series missile for medium range intercept, and later Hawk for short-range.
Data for the XS.1:
Length: 8.80 m
Span: 5.60 m
Wing surface: 9 sqm
Weight:
empty 2050 Kgs
MTOW 4870 Kgs
Radius: 150 Km
Landing lenght: 150 m
with arresting hook 80 m
Armament: 2 not specified guided missiles (weight 100 kg each)
Data for the XS.1:
Length: 8.80 m
Span: 5.60 m
Wing surface: 9 sqm
Weight:
empty 2050 Kgs
MTOW 4870 Kgs
Radius: 150 Km
Landing lenght: 150 m
with arresting hook 80 m
Armament: 2 not specified guided missiles (weight 100 kg each)