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|name=Aerfer Ariete |
|name=Aerfer Ariete |
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|image=Aerfer Ariete from Flightglobal Archive 1958-0492.jpg |
|image=Aerfer Ariete from Flightglobal Archive 1958-0492.jpg |
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|caption= |
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}} |
}} |
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− | {{Infobox |
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|type=Prototype fighter |
|type=Prototype fighter |
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|manufacturer=[[Aerfer]] |
|manufacturer=[[Aerfer]] |
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− | The '''Aerfer''' '''''Ariete''''' (Italian for ''Ram'') was a prototype [[fighter aircraft]] built in |
+ | The '''Aerfer''' '''''Ariete''''' (Italian for ''Ram'') was a prototype [[fighter aircraft]] built in Italy in 1958. It was a refined derivative of the [[Aerfer Sagittario 2]], and was an attempt to bring that aircraft up to a standard where it could be mass-produced as a viable combat aircraft. |
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Retaining most of the Sagittario 2's layout with a nose intake and ventral exhaust for the main [[Rolls-Royce Derwent|Derwent]] engine, the Ariete added a [[Rolls-Royce Soar]] RS.2 auxiliary turbojet engine to provide additional power for climbing and sprinting. This used a dorsal, retractable intake with its exhaust at the tail. |
Retaining most of the Sagittario 2's layout with a nose intake and ventral exhaust for the main [[Rolls-Royce Derwent|Derwent]] engine, the Ariete added a [[Rolls-Royce Soar]] RS.2 auxiliary turbojet engine to provide additional power for climbing and sprinting. This used a dorsal, retractable intake with its exhaust at the tail. |
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==Specifications (Ariete)== |
==Specifications (Ariete)== |
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{{Aircraft specifications |
{{Aircraft specifications |
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− | <!-- Now, fill out the specs. Please include units where appropriate (main comes first, alt in parentheses). If an item doesn't apply leave it blank. For instructions on using |more general=, |more performance=, |power original=, and |thrust original= see [[Template talk:Aircraft specifications]]. --> |
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|ref=''Air Enthusiast.''<ref>Swanborough 1971, p. 108.</ref> |
|ref=''Air Enthusiast.''<ref>Swanborough 1971, p. 108.</ref> |
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|crew= one, pilot |
|crew= one, pilot |
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|loaded weight main= 3,535 kg |
|loaded weight main= 3,535 kg |
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|loaded weight alt= 7,793 lb |
|loaded weight alt= 7,793 lb |
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|engine (jet)= [[Rolls-Royce Derwent|Rolls-Royce Derwent 9]] |
|engine (jet)= [[Rolls-Royce Derwent|Rolls-Royce Derwent 9]] |
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|thrust main= 16.2 kN |
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|afterburning thrust alt= <!--lbf--> |
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|engine (prop)= [[Rolls-Royce Soar|Rolls-Royce Soar (RSr 2)]] |
|engine (prop)= [[Rolls-Royce Soar|Rolls-Royce Soar (RSr 2)]] |
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|power main= 8.025 kN |
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==See also== |
==See also== |
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− | |related= |
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* [[Ambrosini S.7]] |
* [[Ambrosini S.7]] |
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* [[Ambrosini Sagittario]] |
* [[Ambrosini Sagittario]] |
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* [[Aerfer Sagittario 2]] |
* [[Aerfer Sagittario 2]] |
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* [[Aerfer Leone]] |
* [[Aerfer Leone]] |
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==References== |
==References== |
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{{Commons|Aerfer Ariete}} |
{{Commons|Aerfer Ariete}} |
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* Swanborough, Gordon. ''Air Enthusiast, Volume One''. London: Pilot Press, 1971. ISBN 0-385-08171-5. |
* Swanborough, Gordon. ''Air Enthusiast, Volume One''. London: Pilot Press, 1971. ISBN 0-385-08171-5. |
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− | {{Aerfer |
+ | {{Wikipedia|Aerfer Ariete}} |
− | {{Aviation lists}} |
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[[Category:Aerfer aircraft]] |
[[Category:Aerfer aircraft]] |
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[[Category:Cancelled military aircraft projects]] |
[[Category:Cancelled military aircraft projects]] |
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− | [[Category:Italian fighter aircraft |
+ | [[Category:1950s Italian fighter aircraft]] |
[[Category:Twinjets]] |
[[Category:Twinjets]] |
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[[Category:Low-wing aircraft]] |
[[Category:Low-wing aircraft]] |
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− | {{Wikipedia|{{PAGENAME}}}} |
Latest revision as of 00:40, 30 January 2020
Aerfer Ariete | |
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Role | Prototype fighter |
Manufacturer | Aerfer |
Designer | Sergio Stefanutti |
First flight | 27 March 1958 |
Primary user | Italian Air Force |
Number built | 2 (1 completed) |
Developed from | Aerfer Sagittario 2 |
The Aerfer Ariete (Italian for Ram) was a prototype fighter aircraft built in Italy in 1958. It was a refined derivative of the Aerfer Sagittario 2, and was an attempt to bring that aircraft up to a standard where it could be mass-produced as a viable combat aircraft. Retaining most of the Sagittario 2's layout with a nose intake and ventral exhaust for the main Derwent engine, the Ariete added a Rolls-Royce Soar RS.2 auxiliary turbojet engine to provide additional power for climbing and sprinting. This used a dorsal, retractable intake with its exhaust at the tail.
No production ensued; a proposed version with an auxiliary rocket engine instead of the auxiliary turbojet, the Aerfer Leone, was abandoned before a prototype could be built.
Specifications (Ariete)
Data from Air Enthusiast.[1]
General characteristics
- Crew: one, pilot
- Length: 9.60 m (31 ft 3 in)
- Wingspan: 7.50 m (24 ft 7 in)
- Height: 3.28 m (10 ft 9 in)
- Wing area: 14.5 m² (156 ft²)
- Empty weight: 2,400 kg (5,290 lb)
- Loaded weight: 3,535 kg (7,793 lb)
- Powerplant:
- 1 × Rolls-Royce Derwent 9 turbojet, 16.2 kN (3,640 lbf)
- 1 × Rolls-Royce Soar (RSr 2) turbojet, 8.025 kN (1,804 lbf)
Performance
- Maximum speed: 1,080 km/h (583 knots, 675 mph)
- Service ceiling: 12,000 m (39,360 ft)
- Rate of climb: 2,667 m/min (8,747 ft/min)
- Wing loading: 244 kg/m² (48 lb/ft²)
- Thrust/weight (jet): 1:2
Armament
See also
References
Wikimedia Commons has media related to Aerfer Ariete. |
- ↑ Swanborough 1971, p. 108.
- Swanborough, Gordon. Air Enthusiast, Volume One. London: Pilot Press, 1971. ISBN 0-385-08171-5.
The original article can be found at Aerfer Ariete and the edit history here.