Military Wiki
m (→‎References: Remove some templates. interwiki links, delink non military terms, add link to Wikipedia and cleanup)
m (→‎References: Refine categories and cleanup)
 
(9 intermediate revisions by 2 users not shown)
Line 1: Line 1:
{|{{Infobox Aircraft Begin
+
{|{{Infobox aircraft begin
 
|name=Aerfer Ariete
 
|name=Aerfer Ariete
 
|image=Aerfer Ariete from Flightglobal Archive 1958-0492.jpg
 
|image=Aerfer Ariete from Flightglobal Archive 1958-0492.jpg
 
|caption=
 
|caption=
 
}}
 
}}
{{Infobox Aircraft Type
+
{{Infobox aircraft type
 
|type=Prototype fighter
 
|type=Prototype fighter
 
|manufacturer=[[Aerfer]]
 
|manufacturer=[[Aerfer]]
Line 22: Line 22:
 
|}
 
|}
   
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.
+
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 [[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.
   
Line 30: Line 29:
 
==Specifications (Ariete)==
 
==Specifications (Ariete)==
 
{{Aircraft specifications
 
{{Aircraft specifications
  +
<!-- if you do not understand how to use this template, please ask at [[Wikipedia talk:WikiProject Aircraft]] -->
 
 
|plane or copter?=<!-- options: plane/copter --> plane
 
|plane or copter?=<!-- options: plane/copter --> plane
 
|jet or prop?=<!-- options: jet/prop/both/neither --> both
 
|jet or prop?=<!-- options: jet/prop/both/neither --> both
  +
<!-- 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]]. -->
 
 
|ref=''Air Enthusiast.''<ref>Swanborough 1971, p. 108.</ref>
 
|ref=''Air Enthusiast.''<ref>Swanborough 1971, p. 108.</ref>
 
|crew= one, pilot
 
|crew= one, pilot
Line 50: Line 49:
 
|loaded weight main= 3,535 kg
 
|loaded weight main= 3,535 kg
 
|loaded weight alt= 7,793 lb
 
|loaded weight alt= 7,793 lb
|useful load main= <!--kg-->
+
|useful load main=
|useful load alt= <!--lb-->
+
|useful load alt=
|max takeoff weight main= <!--kg-->
+
|max takeoff weight main=
|max takeoff weight alt= <!--lb-->
+
|max takeoff weight alt=
 
|more general=
 
|more general=
 
|engine (jet)= [[Rolls-Royce Derwent|Rolls-Royce Derwent 9]]
 
|engine (jet)= [[Rolls-Royce Derwent|Rolls-Royce Derwent 9]]
|type of jet= [[turbojet]]
+
|type of jet= turbojet
 
|number of jets=1
 
|number of jets=1
 
|thrust main= 16.2 kN
 
|thrust main= 16.2 kN
Line 64: Line 63:
 
|afterburning thrust alt= <!--lbf-->
 
|afterburning thrust alt= <!--lbf-->
 
|engine (prop)= [[Rolls-Royce Soar|Rolls-Royce Soar (RSr 2)]]
 
|engine (prop)= [[Rolls-Royce Soar|Rolls-Royce Soar (RSr 2)]]
|type of prop= [[turbojet]]
+
|type of prop= turbojet
 
|number of props=1
 
|number of props=1
 
|power main= 8.025 kN
 
|power main= 8.025 kN
Line 95: Line 94:
   
 
==See also==
 
==See also==
{{Aircontent|
 
|related=
 
 
* [[Ambrosini S.7]]
 
* [[Ambrosini S.7]]
 
* [[Ambrosini Sagittario]]
 
* [[Ambrosini Sagittario]]
 
* [[Aerfer Sagittario 2]]
 
* [[Aerfer Sagittario 2]]
 
* [[Aerfer Leone]]
 
* [[Aerfer Leone]]
|similar aircraft=
 
|lists=
 
|see also=
 
   
}}
 
 
==References==
 
==References==
 
{{Commons|Aerfer Ariete}}
 
{{Commons|Aerfer Ariete}}
Line 111: Line 104:
 
* 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.
   
{{Aerfer aircraft}}
+
{{Wikipedia|Aerfer Ariete}}
{{Aviation lists}}
 
   
 
[[Category:Aerfer aircraft]]
 
[[Category:Aerfer aircraft]]
 
[[Category:Cancelled military aircraft projects]]
 
[[Category:Cancelled military aircraft projects]]
[[Category:Italian fighter aircraft 1950–1959]]
+
[[Category:1950s Italian fighter aircraft]]
 
[[Category:Twinjets]]
 
[[Category:Twinjets]]
 
[[Category:Low-wing aircraft]]
 
[[Category:Low-wing aircraft]]
 
{{Wikipedia|{{PAGENAME}}}}
 

Latest revision as of 00:40, 30 January 2020

Aerfer Ariete
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

  • 2 × 30 mm HDD-825 cannons
  • See also

    References

    1. Swanborough 1971, p. 108.
    • Swanborough, Gordon. Air Enthusiast, Volume One. London: Pilot Press, 1971. ISBN 0-385-08171-5.
    All or a portion of this article consists of text from Wikipedia, and is therefore Creative Commons Licensed under GFDL.
    The original article can be found at Aerfer Ariete and the edit history here.