Military Wiki
m (1 revision: Import articles part 15)
m (Remove some templates, interwiki links, delink non military terms and cleanup)
 
(12 intermediate revisions by 2 users not shown)
Line 1: Line 1:
 
{|{{Infobox aircraft begin
__NOTOC__
 
<!-- This article is a part of [[Wikipedia:WikiProject Aircraft]]. Please see [[Wikipedia:WikiProject Aircraft/page content]] for recommended layout. -->
 
{|{{Infobox Aircraft Begin
 
 
| name=Phönix D.I, D.II, and D.III
 
| name=Phönix D.I, D.II, and D.III
 
| image=Phönix D.I 228.45.jpg
 
| image=Phönix D.I 228.45.jpg
 
| caption=Phönix D.I
 
| caption=Phönix D.I
 
}}
}}{{Infobox Aircraft Type
+
{{Infobox aircraft type
 
| type=[[Fighter plane|Biplane fighter]]
 
| type=[[Fighter plane|Biplane fighter]]
 
| national origin=Austria-Hungary
 
| national origin=Austria-Hungary
Line 20: Line 19:
 
}}
 
}}
 
|}
 
|}
The '''Phönix D.I''' was an [[Austria-Hungary|Austro-Hungarian]] First World War biplane fighter built by the Phönix Flugzeug-Werke and based on the [[Hansa-Brandenburg D.I]].<ref>{{cite web|url=http://www.theaerodrome.com/aircraft/austrhun/phonix_di.php|title=Phönix D.I|work=The Aerodome|accessdate=25 April 2013}}</ref>
+
The '''Phönix D.I''' was an Austro-Hungarian First World War biplane fighter built by the Phönix Flugzeug-Werke and based on the [[Hansa-Brandenburg D.I]].<ref>{{cite web|url=http://www.theaerodrome.com/aircraft/austrhun/phonix_di.php|title=Phönix D.I|work=The Aerodome|accessdate=25 April 2013}}</ref>
 
 
==Development==
 
==Development==
The Phönix D.I was the second design developed by the Phönix Flugzeug-Werke based on Hansa-Brandenburg designs which it has produced under licence.<ref name="Lamberton">Lamberton, 1960. p 22.</ref> The D.I was a single-seat biplane fighter with improvements over the original Hansa-Brandenburg design which included more efficient wings, a more powerful engine and structural improvements.<ref name="Lamberton"/> A prototype was first flown in 1917 and proved to be fast but difficult to handle but because of the urgent need for fighters the D.I entered production. To improve the problems a modified variant, the '''D.II''' was introduced with balanced elevators and balanced ailerons on the upper wings. A further development was the '''D.III''' which had balanced ailerons on both wings and a more powerful 230&nbsp;hp (172&nbsp;kW) Hiero in-line engine. The last of 158 aircraft of all three types was delivered on 4 November 1918.{{cn|date=October 2013}}
+
The Phönix D.I was the second design developed by the Phönix Flugzeug-Werke based on Hansa-Brandenburg designs which it has produced under licence.<ref name="Lamberton">Lamberton, 1960. p 22.</ref> The D.I was a single-seat biplane fighter with improvements over the original Hansa-Brandenburg design which included more efficient wings, a more powerful engine and structural improvements.<ref name="Lamberton"/> A prototype was first flown in 1917 and proved to be fast but difficult to handle but because of the urgent need for fighters the D.I entered production. To improve the problems a modified variant, the '''D.II''' was introduced with balanced elevators and balanced ailerons on the upper wings. A further development was the '''D.III''' which had balanced ailerons on both wings and a more powerful 230&nbsp;hp (172&nbsp;kW) Hiero in-line engine. The last of 158 aircraft of all three types was delivered on 4 November 1918.{{Citation needed|date=November 2014}}
   
 
==Variants==
 
==Variants==
Line 43: Line 41:
 
*[[Royal Yugoslav Air Force]] - Postwar.
 
*[[Royal Yugoslav Air Force]] - Postwar.
   
==Specifications (D.1) ==
+
==Specifications (D.1)==
 
{{aerospecs
 
{{aerospecs
 
|ref=Orbis 1985, page 2700
 
|ref=Orbis 1985, page 2700
Line 55: Line 53:
 
|span ft=31
 
|span ft=31
 
|span in=11¾
 
|span in=11¾
|width m=<!-- if applicable -->
+
|width m=
|width ft=<!-- if applicable -->
+
|width ft=
|width in=<!-- if applicable -->
+
|width in=
 
|height m=2.80
 
|height m=2.80
 
|height ft=9
 
|height ft=9
Line 73: Line 71:
 
|eng2 number=
 
|eng2 number=
 
|eng2 type=
 
|eng2 type=
|eng2 kw=<!-- prop engines -->
+
|eng2 kw=
|eng2 hp=<!-- prop engines -->
+
|eng2 hp=
 
|max speed kmh=180
 
|max speed kmh=180
 
|max speed mph=112
 
|max speed mph=112
|cruise speed kmh=<!-- if max speed unknown -->
+
|cruise speed kmh=
|cruise speed mph=<!-- if max speed unknown -->
+
|cruise speed mph=
|stall speed kmh=<!-- aerobatic and STOL aircraft -->
+
|stall speed kmh=
|stall speed mph=<!-- aerobatic and STOL aircraft -->
+
|stall speed mph=
 
|range km=
 
|range km=
 
|range miles=
 
|range miles=
|endurance h=<!-- if range unknown -->2
+
|endurance h=2
|endurance min=<!-- if range unknown -->0
+
|endurance min=0
 
|ceiling m=6000
 
|ceiling m=6000
 
|ceiling ft=19,685
 
|ceiling ft=19,685
|g limits=<!-- aerobatic aircraft -->
+
|g limits=
|roll rate=<!-- aerobatic aircraft -->
+
|roll rate=
 
|climb rate ms=
 
|climb rate ms=
 
|climb rate ftmin=
 
|climb rate ftmin=
Line 97: Line 95:
 
|armament5=
 
|armament5=
 
|armament6=
 
|armament6=
}}
 
<!-- ==See also== -->
 
{{aircontent
 
<!-- include as many lines are appropriate. additional lines/entries with carriage return. -->
 
|see also=
 
|related=<!-- related developments -->
 
|similar aircraft=<!-- similar or comparable aircraft -->
 
|lists=<!-- related lists -->
 
 
}}
 
}}
   
Line 112: Line 102:
 
===Bibliography===
 
===Bibliography===
 
{{refbegin}}
 
{{refbegin}}
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages= }}
+
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London}}
*{{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
+
*{{cite book |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing}}
 
* {{cite book |last= Lamberton |first= W.M. |title=Fighter Aircraft of the 1914-1918 War |year=1960 |publisher=Harleyford Publications Ltd. |location=Herts |pages= 22–23}}
 
* {{cite book |last= Lamberton |first= W.M. |title=Fighter Aircraft of the 1914-1918 War |year=1960 |publisher=Harleyford Publications Ltd. |location=Herts |pages= 22–23}}
 
{{refend}}
 
{{refend}}
<!-- ==External links== -->
 
 
 
{{KuKLFT D-class designations}}
 
{{KuKLFT D-class designations}}
 
{{Swedish fighter aircraft}}
 
{{Swedish fighter aircraft}}
  +
{{Aviation lists}}
 
  +
{{Wikipedia|Phönix D.I}}
   
 
{{DEFAULTSORT:Phonix D.I}}
 
{{DEFAULTSORT:Phonix D.I}}
[[Category:Austro-Hungarian fighter aircraft 1910–1919]]
+
[[Category:1910s Austro-Hungarian fighter aircraft]]
 
[[Category:Phönix aircraft|D01]]
 
[[Category:Phönix aircraft|D01]]
 
[[Category:Single-engined tractor aircraft]]
 
[[Category:Single-engined tractor aircraft]]

Latest revision as of 19:58, 1 February 2020

Phönix D.I, D.II, and D.III
Phönix D.I 228.45
Phönix D.I
Role Biplane fighter
National origin Austria-Hungary
Manufacturer Phönix Flugzeug-Werke
First flight 1917
Primary user KuKLFT
Number built 158

The Phönix D.I was an Austro-Hungarian First World War biplane fighter built by the Phönix Flugzeug-Werke and based on the Hansa-Brandenburg D.I.[1]

Development

The Phönix D.I was the second design developed by the Phönix Flugzeug-Werke based on Hansa-Brandenburg designs which it has produced under licence.[2] The D.I was a single-seat biplane fighter with improvements over the original Hansa-Brandenburg design which included more efficient wings, a more powerful engine and structural improvements.[2] A prototype was first flown in 1917 and proved to be fast but difficult to handle but because of the urgent need for fighters the D.I entered production. To improve the problems a modified variant, the D.II was introduced with balanced elevators and balanced ailerons on the upper wings. A further development was the D.III which had balanced ailerons on both wings and a more powerful 230 hp (172 kW) Hiero in-line engine. The last of 158 aircraft of all three types was delivered on 4 November 1918.[citation needed]

Variants

D.I
Initial production variant with a 200hp (149kW) Hiero inline engine.[2]
D.II
Improved variant with balanced elevators and balanced ailerons on the upper wings.[2]
D.III
Improved variant with balanced ailerons on both wings and powered by a 230hp (172kW) Hiero in-line engine.[2]

Operators

Phonix D III

Phönix D.III of the Swedish Air Force

Flag of Austria-Hungary 1869-1918 Austria-Hungary
Flag of Sweden Sweden
Flag of the Kingdom of Yugoslavia Kingdom of Yugoslavia

Specifications (D.1)

Data from Orbis 1985, page 2700

General characteristics

  • Crew: 1
  • Length: 6.65 m (21 ft 9¾ in)
  • Wingspan: 9.75 m (31 ft 11¾ in)
  • Height: 2.80 m (9 ft 2¼ in)
  • Gross weight: 805 kg (1775 lb)
  • Powerplant: 1 × Hiero 6-cylinder inline piston, 149 kW (200 hp)

Performance

  • Maximum speed: 180 km/h (112 mph)
  • Endurance: 2 hours  0 min
  • Service ceiling: 6000 m (19,685 ft)

Armament

  • 2 x Synchronised fixed forward-firing 8 mm Schwarzlose machine guns
  • References

    1. "Phönix D.I". The Aerodome. http://www.theaerodrome.com/aircraft/austrhun/phonix_di.php. Retrieved 25 April 2013. 
    2. 2.0 2.1 2.2 2.3 2.4 Lamberton, 1960. p 22.

    Bibliography

    • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. 
    • The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. 
    • Lamberton, W.M. (1960). Fighter Aircraft of the 1914-1918 War. Herts: Harleyford Publications Ltd.. pp. 22–23. 
    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 Phönix D.I and the edit history here.