Sikorsky S-20: Difference between revisions
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{|{{Infobox Aircraft Begin |
{|{{Infobox Aircraft Begin |
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|name = RBVZ S-XX |
|name = RBVZ S-XX |
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|image = |
|image =File:06072007-sikorskiy20-1.jpg |
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|caption = |
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|manufacturer = [[RBVZ]] (Russo-Baltic Wagon Works) |
|manufacturer = [[RBVZ]] (Russo-Baltic Wagon Works) |
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|designer = [[Igor Sikorsky]] |
|designer = [[Igor Sikorsky]] |
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|first flight = |
|first flight = 1916 |
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|introduced = |
|introduced = 1916 |
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|retired = |
|retired = 1920 |
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|status = |
|status = |
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|primary user = [[Imperial Russian Air Service]] |
|primary user = [[Imperial Russian Air Service]] |
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|more users = |
|more users = |
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|produced = |
|produced = |
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|number built =5 |
|number built =5 |
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|unit cost = |
|unit cost = |
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|variants with their own articles = |
|variants with their own articles = |
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}} |
}} |
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The '''Sikorsky S-20''' (named after its designer) or '''RBVZ S-XX''' (named after its manufacturer) was a Russian single-bay |
The '''Sikorsky S-20''' (named after its designer) or '''RBVZ S-XX''' (named after its manufacturer) was a Russian [[single-bay]] unequal span two-seat biplane designed by [[Igor Sikorsky]] in 1916. Displaying some [[Nieuport]] influence, it saw very little service during [[World War I]]. |
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Five S-XX aircraft were built in September 1916, with the first two powered by the 100 hp Gnome rotary engine which had powered its predecessor, the [[RBVZ S-XVI]]. However, the other three were powered with the 120 hp Le Rhone engine, with which they were allegedly faster than the French [[Nieuport 17]]. |
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== Operational History== |
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The S-XX saw little service due to it being viewed as inferior to newer enemy aircraft and no series production was undertaken. As such only 5 aircraft were ever produced. |
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==Operational history== |
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== List of operators == |
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The S-XX saw little service because it was viewed as inferior{{Citation needed|reason=Contradicts with russian source|date=October 2024}} to newer enemy aircraft, and no series production was undertaken. As such, only five aircraft were ever produced. |
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==List of operators== |
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; {{flag|Russian Empire|1914}} |
; {{flag|Russian Empire|1914}} |
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* [[Imperial Russian Air Service]] |
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==Specifications== |
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{{Aircraft specs |
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{{aircraft specifications| |
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|ref=<!-- reference --> |
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|crew= |
|crew= |
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|capacity= |
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|span main=8.60m |
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|length m=6.5 |
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|span alt=28 ft 2½ in |
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|length note= |
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|area main=17m² |
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|span m=8.6 |
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|area alt=182.99 ft² |
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|span note= |
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|length main=6.50m |
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|height m=2.6 |
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|length alt=21 ft 3⅞ in |
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|height |
|height note= |
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|wing area sqm=17 |
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|height alt= |
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|wing area note= |
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|empty weight main=395 kg |
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|aspect ratio=<!-- sailplanes --> |
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|empty weight alt= 871 lb |
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|airfoil=<!--'''root:''' [[NACA airfoil|NACA ]]; '''tip:''' [[NACA airfoil|NACA ]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}</ref>--> |
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|loaded weight main=570 kg |
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|empty weight kg=395 |
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|empty weight note= |
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|gross weight kg=570 |
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|gross weight note= |
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|max takeoff weight kg= |
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|max takeoff weight note= |
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|fuel capacity= |
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|more general= |
|more general= |
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|engine (prop)=120hp Le Rhône |
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Powerplant |
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|type of prop=air-cooled [[rotary engine]] |
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|number of props=1 |
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|eng1 number=1 |
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|power main=90 kW |
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|eng1 name=[[Le Rhône Type 9Jb]] |
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|power alt=120 hp |
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|eng1 type=9-cylinder air-cooled rotary piston engine |
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|max speed main=190 km/h |
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|eng1 hp=120 |
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|max speed alt=118 mph |
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|eng1 note= |
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|max speed more= |
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|range main= |
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|prop blade number=2 |
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|range alt= |
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|prop name=fixed-pitch propeller |
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|ceiling main= |
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|prop dia m=<!-- propeller aircraft --> |
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|loading alt= |
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|max speed kmh=180 |
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|power/mass main= |
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|power/mass alt= |
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|cruise speed kmh= |
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|cruise speed note= |
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|stall speed kmh= |
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|stall speed note= |
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|never exceed speed kmh= |
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|never exceed speed note= |
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|range km=390 |
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|range note= |
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|combat range km= |
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|combat range note= |
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|ferry range km= |
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|ferry range note= |
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|endurance=<!-- if range unknown --> |
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|ceiling m=5600 |
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|ceiling note= |
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|climb rate ms= |
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|climb rate note= |
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|time to altitude={{cvt|2000|m}} in 6 minutes 20 seconds |
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|wing loading kg/m2=33.0 |
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|wing loading note= |
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|fuel consumption kg/km= |
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|power/mass=0.21 hp/kg |
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|more performance= |
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* '''Endurance:''' |
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Armament |
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* '''Climb to 2,000 m (6,560 ft):''' 6.33 minutes |
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|guns=1 x 7.7 mm Lavrov machine gun}} |
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|guns=1 x 7.7 mm [[Lavrov machine gun]] |
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}} |
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==References== |
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{{citations|date=March 2016}} |
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* William Green and Gordon Swanborough. ''The Complete Book of Fighters''. Colour Library Direct, Godalming, UK: 1994. ISBN 1-85833-777-1. |
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{{reflist}} |
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===Bibliography=== |
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{{commons category|Sikorsky S-20}} |
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* William Green and Gordon Swanborough. ''The Complete Book of Fighters''. Colour Library Direct, Godalming, UK: 1994. {{ISBN|1-85833-777-1}}. |
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{{Sikorsky Aircraft}} |
{{Sikorsky Aircraft}} |
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{{aviation lists}} |
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[[Category:Russian fighter aircraft 1910-1919]] |
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[[Category:Sikorsky Aircraft]] |
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[[Category:1910s Russian fighter aircraft]] |
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[[cs:Sikorskij S-XX]] |
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[[Category:Sikorsky aircraft|S-020]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Rotary-engined aircraft]] |
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[[Category:Biplanes]] |
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[[Category:Aircraft first flown in 1916]] |
Latest revision as of 12:25, 24 October 2024
RBVZ S-XX | |
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Role | Fighter |
Manufacturer | RBVZ (Russo-Baltic Wagon Works) |
Designer | Igor Sikorsky |
First flight | 1916 |
Introduction | 1916 |
Retired | 1920 |
Primary user | Imperial Russian Air Service |
Number built | 5 |
The Sikorsky S-20 (named after its designer) or RBVZ S-XX (named after its manufacturer) was a Russian single-bay unequal span two-seat biplane designed by Igor Sikorsky in 1916. Displaying some Nieuport influence, it saw very little service during World War I.
Five S-XX aircraft were built in September 1916, with the first two powered by the 100 hp Gnome rotary engine which had powered its predecessor, the RBVZ S-XVI. However, the other three were powered with the 120 hp Le Rhone engine, with which they were allegedly faster than the French Nieuport 17.
Operational history
[edit]The S-XX saw little service because it was viewed as inferior[citation needed] to newer enemy aircraft, and no series production was undertaken. As such, only five aircraft were ever produced.
List of operators
[edit]Specifications
[edit]General characteristics
- Length: 6.5 m (21 ft 4 in)
- Wingspan: 8.6 m (28 ft 3 in)
- Height: 2.6 m (8 ft 6 in)
- Wing area: 17 m2 (180 sq ft)
- Empty weight: 395 kg (871 lb)
- Gross weight: 570 kg (1,257 lb)
- Powerplant: 1 × Le Rhône Type 9Jb 9-cylinder air-cooled rotary piston engine, 89 kW (120 hp)
- Propellers: 2-bladed fixed-pitch propeller
Performance
- Maximum speed: 180 km/h (110 mph, 97 kn)
- Range: 390 km (240 mi, 210 nmi)
- Service ceiling: 5,600 m (18,400 ft)
- Time to altitude: 2,000 m (6,600 ft) in 6 minutes 20 seconds
- Wing loading: 33.0 kg/m2 (6.8 lb/sq ft)
- Power/mass: 0.21 hp/kg
Armament
- Guns: 1 x 7.7 mm Lavrov machine gun
References
[edit]This article includes a list of references, related reading, or external links, but its sources remain unclear because it lacks inline citations. (March 2016) |
Bibliography
[edit]- William Green and Gordon Swanborough. The Complete Book of Fighters. Colour Library Direct, Godalming, UK: 1994. ISBN 1-85833-777-1.