Eurocopter AS555 Fennec - přehled verzí : Eurocopter / Airbus Helicopters

Aerospatiale/Eurocopter AS355 Écureuil 2, TwinStar - track version[/heading]
AS 355E Écureuil 2 - twin variant of the light multirole helicopter AS 350, engines Allison 250-C20F; approx 65 pcs
AS 355F Écureuil 2 - a variant with wider rotor blades and twin controls, higher takeoff weight; approx 170 pcs
AS 355F1 Écureuil 2 - the wider tail rotor blades, reinforced transmission, a higher takeoff weight; approx 70 + 200 conversion 355E/355F
AS 355F2 Écureuil 2 - further adjustments leading to an increase in take-off weight; about 130 + 60 conversions
AS 355M Écureuil 2 - the military variant of the F1/F2 for the French air force, completed as 555AN
AS 355N Écureuil 2 - variant of the corresponding F2 with engines Turboméca Arrius 1A; approx 180 pcs
AS 355NP Écureuil 2 - modernized variant with engines Turboméca Arrius 1A1; approx 70 pcs

AS 555 TwinStar - name for the north american market

AS 555AN Fennec - armed multi-purpose version of the 355N for the French air force; 44 pcs
AS 555UN Fennec - unarmed multi-purpose version of the 355N for the French army air force; 18 pcs
AS 555MN Fennec - unarmed maritime multi-purpose version 355N, nestavěna
AS 555SN Fennec - a naval ship-to-ship multi-purpose version 355N, 13 pcs

Twin Squirrel HCC.1 - three 555F1 leased to the RAF for VIP transport

HB.355F2 Esquilo Biturbina - brazilian licensed version of the F2, 27 pcs
CH-55 - the markings of the brazilian air force for the 10 HB.355F2
UH-13 - the designation of the brazilian navy for 11 HB.355F2

Taylor, John W. R. Jane's All the World's Aircraft 1979-80. Macdonald and Jane's, London 1979. ISBN: 0-531-03915-3.
Taylor, John W. R. Jane's All the World's Aircraft 1986-87. Jane's Publishing Company, London 1986. ISBN 0-7106-0835-7.
Lambert, Mark. Jane's All the World's Aircraft 1991-1992. Jane's Information Group, Coulsdon 1991. ISBN 0-7106-0965-5.
Jackson, Paul. Jane's All the World's Aircraft 2004-2005. Jane's Information Group, Coulsdon 2004.
http://www.rotorspot.nl/product/as355.php
www.helis.com
http://helimat.free.fr/ecureuil_familly.htm
www.aviationsmilitaires.net

URL : https://www.valka.cz/Eurocopter-AS355-Ecureuil-2-t8722#605258 Version : 0

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77 - Vrtulník / Helicopter

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Czech transcription
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English transcription
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Název:
Name:

Originální název:
Original Name:

Kategorie:
Category:

Výrobce:
Producer:

From:

To:

Výrobce/Producer

Obec/City

Vlajky/Flags

Období výroby:
Production Period:

From:

Do:

Vyrobeno kusů:
Number of Produced:

První vzlet:
Maiden Flight:

Osádka:
Crew:

Základní charakteristika:
Basic Characteristics:

Uspořádání rotorů:
Rotor Configuration:

Podvozek:
Undercarriage:

Přistávací zařízení:
Landing Gear:

Technické údaje:
Technical Data:

Hmotnost prázdného vrtulníku:
Empty Weight:

(kg)

(lb)

Vzletová hmotnost:
Take-off Weight:

(kg)

(lb)

Maximální vzletová hmotnost:
Maximum Take-off Weight:

(kg)

(lb)

Délka s otáčejícími se rotory:
Length with Rotors Turning:

(m)

(ft in)

Délka trupu:
Fuselage Length:

(m)

(ft in)

Šířka trupu:
Fuselage Width:

(m)

(ft in)

Celková výška:
Overall Height:

(m)

(ft in)

Průměr hlavního rotoru:
Main Rotor Diameter:

(m)

(ft in)

Průměr vyrovnávacího rotoru:
Tail Rotor Diameter:

(m)

(ft in)

Plocha disku hlavního rotoru:
Main Rotor Disc Area:

(m²)

(ft²)

Plocha disku vyrovnávacího rotoru:
Tail Rotor Disc Area:

(m²)

(ft²)

Pohon:
Propulsion:

Kategorie:
Category:

Počet motorů:
Number of engines:

Typ:
Type:

Objem palivových nádrží:
Fuel Tank Capacity:

Výkony:
Performance:

Maximální rychlost:
Maximum Speed:

(km/h) ve výšce

(m)

(mph) in

(ft)

Cestovní rychlost:
Cruise Speed:

(km/h) ve výšce

(m)

(mph) in

(ft)

Rychlost stoupání:
Climb Rate:

(m/s)

(ft/min)

Statický dostup:
Static Ceiling:

(m)

(ft)

Dynamický dostup:
Dynamic Ceiling:

(m)

(ft)

Dolet:
Range:

(km)

(mi)

Maximální dolet:
Maximum Range:

(km)

(mi)

Přepravní kapacita:
Transport Capacity:

Výzbroj a vybavení:
Armament and Equipment:

Výzbroj:
Armament:

Vybavení:
Equipment:

Uživatelské státy:
User States:

Poznámka:
Note:

Zdroje:
Sources:

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