Sikorsky_CH-53E_Super_Stallion
predecessor
Wikipage disambiguates
developed into
major applications
primaryTopic
Sikorsky_CH-53E_Super_Stallion
has abstract
CH-53Eは、シコルスキー・エアクラフト・ディビジョン社が ...... 後継機として作られた、現在西側諸国最大のヘリコプターである。
@ja
El Sikorsky CH-53E Super Stall ...... estos, y una cabina más ancha.
@es
Il Sikorsky S-80 (noto con den ...... posito e una cabina più ampia.
@it
Le Sikorsky CH-53E Super Stall ...... (AMCM) et de transport lourd.
@fr
O Sikorsky CH-53E Super Stalli ...... s e maior capacidade de carga.
@pt
Sikorsky CH-53 Sea Stallion – ...... maga 44 roboczogodzin obsługi.
@pl
The Sikorsky CH-53E Super Stal ...... s, and a wider aircraft cabin.
@en
سيكورسكي سي إتش-53 إي سوبر ستا ...... لمواد المركبة، مع مقصورة أوسع.
@ar
西科斯基CH-53E超級种马(Sikorsky CH-53E ...... 7500轴马力的涡轴发动机,新型旋翼材料和���宽敞的机舱。
@zh
number built
predecessor
production end year
production start year
unit cost ($)
Link from a Wikipage to an external page
Wikipage page ID
Wikipage revision ID
741,653,102
area alt
area main
capacity
ceiling alt
ceiling main
climb rate alt
climb rate main
cruise speed alt
cruise speed main
developed into
empty weight alt
empty weight main
engine(prop)_
ferry range alt
ferry range main
first flight
1974-03-01
guns
** 2× .50 BMG window-mounted ...... er: Chaff and flare dispensers
height alt
height main
introduced
jetOrProp%3F_
length alt
length main
lists
* List of active United States military aircraft
* List of rotorcraft
max speed alt
max speed main
max takeoff weight alt
max takeoff weight main
more general
Rotor systems: 7 blades on main rotor, 4 blades on anti-torque tail rotor
more users
Japan Maritime Self-Defense Force
number of props
payload alt
external: 36,000 lb or 14,500 kg
payload main
internal: 30,000 lb or 13,600 kg