Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:anti-torque_system
|
| gptkbp:advantage |
reduced noise
increased safety lower maintenance |
| gptkbp:category |
helicopter technology
|
| gptkbp:component |
direct jet thruster at tail end
fan inside tail boom slots along tail boom |
| gptkbp:developedBy |
gptkb:MD_Helicopters
|
| gptkbp:firstFlight |
1981
|
| gptkbp:operates |
gptkb:Coandă_effect
|
| gptkbp:patent |
1983
|
| gptkbp:provides |
yaw control
|
| gptkbp:removes |
conventional tail rotor
|
| gptkbp:standsFor |
No Tail Rotor
|
| gptkbp:usedIn |
helicopters
|
| gptkbp:usedOn |
gptkb:MD_520N
gptkb:MD_600N gptkb:MD_Explorer |
| gptkbp:bfsParent |
gptkb:MD_600N
gptkb:MD_900 gptkb:MD_902_Explorer |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
NOTAR anti-torque system
|