NO TAil Rotor (NOTAR) system
GPTKB entity
Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
helicopter anti-torque system
|
| gptkbp:advantage |
reduced noise
increased safety lower maintenance |
| gptkbp:alternativeTo |
gptkb:Fenestron
conventional tail rotor |
| gptkbp:category |
aerospace engineering
helicopter technology |
| gptkbp:developedBy |
gptkb:McDonnell_Douglas_Helicopter_Systems
|
| gptkbp:firstFlight |
1981
|
| gptkbp:function |
provides anti-torque control
replaces conventional tail rotor |
| https://www.w3.org/2000/01/rdf-schema#label |
NO TAil Rotor (NOTAR) system
|
| gptkbp:mechanismOfAction |
uses directed jet of air
utilizes Coandă effect |
| gptkbp:notableAircraft |
gptkb:MD_520N
gptkb:MD_600N gptkb:MD_Explorer |
| gptkbp:patent |
1983
|
| gptkbp:usedIn |
gptkb:MD_Explorer
gptkb:MD_Helicopters_MD_600N MD Helicopters MD 520N |
| gptkbp:bfsParent |
gptkb:MD_520N
|
| gptkbp:bfsLayer |
7
|