Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft wing design
|
| gptkbp:benefit |
up to 10% fuel savings
|
| gptkbp:category |
aeronautical engineering
experimental aircraft technology |
| gptkbp:developedBy |
gptkb:NASA
gptkb:Boeing |
| gptkbp:feature |
high aspect ratio
long, thin wings truss support structure |
| https://www.w3.org/2000/01/rdf-schema#label |
Transonic Truss-Braced Wing
|
| gptkbp:notableProject |
gptkb:Sustainable_Flight_Demonstrator
|
| gptkbp:purpose |
increase fuel efficiency
reduce drag |
| gptkbp:relatedTo |
gptkb:Boeing_X-66
NASA Sustainable Flight National Partnership |
| gptkbp:status |
in development
|
| gptkbp:targetAircraftType |
single-aisle airliner
|
| gptkbp:targetSpeed |
Mach 0.80
|
| gptkbp:testbedAircraft |
Boeing X-66A
|
| gptkbp:unveiled |
2019
|
| gptkbp:wingspan |
170 feet (approximate)
|
| gptkbp:bfsParent |
gptkb:Sustainable_Flight_Demonstrator
|
| gptkbp:bfsLayer |
8
|