Statements (18)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:countryOfOrigin |
gptkb:United_States
|
| gptkbp:developedBy |
gptkb:US_Air_Force
|
| gptkbp:diameter |
48 in
|
| gptkbp:firstFlight |
1970
|
| https://www.w3.org/2000/01/rdf-schema#label |
General Electric F101
|
| gptkbp:length |
180 in
|
| gptkbp:manufacturer |
gptkb:General_Electric
|
| gptkbp:numberOfStages |
9
|
| gptkbp:relatedTo |
gptkb:General_Electric_F110
gptkb:General_Electric_F118 |
| gptkbp:status |
in service
|
| gptkbp:thrust |
30,000 lbf
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedIn |
gptkb:Rockwell_B-1_Lancer
|
| gptkbp:bfsParent |
gptkb:General_Electric_F101-GE-102
|
| gptkbp:bfsLayer |
7
|