Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:assemblyLocation |
gptkb:Indianapolis,_Indiana,_USA
|
| gptkbp:basedOn |
gptkb:Rolls-Royce_BR700
|
| gptkbp:bypassRatio |
high-bypass
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
gptkb:United_States |
| gptkbp:criteria |
gptkb:United_States_Air_Force
2021 |
| gptkbp:diameter |
about 0.54 m
|
| gptkbp:family |
gptkb:BR700_engine_family
|
| gptkbp:firstFlight |
not yet flown on B-52 as of 2024
|
| gptkbp:hasConcept |
two-shaft
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce F130
|
| gptkbp:intendedUse |
B-52 Stratofortress
|
| gptkbp:length |
about 2.6 m
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_North_America
|
| gptkbp:numberOfEnginesOrdered |
608
|
| gptkbp:primaryUse |
B-52 re-engining program
|
| gptkbp:replacedBy |
gptkb:Pratt_&_Whitney_TF33
|
| gptkbp:status |
in development
|
| gptkbp:targetUser |
$2.6 billion (initial)
|
| gptkbp:thrust |
about 17,000 lbf
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_jet_engines
|
| gptkbp:bfsLayer |
8
|