Rolls-Royce Orpheus turbojet
GPTKB entity
Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:aircraft
gptkb:trainer_aircraft |
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:designer |
gptkb:Dr._Stanley_Hooker
|
| gptkbp:developedBy |
gptkb:Rolls-Royce_Nene
|
| gptkbp:diameter |
24 in
|
| gptkbp:firstRun |
1954
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Orpheus turbojet
|
| gptkbp:length |
86 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFor |
simplicity and reliability
|
| gptkbp:numberOfStages |
2
7 |
| gptkbp:status |
out of production
|
| gptkbp:successor |
gptkb:Rolls-Royce_Viper
|
| gptkbp:thrust |
4,850 lbf
|
| gptkbp:type |
single-spool turbojet
|
| gptkbp:usedInAircraft |
gptkb:Fiat_G.91
gptkb:Aermacchi_MB-326 gptkb:Folland_Gnat gptkb:HAL_HF-24_Marut |
| gptkbp:weight |
850 lb
|
| gptkbp:bfsParent |
gptkb:Vampire_dragster
|
| gptkbp:bfsLayer |
6
|