Bristol Siddeley Orpheus engine
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
light fighter aircraft
|
| gptkbp:diameter |
22 in
|
| gptkbp:firstRun |
1954
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Siddeley Orpheus engine
|
| gptkbp:length |
86 in
|
| gptkbp:manufacturer |
gptkb:Bristol_Siddeley
|
| gptkbp:notableFor |
simplicity and reliability
|
| gptkbp:numberOfStages |
1
7 |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:Rolls-Royce_Viper
|
| gptkbp:thrust |
4,520 lbf
|
| gptkbp:type |
turbojet
|
| gptkbp:usedInAircraft |
gptkb:Fiat_G.91
gptkb:Folland_Gnat gptkb:HAL_HF-24_Marut Ajeet |
| gptkbp:weight |
850 lb
|
| gptkbp:bfsParent |
gptkb:Aerospace_Bristol
|
| gptkbp:bfsLayer |
6
|