Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:application |
military aviation
|
| gptkbp:controls |
manual
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
3 ft 6 in
|
| gptkbp:engine |
military service
advanced technology fighter aircraft innovative features pylon-mounted large dimensions influential engine Rolls-Royce_design |
| gptkbp:engineConfiguration |
limited production
turbojet developed_in_UK |
| gptkbp:engineType |
axial
air start several variants single_spool |
| gptkbp:exhaustSystem |
straight
|
| gptkbp:firstFlight |
1948
|
| gptkbp:fuel_capacity |
0.8 lb/hp/hr
|
| gptkbp:fuelType |
annular
spark plug kerosene |
| gptkbp:hasArea |
ground testing
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mamba Mk III
|
| gptkbp:is_used_in |
gptkb:de_Havilland_Vampire
de Havilland Venom |
| gptkbp:length |
12 ft 6 in
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:noise_level |
high noise level
|
| gptkbp:number_of_stages |
8
|
| gptkbp:operational_status |
1950s
|
| gptkbp:operationalHistory |
historical significance
|
| gptkbp:performances |
high performance
high reliability moderate maintenance performance metrics available detailed specifications distinct characteristics |
| gptkbp:productionYears |
produced in 1950s
|
| gptkbp:propulsion |
2.5
3,000 lbf |
| gptkbp:related_engine |
gptkb:Rolls-Royce_Derwent
gptkb:Rolls-Royce_Nene Brayton_cycle |
| gptkbp:successor |
gptkb:Mamba_Mk_IV
|
| gptkbp:type |
turbojet engine
|
| gptkbp:updates |
upgraded versions
|
| gptkbp:weight |
1,200 lb
|