|
gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:airlines
|
40 kg/s
|
|
gptkbp:commissioningDate
|
1947
|
|
gptkbp:compressionRatio
|
7:1
|
|
gptkbp:controls
|
hydraulic
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
post-World_War_II
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_3
|
|
gptkbp:engine
|
550 kg
starter motor
|
|
gptkbp:engineConfiguration
|
single-spool
|
|
gptkbp:engineType
|
axial-flow
|
|
gptkbp:exhaustSystem
|
straight
|
|
gptkbp:firstFlight
|
1949
1990s
|
|
gptkbp:fuelCapacity
|
0.5 kg/s
|
|
gptkbp:fuelType
|
annular
spark plug
kerosene
|
|
gptkbp:generator
|
1,200 K
|
|
gptkbp:hasContent
|
0.85 kg/(kN·h)
|
|
gptkbp:historicalSignificance
|
first Polish turbojet engine.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
WP-13 turbojet
|
|
gptkbp:length
|
3.4 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
WSK PZL Rzeszów
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:notableUsers
|
gptkb:Polish_Air_Force
|
|
gptkbp:numberOfStudents
|
5
|
|
gptkbp:operationalArea
|
military aviation
|
|
gptkbp:operationalRange
|
1,000 km
|
|
gptkbp:operationalStatus
|
retired
|
|
gptkbp:propulsion
|
5:1
3,000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:relatedPatent
|
RD-500
|
|
gptkbp:revenue
|
1950
|
|
gptkbp:services
|
12,000 m
|
|
gptkbp:successor
|
WP-14 turbojet
|
|
gptkbp:totalGoals
|
over 1,000 units
|
|
gptkbp:usedIn
|
gptkb:Mikoyan-Gurevich_MiG-15
|
|
gptkbp:variant
|
WP-13B
WP-13C
WP-13A
|
|
gptkbp:weight
|
600 kg
|