Tumansky R-29-300

GPTKB entity

Statements (59)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
gptkbp:combustor_type annular
gptkbp:compressor_type axial
gptkbp:cooling_system air-cooled
gptkbp:design_date gptkb:1958
gptkbp:diameter 1.1 m
gptkbp:engine Brayton cycle
gptkbp:engine_configuration twin-shaft
gptkbp:engine_type R-29-300 A
R-29-300 B
R-29-300 C
R-29-300 D
R-29-300 E
R-29-300 F
R-29-300 G
R-29-300 H
R-29-300 I
R-29-300 J
R-29-300 K
R-29-300 L
R-29-300 M
R-29-300 N
R-29-300 O
R-29-300 P
R-29-300 Q
R-29-300 R
R-29-300 S
R-29-300 T
R-29-300 U
R-29-300 V
R-29-300 W
R-29-300 X
R-29-300 Y
R-29-300 Z
gptkbp:first_flight gptkb:1964
gptkbp:fuel_economy 0.85 kg/k N·h
gptkbp:fuel_type kerosene
https://www.w3.org/2000/01/rdf-schema#label Tumansky R-29-300
gptkbp:length 4.1 m
gptkbp:manufacturer Tumansky
gptkbp:max_speed Mach 3.2
gptkbp:notable_users gptkb:Egypt
gptkb:India
gptkb:Syria
gptkb:Iraq
gptkb:Libya
gptkbp:operational_use gptkb:Soviet_Air_Force
gptkbp:propulsion 20:1
30000 lbf
gptkbp:related_aircraft gptkb:Mi_G_family
gptkbp:service_ceiling 25000 m
gptkbp:successor gptkb:Tumansky_R-33
gptkbp:turbine_type single spool
gptkbp:type turbojet
gptkbp:used_in gptkb:Mikoyan_Mi_G-25
gptkbp:weight 1500 kg
gptkbp:bfsParent gptkb:Mi_G-27_Flogger
gptkbp:bfsLayer 5