|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Dassault_Mystère_IV
gptkb:Dassault_Mystère
|
|
gptkbp:aircraft_operated
|
Dassault Super Mystère
|
|
gptkbp:controls
|
hydraulic control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:developer
|
SNECMA Atar series
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
high
|
|
gptkbp:engine
|
gptkb:musical
gptkb:Pratt_&_Whitney_J57
gptkb:Rolls-Royce_Avon
Brayton cycle
axial-flow
air start
|
|
gptkbp:engine_type
|
2
8
turbojet
Atar 101
Atar 102
Atar 103
Atar 104
Atar 105
Atar 106
Atar 107
Atar 108
Atar 109
Atar 110
Atar 111
Atar 112
Atar 113
Atar 114
Atar 115
Atar 116
Atar 117
Atar 118
Atar 119
Atar 120
|
|
gptkbp:first_flight
|
gptkb:1954
|
|
gptkbp:fuel_capacity
|
0.9 m
1,200 kg
4.1 m
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
annular combustion chamber
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
SNECMA Atar 101
|
|
gptkbp:introduced
|
gptkb:1954
|
|
gptkbp:length
|
4.1 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:SNECMA
|
|
gptkbp:max_speed
|
Mach 2.2
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_feature
|
afterburner capability
|
|
gptkbp:operational_history
|
used in various military aircraft
|
|
gptkbp:propulsion
|
4.2
50 k N
|
|
gptkbp:retired
|
1970s
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:successor
|
SNECMA Atar 09
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:used_in
|
gptkb:Dassault_Mirage_III
|
|
gptkbp:water_source
|
1,000 kg/h
|
|
gptkbp:weight
|
1,200 kg
|