Gnome Mk 104

URI: https://gptkb.org/entity/Gnome_Mk_104
GPTKB entity
Statements (57)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 6
gptkbp:bfsParent gptkb:Rolls-Royce_Gnome
gptkbp:application gptkb:aircraft
gptkbp:certification military certification required
gptkbp:compression_ratio 5.5:1
gptkbp:cooling_system air-cooled
gptkbp:date 1916
gptkbp:displacement 14.5 L
gptkbp:engine gptkb:aircraft
gptkb:television_series
gptkb:Gnome_series
gptkb:Gnome_9_N
gptkb:engine
lightweight design
high reliability
100 hp
high power-to-weight ratio
two-stroke
horizontally opposed
detailed specifications available
produced in large numbers
every 500 hours
designed for reliability
used in early aviation
developed during WWI
100 hp output
1500 rpm
Mk 104
characterized by rotary motion
influenced rotary engine design
widely used in France
gptkbp:engine_type gptkb:engine
Gnome 7
Gnome 9 N variant available
gptkbp:first_flight gptkb:1917
gptkbp:fuel_capacity 120 kg
40 L/h
1.2 m diameter
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Gnome Mk 104
gptkbp:ignition_system magneto
magneto ignition
gptkbp:is_tested_for bench testing required
gptkbp:maintenance 100 hours
routine checks
gptkbp:manufacturer gptkb:Gnome_et_Rhône
gptkbp:notable_users gptkb:French_Air_Force
gptkbp:operational_history gptkb:World_War_I
gptkbp:power_output 100 hp
gptkbp:propulsion fixed-pitch
gptkbp:setting gptkb:engine
gptkbp:successor gptkb:Gnome_Omega
gptkbp:torque 200 Nm
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:aircraft
gptkbp:weight 120 kg