|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:T-14_Armata_tank
gptkb:T-14_Armata
|
|
gptkbp:aircraft_operated
|
100 A
|
|
gptkbp:application
|
marine propulsion
|
|
gptkbp:availability
|
high
|
|
gptkbp:bore
|
4.0 in
|
|
gptkbp:breathability
|
turbocharged
|
|
gptkbp:color
|
gptkb:blue
|
|
gptkbp:compression_ratio
|
16.5:1
|
|
gptkbp:controls
|
gptkb:electronic
ECU
|
|
gptkbp:cooling_system
|
water-cooled
liquid cooled
water/glycol mixture
|
|
gptkbp:displacement
|
12.7 L
|
|
gptkbp:emissions_standard
|
gptkb:EPA_Tier_2
natural aspiration
wet exhaust
|
|
gptkbp:engine
|
gptkb:V8
gptkb:theorem
high
aluminum
flexible
linear
cast iron
10,000 hours
electric start
|
|
gptkbp:engine_type
|
gptkb:ISO_3046
four-stroke
full-flow
|
|
gptkbp:first_introduced
|
gptkb:1990
|
|
gptkbp:fuel_capacity
|
200 gallons
0.4 miles per gallon
36 x 30 x 30 in
40 qt
5 gph
|
|
gptkbp:fuel_type
|
diesel
mechanical
direct injection
spin-on
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
V-92 S2 F diesel engine
|
|
gptkbp:ignition_system
|
compression ignition
|
|
gptkbp:launch_site
|
electric
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Detroit_Diesel_Corporation
|
|
gptkbp:market_segment
|
commercial marine
|
|
gptkbp:max_speed
|
2,300 RPM
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:power_output
|
735 hp
|
|
gptkbp:propulsion
|
0.41 hp/lb
|
|
gptkbp:strategic_importance
|
overheating
|
|
gptkbp:stroke
|
5.0 in
|
|
gptkbp:successor
|
V-92 TA
|
|
gptkbp:torque
|
flat
pressure fed
1,950 lb-ft
|
|
gptkbp:used_in
|
gptkb:starship
|
|
gptkbp:user_manual
|
gptkb:theorem
|
|
gptkbp:valve_configuration
|
OHV
|
|
gptkbp:warranty
|
2 years
|
|
gptkbp:weight
|
1,800 lbs
|