Difference between revisions of "J-90 "Goliath" Turbofan Engine/Box"
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− | + | <noinclude>{{Data template used}}</noinclude> | |
+ | {{Infobox/Part | ||
+ | |file=J-90 Goliath Turbofan Engine.png | ||
+ | |since=1.0.5 | ||
+ | |type=je | ||
+ | |part=jetEngines | ||
+ | |costs=2600 | ||
+ | |mass=4.5 | ||
+ | |tolerance=7 | ||
+ | |temp=2000 | ||
+ | |drag=0.2 | ||
+ | |research=Heavy Aerodynamics | ||
+ | |unlock cost=15000 | ||
+ | |manufacturer=C7 | ||
+ | |filename=jetEngineBig.cfg | ||
+ | |part=jetEngines | ||
+ | |more= | ||
+ | {{Infobox/Part/jet engine | ||
+ | |isp=12600 | ||
+ | |thrust=360 | ||
+ | |vectoring= | ||
+ | }} | ||
+ | {{Infobox/Part/air intake | ||
+ | |speed=30 | ||
+ | |area=0.03 | ||
+ | |max=3.4 | ||
+ | }} | ||
+ | }} |
Revision as of 18:31, 17 March 2017
J-90 "Goliath" Turbofan Engine | ||
Jet engine by C7 Aerospace Division | ||
Cost | (total) | 2 600.00 |
Mass | (total) | 4.50 t |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Volume | ? | |
Impact Tolerance | 7 m/s | |
Research | Heavy Aerodynamics | |
Unlock cost | 15 000 | |
Since version | 1.0.5 | |
Part configuration | jetEngineBig.cfg | |
Maximum thrust | 360 kN | |
Isp | (max) | 12600 s |
Fuel consumption | 0.58 /s | |
Intake air consumption | 0.00 /s | |
Thrust vectoring | No | |
Intake speed | 30 | |
Intake area | 0.03 m2 | |
Maximum intake air | 3.4 |