Difference between revisions of "R121 Turboshaft Engine/Box"
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|base=0.1 | |base=0.1 | ||
|motor=150 | |motor=150 | ||
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+ | |motorMass=0.004 | ||
|efficiency=0.4 | |efficiency=0.4 | ||
|lf=0.01 | |lf=0.01 |
Revision as of 21:41, 31 August 2024
R121 Turboshaft Engine | ||
Turboshaft engine by C7 Aerospace Division | ||
Radial size | Tiny | |
Cost | (total) | 200.00 |
(dry) | 200.00 | |
Mass | (total) | 0.615 t |
(dry) | 0.615 t | |
Drag | 0.2 | |
Max. Temp. | 2000 K | |
Impact Tolerance | 12 m/s | |
Research | Aerodynamics | |
Unlock cost | 1 200 | |
Since version | 1.7.3 | |
Part configuration | RotorEngine_02.cfg | |
Fuel consumption | 0.0 /s | |
Intake air consumption | 0.0 /s | |
Intake speed | 75 m/s | |
Intake area | 0.5 m2 | |
Electricity generated | 0.4 ⚡/s | |
Packed volume | None | |
Intake air | 3 |