Difference between revisions of "R121 Turboshaft Engine/Box"
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|mass=0.6 | |mass=0.6 | ||
|ia=3 | |ia=3 | ||
| + | |motorOutput=150 | ||
| + | |motorCost=2 | ||
| + | |motorMass=0.004 | ||
|drag=0.2 | |drag=0.2 | ||
|temp=2000 | |temp=2000 | ||
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|part=Robotics | |part=Robotics | ||
|more={{Infobox/Part/servo | |more={{Infobox/Part/servo | ||
| − | | | + | |baseRate=0.1 |
| − | | | + | |motorOutput=150 |
|efficiency=0.4 | |efficiency=0.4 | ||
|lf=0.01 | |lf=0.01 | ||
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}} | }} | ||
{{Infobox/Part/cargo | {{Infobox/Part/cargo | ||
| + | |volume=-1 | ||
|stack=1 | |stack=1 | ||
| − | |||
}} | }} | ||
{{Infobox/Part/tank | {{Infobox/Part/tank | ||
| − | |ia=3 | + | |ia=3 |
}} | }} | ||
}} | }} | ||
Latest revision as of 20:36, 21 September 2024
| R121 Turboshaft Engine | ||
 | ||
| Turboshaft engine by C7 Aerospace Division | ||
| Radial size | Tiny | |
| Cost | (total) | 500.00 
|
| (dry) | 200.00
| |
| Mass | (total) | 1.215 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 | 0.4  /s
| |
| Intake air consumption | 18.8  /s
| |
| Intake speed | 75 m/s | |
| Intake area | 0.5 m2 | |
| Electricity generated | 0.4 ⚡/s | |
| Packed volume | None | |
| Intake air | 3
| |
