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T3-ST "Default" Example Methalox Engine |
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Mass | 0.500 t |
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Size | SM |
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Max Temp | 1000 K |
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Impact Tolerance | 10 m/s |
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Monopropellant | 100 t |
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Electric Charge | 200 U |
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Stores Research | ✔ |
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Oxidizer Methane
| 0.040 t/s 0.010 t/s
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Thrust: 1 atm. | 42.0 kN |
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Thrust: Vac. | 88.0 kN |
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Isp: 1 atm. | 223 s |
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Isp: Vac. | 628 s |
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Oxidizer Methane
| 0.040 t/s 0.010 t/s
|
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Thrust: 1 atm. | 42.0 kN |
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Thrust: Vac. | 88.0 kN |
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Isp: 1 atm. | 223 s |
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Isp: Vac. | 628 s |
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Output | 20.250 U/s |
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Always Active | ✔ |
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Engine Alternator | ✔ |
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Output Decays | 21 y 360 d 04 h 20 m 10 s |
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Hydrogen (t) Methane (t)
| 1 1
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Solid Fuel (t)
| 2
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Semi-deployed drag | 400.0 kN |
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Deployed drag | 850.0 kN |
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Experiment | Crew Observation |
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Reports Create | Samples ✔ Data ✗ |
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Report Size | 5 KiB |
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Requirements | All situations and locations |
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Crew Required | 1 |
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Community Conglomerate |
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