Difference between revisions of "IX-6315 "Dawn" Electric Propulsion System/Box"
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| − | |thrust=2 | + | |thrust=2 |
| − | |isp-atm=100 | + | |isp-atm=100 |
| − | |isp-vac=4200 | + | |isp-vac=4200 |
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{{Infobox/Part/test subject | {{Infobox/Part/test subject | ||
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| − | |staging= | + | |event=y |
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Latest revision as of 20:24, 9 October 2024
| IX-6315 "Dawn" Electric Propulsion System | ||
 | ||
| Ion engine by Ionic Symphonic Protonic Electronics | ||
| Radial size | Tiny | |
| Cost | (total) | 8 000.00 
|
| Mass | (total) | 0.250 t |
| Drag | 0.2 | |
| Max. Temp. | 2000 K | |
| Impact Tolerance | 7 m/s | |
| Research |  Ion Propulsion
| |
| Unlock cost | 16 800
| |
| Since version | 0.18 | |
| Part configuration | ionEngine.cfg | |
| Maximum thrust | (1 atm) | 0.05 kN |
| (vacuum) | 2.00 kN | |
| Isp | (1 atm) | 100 s |
| (vacuum) | 4200 s | |
| Fuel consumption | 0.486  /s
| |
| Electricity required | 8.74 ⚡/s | |
| Testing Environments | ||
| On the surface | No | |
| In the ocean | No | |
| On the launchpad | No | |
| In the atmosphere | No | |
| Sub-orbital | Yes | |
| In an orbit | Yes | |
| On an escape | Yes | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
| Packed volume | 160 l | |
