Difference between revisions of "IX-6315 "Dawn" Electric Propulsion System/Box"
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|mass=0.25 | |mass=0.25 | ||
|drag=0.2 | |drag=0.2 | ||
| − | |temp= | + | |temp=2000 |
|tolerance=7 | |tolerance=7 | ||
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{{Infobox/Part/ion engine | {{Infobox/Part/ion engine | ||
| − | |thrust= | + | |thrust=0.048 |
| − | |isp-atm=4200 | + | |isp-atm=100 |
| + | |isp-vac=4200 | ||
|vectoring= | |vectoring= | ||
|ele-req=0.18000000000000002 | |ele-req=0.18000000000000002 | ||
Revision as of 16:47, 29 April 2015
| IX-6315 "Dawn" Electric Propulsion System | ||
 | ||
| Ion engine by Ionic Symphonic Protonic Electronics | ||
| 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) | 0.00 kN |
| (vacuum) | 0.05 kN | |
| Isp | (1 atm) | 100 s |
| (vacuum) | 4200 s | |
| Fuel consumption | 0.012  /s
| |
| Electricity required | 0.02 ⚡/s | |
| Testing Environments | ||
| On the surface | Yes | |
| In the ocean | Yes | |
| On the launchpad | Yes | |
| In the atmosphere | Yes | |
| Sub-orbital | No | |
| In an orbit | No | |
| On an escape | No | |
| Docked | No | |
| Test by staging | Yes | |
| Manually testable | Yes | |
