Difference between revisions of "IX-6315 "Dawn" Electric Propulsion System/Box"

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|file=PB-ION.png
 
|file=PB-ION.png
 
|type=ie
 
|type=ie
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|size=0
 
|manufacturer=ISPE
 
|manufacturer=ISPE
|costs=5700
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|costs=8000
 
|mass=0.25
 
|mass=0.25
 
|drag=0.2
 
|drag=0.2
|temp=3600
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|temp=2000
 
|tolerance=7
 
|tolerance=7
 
|research=Ion Propulsion
 
|research=Ion Propulsion
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|filename=ionEngine.cfg
 
|filename=ionEngine.cfg
 
|part=ionEngine
 
|part=ionEngine
|more=
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|parent=Engine
{{Infobox/Part/ion engine
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|more={{Infobox/Part/ion engine
|thrust=2
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|thrust=2
|isp-atm=4200
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|isp-atm=100
|vectoring=
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|isp-vac=4200
|ele-req=0.18000000000000002
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|ele-req=1.8
 
}}
 
}}
 
{{Infobox/Part/test subject
 
{{Infobox/Part/test subject
|environments=15
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|environments=112
|staging=True
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|event=y
|event=True
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|staging=y
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}}
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{{Infobox/Part/cargo
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|volume=160
 
}}
 
}}
 
}}
 
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Latest revision as of 20:24, 9 October 2024

This is a data template. To add content which doesn't belong to this template edit the English page (or one of its translations).
IX-6315 "Dawn" Electric Propulsion System
Part image
Ion engine by
Ionic Symphonic Protonic Electronics

Radial size Tiny
Cost (total) 8 000.00 Funds
Mass (total) 0.250 t
Drag 0.2
Max. Temp. 2000 K
Impact Tolerance 7 m/s
Research Ion propulsion.png Ion Propulsion
Unlock cost 16 800 Funds
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 Xenon unit/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