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

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{{Infobox/Part/Engine/Ion
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<noinclude>{{Data template used}}</noinclude>{{Infobox/Part
|file=Pb-ion electric propulsion system.jpg
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|file=PB-ION.png
|costs=5700
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|type=ie
 +
|size=0
 +
|manufacturer=ISPE
 +
|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
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|unlock cost=16800
 
|since=0.18
 
|since=0.18
|manufacturer=Ionic Protonic Electronics
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|filename=ionEngine.cfg
|thrust=0.5
 
|isp-atm=4200
 
|ele-req=120
 
 
|part=ionEngine
 
|part=ionEngine
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|parent=Engine
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|more={{Infobox/Part/ion engine
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|thrust=2
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|isp-atm=100
 +
|isp-vac=4200
 +
|ele-req=1.8
 +
}}
 +
{{Infobox/Part/test subject
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|environments=112
 +
|event=y
 +
|staging=y
 +
}}
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{{Infobox/Part/cargo
 +
|volume=160
 +
}}
 
}}
 
}}

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