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

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Revision as of 17:48, 4 April 2016

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) 0.25 t
Drag 0.2
Max. Temp. 2000 K
Volume  ?
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


Thrust vectoring No
Electricity required 3.671 ⚡/s
0.087 ⚡/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