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

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Revision as of 23:03, 17 August 2018

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 367.098 ⚡/s
8.740 ⚡/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