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) 0.250 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 87.40 ⚡/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