RAIL PLASMA
thruster design engine
T:
0
mN
ISP:
0
s
v
e
:
0
km/s
P:
0
W
η:
0
%
ṁ:
0
mg/s
click tube to place coil · drag to move · scroll = strength · DEL remove
Geometry
Cathode r
5 mm
Anode r
25 mm
Length
80 mm
Nozzle
50%
Operating Point
Current
200 A
Mass flow
10 mg/s
B applied
0.10 T
Gas
Argon
Xenon
Hydrogen
Helium
Lithium
Krypton
40.0 AMU
View
Field
Temperature
Density
Velocity
|B| field
|J| current
Pressure
Overlay
Particles
B field lines
Velocity arrows
None
Presets
SX3 Class
JPL Class
Self-Field
Low Power
Validation vs Published Data
Parameter Sweep
Sweep
Current
Mass flow
B applied
Min
10
Max
90
Run Sweep
Hardware Specification
Thrust Breakdown
—
Simulate
Validate
Optimize
Spec
RAIL PLASMA v2 — SI calibrated