VASIMR

Type: Space Thruster
Country of Origin: United States
Manufacturer: Ad Astra Rocket Company

First Flight:
Status: In development
Propellant (O/F): Argon
Mixture Ratio (O/F by mass):
Cycle:
Chambers: 1

Thrust (vac.): 5 N (200 kW)
Thrust (s.l.):
Throttle: none
ISP (vac.): 5000 s
ISP (s.l.):
Chamber Pressure:
Nozzle Ratio:
Burn time:
Ignitions:

Mass:
Length:
Diameter:

Used in:

Links: