THRUSTERS & SYSTEMS
ENABLING YOUR MISSIONS IN SPACE
M4
MONOPROPELLANT THRUSTER
A110
BIPROPELLANT
THRUSTER
LE144
BIPROPELLANT
THRUSTER
A2200
BIPROPELLANT
ENGINE
THRUST: 144N (32-lbf)
LE144 is a dual mode engine operating on hydrazine in monopropellant mode and MON-3 oxidizer in bipropellant mode to provide class-leading performance in space propulsion
THRUST: 2200N (500-lbf)
A2200 is a high performance M20 and MON-3 engine for high ΔV missions requiring deep throttling capability.
THRUST: 111N (25-lbf)
A110 is a M20 and MON-3 bipropellant, radiatively-cooled thruster for spacecraft attitude control and ΔV maneuvers.
THRUST: 4 N (0.9 lbf)
Hydrazine monopropellant thrusters designed to provide attitude and position control to small spacecraft.
IN DEVELOPMENT
M350
THRUSTER
DS45
THRUSTER
THRUST: 350N
Monopropellant thruster that delivers large-impulse delta-V propulsion capability with the ability to be pulsed for precise velocity or attitude adjustment with a dual-coil valve providing operational redundancy for any mission.
THRUST: 45N
Bipropellant thrusters designed for precision control with the performance suitable for both attitude control and ΔV maneuvers.
M35
THRUSTER
DS22
THRUSTER
THRUST: 35N
Hydrazine monopropellant thrusters designed to provide attitude control and delta-V propulsion to spacecraft requiring low complexity.
THRUST: 22N
Bipropellant thrusters designed to be used for ultra-precise control of spacecraft.
PROPULSION SYSTEMS:
PROPULSION SYSTEM
Refuellable, electrically pumped, monopropellant hydrazine system with an array of redundant 4-N thrusters for orbit adjustment and attitude control that can deliver 149.7 kN-s of total impulse
MOAB
PROPULSION SYSTEM
An attitude and ∆V control propulsion system.
Four (4x) Agile A110 thrusters provide primary propulsion for ∆V maneuvers with thrust vectoring and eight helium-driven Agile TD25 cold-gas thrusters provide attitude control.