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.

A2200 Agile Space Engine

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.

YOSEMITE

TANKS

ZERO SLOSH PISTON TANKS

The Zero Slosh Piston Tanks ensure over 99.75% expulsion efficiency while preventing propellant slosh during maneuvers. Constructed with Aluminum and PTFE seals, they offer durability and minimal diffusion. Their simple, scalable design reduces manufacturing complexity, enabling rapid production in under six months.

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.