DESIGNED FOR THE FUTURE, PROPELLING HUMANITY
M4
THRUST: 4 N (0.9 lbf)
Hydrazine monopropellant thrusters designed to provide attitude and position control to small spacecraft.
DS110
THRUST: 110N (25-lbf)
A MMH/MON3 bipropellant, radiatively-cooled thruster for spacecraft attitude control and ΔV maneuvers.
HP250
THRUST: 250N (56-lbf)
A bipropellant thruster using N2H4/MON3, designed to be used as axial thrusters for midsize to large size spacecraft.
VoidRunner
THRUST: 3000N (600-lbf)
VoidRunner (aka DS3000) was designed to be the main thrust engine on spacecraft like lunar landers or other large vehicles.
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.
TANKS
ZERO SLOSH PISTON TANKS
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