211 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
Pressure-fed liquid rocket engine using nitric-acid/N2O4 oxidizer, developed by VENG.
Clustered (x3) first-stage liquid rocket engine (LOX/RP-1, gas-generator cycle) in development for the Tronador II launch vehicle.
Pressure-fed second-stage rocket engine (MMH/NTO) developed by VENG for the Tronador II launch vehicle.
First-stage liquid rocket engine (LOX/RP-1) developed by VENG for the Tronador II launch vehicle programme.
Air-breathing electric propulsion system that harvests residual upper-atmosphere gas in Very Low Earth Orbit and converts it into…
Compact, scalable electrospray electric propulsion module for CubeSats and small satellites.
A high-power ionic liquid electrospray thruster using EMI-Im propellant with an estimated 289uN thrust in a 94x94x42mm form…
A low-profile CubeSat ionic liquid electrospray thruster using EMI-Im propellant with an estimated 50uN thrust in an ultra-thin…
A PocketQube-class ionic liquid electrospray thruster using EMI-Im propellant with an estimated 50uN thrust in a compact 44x44x36mm…
A CubeSat-class ionic liquid electrospray thruster using EMI-Im propellant with an estimated 50uN thrust in a 65x65x37mm form…
A PocketQube-class ionic liquid electrospray thruster using EMI-Im propellant with an estimated 25uN thrust in a 42x42x35mm form…
A PocketQube-class ionic liquid electrospray thruster using EMI-Im propellant, providing approximately 1uN of thrust in an ultra-compact 44x40x16mm…
A next-generation quad-nozzle sublimation warm gas thruster using solid unpressurized Adamantane, providing an estimated 588uN thrust in a…
The first DIY educational kit for ionic liquid electrospray propulsion, using EMI-Im propellant and providing approximately 1uN of…
A next-generation single-nozzle sublimation warm gas thruster using solid unpressurized Adamantane, providing an estimated 147uN thrust in a…
A quad-nozzle sublimation warm gas thruster using solid unpressurized Adamantane propellant, providing 480uN thrust from a 20W system…
A PocketQube-class sublimation warm gas thruster using solid unpressurized Adamantane propellant, providing 120uN thrust for up to 7…
A dual-nozzle sublimation warm gas thruster using solid unpressurized Adamantane propellant, providing 240uN thrust from a 10W system…
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