PEPT-590GB Diaphragm Propellant Tank
Rafael Advanced Defense Systems - Space DivisionThe PEPT-590GB is Rafael’s highest-capacity propellant tank, providing 204 liters nominal volume and 154 kg propellant capacity in…
14 flight-proven satellite platforms, components and ground equipment from verified manufacturers worldwide.
The PEPT-590GB is Rafael’s highest-capacity propellant tank, providing 204 liters nominal volume and 154 kg propellant capacity in…
The PEPT-590 is a large-volume spherical titanium propellant tank with 102.5 liters nominal net volume and 75 kg…
The PEPT-420N is a large-volume spherical titanium propellant tank with 37.5 liters nominal volume and 30 kg maximum…
The PEPT-260 is a spherical titanium propellant tank with 9.3 liters nominal volume for hydrazine monopropellant propulsion systems.…
The PEPT-230 (Positive Expulsion Propellant Tank) is a spherical titanium propellant tank with 6 liters nominal volume designed…
The R-800 EPS is Rafael’s second-generation Electric Propulsion System following the flight-proven R-400 EPS (Venµs satellite). It operates…
The R-200 EPS (Electric Propulsion System) is a complete, turnkey electric propulsion solution built around Rafael’s qualified R-200…
The R-800 is a Hall Effect Thruster designed for the 450–900W discharge power range, suitable for low to…
The R-200 is a low-power Hall Effect Thruster designed to operate in the 100–300W discharge power range, suitable…
The IHET-300 (Israeli Hall Effect Thruster) is the flight-proven core of Rafael’s first-generation Electric Propulsion System. It operates…
The Rafael 200N Monopropellant Hydrazine Thruster is a high-thrust space propulsion unit designed for integration into Roll Attitude…
The Rafael 25N Monopropellant Hydrazine Thruster is designed for high-thrust satellite maneuvers, providing 9.5 to 28 N of…
The Rafael 5N Monopropellant Hydrazine Thruster is designed for satellite attitude control and orbit correction maneuvers. It produces…
The Rafael 1N Monopropellant Hydrazine Thruster generates the required thrust for maneuvering satellites by means of a hot…
We use cookies. Strictly necessary cookies keep the platform working. With your consent we also use Google Analytics to understand how the platform is used and improve it. We do not use advertising cookies. Cookie Policy · Privacy
Favorites are available to clients only. Sign in to your client cabinet or create a free account — it takes less than a minute.
How is your experience with the platform? Your message goes straight to our team.
Thank you! Your feedback has been sent to our team.