HYDROS® Thruster
HYDROS® is a green, water-based hybrid electrical/chemical propulsion thruster from Tethers Unlimited, available in CubeSat (HYDROS-C) and micro-satellite (HYDROS-M) configurations.
Typed specifications23 values
Discloses 8 of 10 fields engineers filter by in this category (category median 3).
- Propulsion family
- hybrid datasheet p.1
- Mass
- 2.2 kg Dry Mass · datasheet p.2 500 g Water Capacity | 2.7 kg Wet Mass
- Thrust
- 1 200 mN min · HYDROS-C and HYDROS-M · datasheet p.2 1 200 mN min
- Envelope (L×W×H)
- 190 x 130 x 92mm datasheet p.2
- Specific impulse
- 310 s min · HYDROS-C and HYDROS-M · datasheet p.2 310 s min
- Total impulse
- 2 151 N·s min · product page 18 000 N·s min
- Propellant
- water datasheet p.1
- Power consumption
- 16 W Nominal MAX · datasheet p.2 5 W MAX W/ Heaters | 3.5 W standby, HYDROS-C and HYDROS-M | 5–25 W | 25 W MAX W/ Heaters +1
- TRL
- 9 datasheet p.2
- Thruster technology
- water electrolysis datasheet p.1
- Min impulse bit
- 1 750 mN·s min · impulse per thrust event, HYDROS-C and HYDROS-M · datasheet p.2
- Flight heritage
- Proven capability on-orbit datasheet p.1
- Missions flown
- 1 Proven capability on-orbit · datasheet p.1
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier12 lines, in the manufacturer's own wording
- Hydros-c specific impulse
- > 310 s
- Hydros-c thrust
- > 1.2 N
- Hydros-c power
- 5-25 W
- Hydros-c total impulse
- > 2,151 Ns
- Hydros-c water tanks
- Customizable
- Hydros-m specific impulse
- > 310 s
- Hydros-m thrust
- > 1.2 N
- Hydros-m power
- 7-40 W
- Hydros-m total impulse
- > 18,000 Ns
- Hydros-m water tanks
- Customizable
- Hydros-m form factor
- Fits inside a 15" separation ring
- Flight heritage
- Flight units delivered; NASA used HYDROS-C on the first Pathfinder Technology Demonstrator mission
About
The HYDROS® Propulsion System is a ‘hybrid’ electrical/chemical propulsion technology that provides safe, high-thrust, high fuel economy propulsion for satellites. It uses water as propellant, making it safe for personnel during satellite integration and posing no significant risks to primary payloads during launch. Once on-orbit, HYDROS uses an electrolysis system designed for zero-G operation to split water into hydrogen and oxygen, which are combusted as a bi-propellant through a rocket nozzle. It provides higher thrust efficiencies while requiring lower input power than electric propulsion technologies, and provides higher specific impulse than monopropellant chemical propulsion. HYDROS is a modular and scalable system, currently available in two flight-qualified configurations, with Tethers Unlimited (TUI) able to customize designs to specific mission needs. HYDROS-M is sized for micro-satellites and is designed to fit inside a 15-inch separation ring. HYDROS-C is sized for CubeSat spacecraft. The size and configuration of the water tank can be tailored to fit the mission requirements of the spacecraft. HYDROS also includes integrated avionics to greatly simplify the commanding interface and integration with the host spacecraft. Flight heritage includes NASA’s use of TUI’s HYDROS®-C unit on the first Pathfinder Technology Demonstrator mission, and flight units of HYDROS-M have been delivered.
Documentation
- hydros-updated-.pdf PDF source: web.archive.org ↗
- TUI-DATA-SHEETS-2-compressed.pdf web.archive.org ↗
Need the full ICD, test reports or a specific revision? Ask the supplier directly.