Peregrine Bipropellant Thruster System
Benchmark Space Systems
Green bipropellant propulsion system for 6U to ESPA-class satellites. HTP + Alcohol, >270 s Isp, 100 mN–22 N thrust, ODPS pressurization.
Typed specifications7 values
Discloses 4 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 4 kg product page
- Thrust
- 100 mN product page
- Specific impulse
- 270 s min · product page
- Propellant
- HTP (hydrogen peroxide) product page other HTP (High-Test Peroxide) + Alcohol
- Power consumption
- 5 W product page
- Min impulse bit
- 0.5 mN·s max · product page
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 supplier9 lines, in the manufacturer's own wording
- Propellant
- HTP (High-Test Peroxide) + Alcohol
- Specific impulse
- > 270 s
- Thrust range
- 100 mN – 22 N
- Minimum impulse bit
- < 0.5 mN·s
- Dry mass
- 4.0 kg
- Power (thrust valve)
- < 3 W
- Power (pressurization)
- 5 W
- Available impulse
- 1,750 – 200,000 N·s (configurable)
- Nozzle configurations
- 1–12 nozzles
About
The Peregrine is Benchmark Space Systems’ high-performance green bipropellant propulsion system for small satellites from 6U to ESPA class. Uses HTP (High-Test Peroxide) + Alcohol propellants with patented micromixing technology enabling hypergolic combustion without catalyst beds. ODPS™ on-demand pressurization eliminates pressurized propellant at launch. Available in impulse configurations from 1,750 to 200,000 N·s. 4.0 kg dry mass.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.