5 N HPGP Thruster
Bradford Space
Mid-class HPGP monopropellant thruster delivering 1.4-5.5 N thrust for AOCS and delta-V on small and medium satellites.
Typed specifications6 values
Discloses 4 of 10 fields engineers filter by in this category (category median 3).
- Mass
- 450 g product page
- Thrust
- 1 400–5 500 mN product page
- Specific impulse
- 220–245 s product page
- Propellant
- LMP-103S (ADN) product page
- Power consumption
- 25–30 W product page
- Feed / tank pressure
- 5.5–24 bar 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 supplier8 lines, in the manufacturer's own wording
- Thrust
- 1.4-5.5 N
- Specific impulse
- 220-245 s
- Mass
- 0.45 kg
- Pulse count
- 50,000
- Feed pressure
- 5.5-24 bar
- Heater power
- 25-30 W
- Function
- AOCS + ΔV
- Propellant
- LMP-103S (ADN-based, non-toxic)
About
The 5 N HPGP thruster from ECAPS (a Bradford Space company) is a mid-thrust-class monopropellant engine running on the non-toxic, ADN-based LMP-103S propellant. It provides attitude control and orbital maneuvering capability for small and medium satellite platforms.
Part of ECAPS’ flight-qualified HPGP thruster family spanning 100 mN to 220 N, offering higher performance than hydrazine without the associated toxic-propellant handling requirements.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.