5 N HPGP Thruster
bradford-space-ecaps
Mid-class HPGP monopropellant thruster delivering 1.4-5.5 N thrust for AOCS and delta-V on small and medium satellites.
Technical specifications
- 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.
