GP-LAM
Manastu Space
GP-LAM is a compact, modular, and safe 300 N green thruster designed for upper stages of Launch Vehicles, Orbital Transfer Vehicles (OTVs), and GEO spacecraft, utilizing non-toxic MS289 propellant.
Typed specifications5 values
Discloses 3 of 10 fields engineers filter by in this category (category median 3).
- Thrust
- 300 000 mN product page 300 000 mN
- Total impulse
- 80 000 N·s product page
- Propellant
- HTP (hydrogen peroxide) product page other non-toxic MS289 green propellant
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 supplier6 lines, in the manufacturer's own wording
- Thruster type
- 300 N thruster
- Propellant
- non-toxic MS289 green propellant
- Features
- Compact, modular and safe
- Thermal management
- Controlled Thermal Stress
- Thrust
- 300 N
- Total impulse
- 80,000 N-s
About
GP-LAM is a 300 N thruster that utilizes non-toxic MS289 green propellant, making it an ideal solution for various space applications. Its compact, modular, and safe design allows for versatile integration into different spacecraft and launch vehicle architectures. The thruster is particularly suited for the upper stages of Launch Vehicles, Orbital Transfer Vehicles (OTVs), and Geostationary Earth Orbit (GEO) spacecraft. Key applications include LEO circularization, GTO-GEO transfer, trajectory correction, and collision avoidance. These capabilities enable a wide range of advanced orbital maneuvers, making GP-LAM an excellent choice for a versatile Auxiliary Propulsion System (APS). The system is designed to manage controlled thermal stress.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.