Powered Modular Architecture Propulsion System
U.S. Government Orbital Debris Mitigation Standard Practices (USGODMSP) and other agencies call for satellites to either deorbit within 25 years of mission completion or maneuver to a storage orbit. Most SmallSats do not contain propulsion to comply with these standard practices or maneuver to improved orbits after separation from the launch vehicle. Satellite owners now have an option for onboard propulsion AND deorbit.
Powered Modular Architecture Propulsion System (P-MAPS™) provides a fully powered module to assist with decommission and/or deorbit of a satellite. P-MAPS enables SmallSats and CubeSats to comply with 25-year lifetime restrictions in orbit.
P-MAPS includes a self-contained power supply, ADCS and UHF receiver, providing reliable power to deorbit in the event of satellite power loss. With all the same performance features as MAPS™ (precise and repeatable impulse bits initiated with hermetically sealed, clean burning, solid propellant with no propellant tanks, valves, fittings, heaters or thrusters) and without any compromise to the satellite design by fitting into unused satellite volume. With our standby power unit, should satellite power supply malfunction, P-MAPS will continue to perform planned decommission and deorbit objectives.
P-MAPS: a fully powered module, UHF receiver and Attitude Determination and Control System (ADCS)