SATELLITE PROPULSION SYSTEM
(MODULAR ARCHITECTURE PROPULSION SYSTEM)
NOW TRL-9 QUALIFIED!
Providing station keeping, constellation management and deorbiting to the small satellite market, MAPS is a highly configurable, compact satellite propulsion system, complete with high-performance capabilities. MAPS has been demonstrated and proven on a 3u CubeSat and is compatible with many satellites, such as a 6u CubeSat and larger.
MAPS is an array of high performance, hermetically-sealed, solid propellant rocket motors, all of which extend the orbital life of CubeSats and SmallSats while providing propulsion capability for small upper stages. Our MAPS satellite propulsion system can be used for orbital maneuvers and deorbit with very precise and predictable delivered impulse. The module has no tanks, valves, tubing or heaters, making it a “plug and play” bolt-on design. MAPS is instant on with a 10+ year life, uses very low power, has three independent inhibits against firing, and provides variable thrust by firing in pairs, triples, quads, etc. MAPS is adaptable and scalable and fits in unused separation system or other spacecraft real-estate.
Our MAPS CubeSat thrusters are customized for CubeSat propulsion systems configurations at least 3u CubeSat or larger. Interested in our Powered Modular Architecture Propulsion System (P-MAPS™)? P-MAPS provides a fully powered module to assist with decommission and/or deorbit of a satellite, enabling compliance with the 25-year lifetime restrictions in orbit. Did you know, we made it into NASA’s iTech TOP 10 Semifinalists for Cycle 2 innovations?
The MAPS system is a clean burning solid propellant-based array of rocket motors and thrusters. Our small satellite propulsion systems require no large propellant tank or associated hardware nor a high electric current draw. Configurations for any cubesat propulsion module are available. Configurable for 3u cubesats, 6u cubesats and larger satellites.
No warm up time
System is operational anytime in 300 Milliseconds
Always very precise, predictable, repeatable
Distributed impulse bits (delta-V increments) reduces angular rate build up over fixed nozzle systems and improves delta-V predictability
High Isp performance
Duty cycle independent: from pulse mode to steady state, delivered mission Isp is constant
Hermetically sealed motors
Ready to fire immediately at satellite deployment or 10+ years later for deorbit/decommissioning
Safe, very clean burning propellant
Will not contaminate optics or solar panels
Results in very high reliability
Very low power
No heaters or valves
“Bolt-on/plug and play” system
Leaves plenty of extra payload volume
Plug and play size and shape
Customizable to fit the mission
Greatly reduces satellite factory cost
No integration of tanks, valves, fittings, or thrusters during satellite assembly
No fueling operations
Saves at least one week during launch vehicle integration with no propellant waste/disposal
Built-in-test (BIT) available
Anytime during mission operations from integration, launch, deployment and while on-orbit
Well known. Flight proven.
Solid propellant technology with three independent inhibit firing system, simplifies transportation and range safety approvals
Fire motors in pairs, triplets, quads, etc. for variable mission acceleration and delta-V flexibility
When it comes to choosing a satellite propulsion system and SW(M)AP
MAPS EXCELS on all levels
Space: Fits into unused lightband volume
Weight (mass): Better than liquids – no valves, fittings, filters, large thrusters
Power: VERY low power: no heaters, solenoid valves, etc.
POSSIBLE MAPS CONFIGURATIONS
(many options available)
LET US HELP
Need more information or have a specific requirement you would like us to meet?
Contact us at the link below, or for immediate assistance call 888.995.5659.