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Dual Mode Green Monopropellant Propulsion System for Interplanetary Missions
Completed
TRL 3 (started at 1, targeting 3)
Description
Today many spacecraft carry two propulsion options: high thrust required for high acceleration maneuvers such as orbit insertion and rapid response; and low thrust required for station keeping and less critical maneuvers. A new class of non-toxic monopropellants, such as AF-M315E and LMP-103S, perform well in both high and low thrust regimes. Significant investments are maturing both monopropellants into propulsion systems tailored for each option. Of interest is leveraging these new technologies into a common propellant, dual mode propulsion system with integrated system design and performance. In support of this concept, Plasma Processes will design an AF-M315E-based dual mode propulsion system in cooperation with Georgia Tech. The baseline system is an extended 4-unit CubeSat propulsion module with four 100 mN thrusters for roll, pitch, and yaw maneuvers; and one 5N thruster for Delta-V maneuvers. The propulsion module is easily expanded to an 8-unit module, allowing for more propellant and longer missions. Non-toxic monopropellants are positioned to provide increased mission safety, reduced life cycle costs, and increased performance over state-of-the-art alternatives. From a spacecraft perspective, a single propellant, dual mode propulsion system can reduce weight and volume, allowing for more payload and greater propulsion flexibility. From a mission perspective, the technology facilitates the use of less expensive launch vehicles, less stringent launch requirements, and transfer to desired orbit. This concept enables frequent low-cost missions allowing for iteration and opportunities to improve technologies.
Benefits
Interplanetary Deep Space Exploration (AEOLUS, CUVE, CHARIOT), Asteroid Exploration (ROSS, APEX), Lunar Exploration (CUBEX), Earth Science & Observation
Earth Observation (PLANET LABS), Satellite De-Orbit De-commissioning & Escape Orbits, Global Connectivity (OneWeb, STARLINK/SpaceX, Athena/Facebook), Science & Technology Missions (NOAA), Low Cost Launch Providers
Details
| Technology area | Propulsion Systems > Chemical Space Propulsion > Earth Storable Propellants |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | Plasma Processes, LLC, Huntsville, AL |
| Start date | 2019-08-19 |
| End date | 2020-09-18 |
Project contacts
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How to get involved
This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
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