SBIR/STTR
Advanced Green Micropropulsion System, Phase II
Project Introduction
Systima in collaboration with University of Washington is developing a high performance injection system for advanced green monopropellant AF-M315E micropropulsion systems (0.1 – 1.0 N) for small- and micro-satellites and cubesats (100 kg-500 kg and <100 kg). The monopropellant has low-toxicity making it easy to store, integrate into modular designs and launch without added costs associated with handling toxic propellants such as hydrazine. The injector is a critical component that is designed to enhance combustion and optimize microthruster performance. In the Phase I program, Systima and UW completed proof-of-concept tests that demonstrated the injector technical concept and system advantages. In the Phase II program we will develop a prototype injector design, conduct injector performance testing and workhorse microthruster hot-fire tests with AF-M315E. This effort will result in a monopropellant injection system for modular microthruster system designs that meets the needs of current and future small- and micro-satellites for NASA missions, commercial and military customers.
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Anticipated Benefits
Green monopropellant micropropulsion systems with Systima's high performance injector offer safer handling, reduced system complexity, decreased launch processing times and increased performance compared to conventional hydrazine micropropulsion systems, and are well suited for a wide range of NASA spacecraft missions. Spacecraft micropropulsion systems with Systima's high performance injector can be used for; orbit maintenance, fine attitude control, troubleshooting and maintenance, and potential needs for quick response at relatively high Isp.
Green monopropellants offer significant advantages in performance and reduced handling infrastructure for commercial and military small and micro satellites and payloads, and allow for modular designs for rapid response capabilities. Systima's injector technology is well suited for micropropulsion systems for orbital insertion or transfer, stationkeeping and drag compensation and attitude control. More »
Green monopropellants offer significant advantages in performance and reduced handling infrastructure for commercial and military small and micro satellites and payloads, and allow for modular designs for rapid response capabilities. Systima's injector technology is well suited for micropropulsion systems for orbital insertion or transfer, stationkeeping and drag compensation and attitude control. More »
Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Glenn Research Center
(GRC)
|
Lead Organization | NASA Center | Cleveland, OH |
| Systima Technologies, Inc. | Supporting Organization | Industry | Bothell, WA |
| University of Washington, Dept. Aeronautics & Astronautics | Supporting Organization | Academic | Seattle, WA |
Primary U.S. Work Locations
-
Washington
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Center / Facility:
- Glenn Research Center (GRC)
Responsible Program:
- SBIR/STTR
Project Management
Program Director:
Program Manager:
Project Manager:
Principal Investigator:
- Stephanie Sawhill
Project Duration
Start: Sep 2014
End: Mar 2017
Technology Maturity (TRL)
| Start: | 3 |
| Current: | 4 |
| Estimated End: | 4 |
Applied Research
Development
Demo & Test
Technology Areas
Primary:
- TA 2 In-Space Propulsion Technologies
- TA 2.1 Chemical Propulsion
- TA 2.1.1 Liquid Storable
Other / Cross-cutting:
- TA 2 In-Space Propulsion Technologies
- TA 2.1 Chemical Propulsion
- TA 2.1.7 Micropropulsion
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