The Green Propellant Infusion Mission (GPIM) was a NASA technology demonstrator project that tested a less toxic and higher performance/efficiency chemical propellant for next-generation launch vehicles and CubeSat spacecraft.[4][5][6] When compared to the present high-thrust and high-performance industry standard for orbital maneuvering systems, which for decades, have exclusively been reliant upon toxic hydrazine based propellant formulations, the "greener" hydroxylammonium nitrate (HAN) monopropellant offers many advantages for future satellites, including longer mission durations, additional maneuverability, increased payload space and simplified launch processing.[4][5][7] The GPIM was managed by NASA's Marshall Space Flight Center in Huntsville, Alabama, and was part of NASA's Technology Demonstration Mission Program within the Space Technology Mission Directorate.
The Green Propellant Infusion Mission launched aboard a SpaceXFalcon Heavy rocket on 25 June 2019, on a test mission called Space Test Program 2 (STP-2).[8] The cost of the program was projected to be US$45 million.[9]
The propellant for this mission is hydroxylammonium nitrate (NH3OHNO3) fuel/oxidizer blend, also known as AF-M315E.[6][10] Preliminary data indicates that it offers nearly 50% higher performance for a given propellant tank volume compared to a conventional monopropellant hydrazine system.[4][6][10] The Green Propellant Infusion Mission sought to improve overall propellant efficiency while reducing the toxic handling concerns associated with the highly toxic propellant hydrazine.[5][11] The new propellant is an energetic ionic liquid. Ionic liquids are salt compounds in a liquid form whose molecules have either a positive or negative charge, which bonds them together more tightly and makes the liquid more stable.[12]
Following the success of GPIM, the AF-M315E propellent was renamed ASCENT (Advanced Spacecraft Energetic Non-Toxic) in preparation for commercial use and production.[14]
A Naval Research Laboratory instrument to measure plasma densities and temperatures.
An Air Force Institute of Technology instrument that will test space collision avoidance measures.[15] Over the course of its mission, GPIM uses these instruments to monitor space weather and continuously track its own position and velocity.[1]
Applications
Once proven in flight, the project presents AF-M315E/ASCENT propellant and compatible tanks, valves and thrusters to NASA and the commercial spaceflight industry as "a viable, effective solution for future green propellant-based mission applications".[7][11] According to NASA, the new propellant will be an enabling technology for commercial spaceports operating across the United States "permitting safer, faster and much less costly launch vehicle and spacecraft fuel loading operations."[5] The combined benefits of low toxicity and easy open-container handling shorten ground processing time from weeks to days, simplifying the launching of satellites.[5] The new fuel is 50% denser than hydrazine,[16] meaning more of it can be stored in containers of the same volume. It also has a lower freezing point, requiring less spacecraft power to maintain its temperature.[7]
In addition to its use on lighter satellites and rockets, the fuel's exceptional volumetric storage properties is also being assessed for military uses such as missile launches.[6]
^ abcSpores, Ronald A.; Robert Masse, Scott Kimbrel, Chris McLean (15–17 July 2013), "GPIM AF-M315E Propulsion System"(PDF), 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Jose, California, USA, archived from the original(PDF) on 28 February 2014, retrieved 27 February 2014{{citation}}: CS1 maint: location missing publisher (link) CS1 maint: multiple names: authors list (link)
Spores, Ronald A.; Robert Masse, Scott Kimbrel, Chris McLean (15–17 July 2013), "GPIM AF-M315E Propulsion System", 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit(PDF), San Jose, California, USA, archived from the original(PDF) on 28 February 2014, retrieved 27 February 2014{{citation}}: CS1 maint: location missing publisher (link) CS1 maint: multiple names: authors list (link)
Launches are separated by dots ( • ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ). Crewed flights are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
