NASA NTRS · 20220009968
Development of ASCENT Propellant Thrusters and Propulsion Systems
Abstract
Since the 1960s, hydrazine technology has dominated the market of propulsion technology by providing reliable performance on a wide variety of spacecraft. Efforts to replace hydrazine with a higher-performance and safer alternative have engaged numerous emerging technologies in the industry to mature. ASCENT propellant, also known as AF-M315E, is an example of one such green propellant. Initially developed to provide a safer handling environment than hydrazine, ASCENT offers higher overall performance than a hydrazine equivalent by creating more heat during ignition. The next generation of propulsion technology, based on ASCENT propellant, produces a higher impulse and energy density, expanding the realm of applicable missions from LEO to GEO and beyond. Building on a strong background in small satellite technology and expertise in thermal and oxidation resistant materials, Plasma Processes began several thruster programs for variety of small satellite applications using ASCENT-based technology. Plasma Processes’ background expertise in thermal and oxidation resistant materials provides the necessary foundation to create ASCENT-based technology hardware.
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Mackenzie Kilcoin, Daniel Cavender, Tomas Hasanof, Michael Zaluki, Tim McKechnie, Corinne Sedano, Hunter Williams. Development of ASCENT Propellant Thrusters and Propulsion Systems. https://ntrs.nasa.gov/citations/20220009968
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