NASA NTRS · 20190027425
Mars Ascent Vehicle Hybrid Propulsion Development
Abstract
Mars Ascent Vehicle Study Agenda: Potential Mars Sample Return (MSR); Potential Hybrid Design; 2019 Preliminary Architecture Assessment; Propellant Combination - Fuel; Propellant Combination - Oxidizer; Full Scale Testing thru 2018; Hypergolic Ignition; TEA/TEB (triethylaluminum/triethylborane) Ignition; Solid Hypergolic Additives; 2018 test - longest duration test; 2019 test; Liquid Injection Thrust Vector Control; White Sands Test Facility; FY19 and Future Work; Summary.
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Story, George, Karp, Ashley, Nakazono, Barry, Whittinghill, George, Zilliac, Greg. 2019-06-01. Mars Ascent Vehicle Hybrid Propulsion Development. https://ntrs.nasa.gov/citations/20190027425
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