Mars Ascent Vehicle Hybrid Propulsion Development

Story, George ; Karp, Ashley ; Nakazono, Barry ; Whittinghill, George ; Zilliac, Greg

关键词: MARS EXPLORATION;    ASCENT PROPULSION SYSTEMS;    MARS SAMPLE RETURN MISSIONS;    HYBRID PROPULSION;    HYPERGOLIC ROCKET PROPELLANTS;    PROPELLANT ADDITIVES;    OXIDIZERS;    LIQUID INJECTION;    THRUST VECTOR CONTROL;    MOON TO MARS PROGRAM;   

RP-ID  :  M19-7403

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

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.