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.
Mars Ascent Vehicle Hybrid Propulsion Development
Joint Army-Navy-NASA-Air Force (JANNAF) Propulsion Systems Hazards (PSHS) Subcommittee Meeting
;
2019
;
Dayton, OH, United States
Joint Army-Navy-NASA-Air Force (JANNAF) Combustion (CS) Subcommittee Meeting
;
2019
;
Dayton, OH, United States
Joint Army-Navy-NASA-Air Force (JANNAF) Exhaust Plume and Signatures (EPSS) Subcommittee Meeting
;
2019
;
Dayton, OH, United States
Joint Army-Navy-NASA-Air Force (JANNAF) Airbreathing Propulsion (APS) Subcommittee Meeting
;
2019
;
Dayton, OH, United States
Joint Army-Navy-NASA-Air Force (JANNAF) Propulsion (JPM) and Programmatic and Industrial Base (PIB) Subcommittee Meeting
;
2019
;
Dayton, OH, United States
2019-06-01
Miscellaneous
No indication
English
Mars Ascent Vehicle Hybrid Propulsion Development
NTRS | 2019
|Mars Ascent Vehicle Hybrid Propulsion Configuration
NTRS | 2020
|MARS ASCENT VEHICLE HYBRID PROPULSION EFFORT
TIBKAT | 2020
|