NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Mars Ascent Vehicle Hybrid Propulsion DevelopmentMars 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.
Document ID
20190027425
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Story, George (NASA Marshall Space Flight Center Huntsville, AL, United States)
Karp, Ashley (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Nakazono, Barry (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Whittinghill, George (Whittinghill Aerospace Camarillo, CA, United States)
Zilliac, Greg (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
July 17, 2019
Publication Date
June 1, 2019
Subject Category
Spacecraft Propulsion And Power
Propellants And Fuels
Report/Patent Number
M19-7403
Meeting Information
Meeting: Joint Army-Navy-NASA-Air Force (JANNAF) Propulsion Systems Hazards (PSHS) Subcommittee Meeting
Location: Dayton, OH
Country: United States
Start Date: June 3, 2019
End Date: June 7, 2019
Sponsors: Department of the Army, Department of the Navy, NASA Headquarters, Department of the Air Force
Distribution Limits
Public
Copyright
Public Use Permitted.

Related Records

IDRelationTitle20190027423See AlsoMars Ascent Vehicle Hybrid Propulsion Development
No Preview Available