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Propulsion System Architecture Refueling Capability Assessment for A Mars Transit Habitat ConceptA pressure-fed hypergolic bi-propellant system is the assumed propulsion approach for the
Reaction Control System (RCS) used by the Mars Transit Habitat (TH), an architectural concept being
traded within the NASA Moon to Mars architecture. The propellants under consideration are Monomethyl Hydrazine (MMH) and Mixed Oxides of Nitrogen with 3% Nitric Oxide (MON3), with helium pressurant.
Document ID
20240003278
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Huu P. Trinh (Marshall Space Flight Center Redstone Arsenal, United States)
Christopher G. Popp (Marshall Space Flight Center Redstone Arsenal, United States)
Brad M. Addona (Marshall Space Flight Center Redstone Arsenal, United States)
Charles W. Pierce (Jacobs Space Exploration Group)
Date Acquired
March 18, 2024
Publication Date
April 2, 2024
Publication Information
Publication: JANNAF
Subject Category
Spacecraft Propulsion and Power
Meeting Information
Meeting: May 2024 JANNAF Meeting
Location: Oklahoma City, OK
Country: US
Start Date: May 6, 2024
End Date: May 9, 2024
Sponsors: United States Department of the Army, United States Department of the Air Force, United States Department of the Navy, National Aeronautics and Space Administration, Joint Army-Navy-NASA-Air Force (JANNAF)
Funding Number(s)
CONTRACT_GRANT: 80MSFC18C0011
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Propulsion Architecture
Mars Transit Habitat
Refueling Capability
Pressure-fed propulsion
pressure-regulated propulsion system
bi-prop system concept
hypergolic propellant system

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