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NASA’s Strategic Analysis Cycle 2021 (SAC21) Human Mars Architecture[Note: this is the presentation for a companion paper with the following abstract]
The National Aeronautics and Space Administration’s (NASA) Mars Architecture Team (MAT) was challenged to develop a mission architecture capable of transporting humans to the surface of Mars and back as fast—and as soon—as practical. This challenge represented a significant departure from previous approaches that minimized Earth-launched mass and maximized in-space transportation efficiency, often resulting in roundtrip missions of three years or more in duration. In the interest of crew health, MAT’s cross-Agency team of subject matter experts was challenged to develop an architecture capable of shortening crew time away from Earth to about two years. MAT was given specific mission constraints, such as number of crew, as well as mandates to minimize surface infrastructure as much as possible and to incorporate nuclear transportation options. The resulting MAT-developed concept, referred to here as the Strategic Analysis Cycle 2021 (SAC21) architecture, leverages Artemis elements and emerging commercial capabilities for cargo and logistics launches, and features a hybrid Nuclear Electric Propulsion (NEP)/Chemical transportation system able to complete the 1.8 billion kilometer round-trip journey to Mars and back in 760 to 850 days transit time for the 2039 Earth departure opportunity. Three Mars Descent Systems (MDS), each capable of landing about 25 metric tons of useful cargo on the surface of Mars, would be pre-deployed in advance of crew departure from Earth; two of these MDS’s would deliver a partially fueled Mars Ascent Vehicle (MAV), a fission power system, surface mobility, and additional MAV propellant. To minimize surface infrastructure, only two of the four Mars crew would descend and live in an MDS-landed pressurized rover, exploring the martian surface for 30 martian days, or sols, before returning to Mars orbit aboard their MAV and rejoining the other two crew on the Deep Space Transport for the Earth return voyage. Specifics of many of these architecture elements are detailed in separate technical publications; this paper outlines the end-to-end integrated architecture performance and concept of operations, including synergies with Artemis lunar architecture elements. It is important to note that NASA does not have a formal human Mars program and no decisions have been made; the architecture described here is intended to fill in an often-overlooked corner of the trade space, helping to complete the menu of options available to decision-makers as they chart the course for humans to Mars.

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Document ID
20220002632
Acquisition Source
Johnson Space Center
Document Type
Presentation
Authors
Michelle Rucker
(Johnson Space Center Houston, Texas, United States)
Douglas A Craig
(National Aeronautics and Space Administration Washington D.C., District of Columbia, United States)
Laura M Burke
(Glenn Research Center Cleveland, Ohio, United States)
Patrick R Chai
(Langley Research Center Hampton, Virginia, United States)
Michael B Chappell
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Bret G Drake
(The Aerospace Corporation El Segundo, California, United States)
Stephen J Edwards
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Stephen Hoffman
(The Aerospace Corporation El Segundo, California, United States)
Andrew C McCrea
(Langley Research Center Hampton, Virginia, United States)
Douglas J Trent
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Patrick A Troutman
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
February 16, 2022
Subject Category
Lunar And Planetary Science And Exploration
Launch Vehicles And Launch Operations
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: US
Start Date: March 6, 2022
End Date: March 12, 2022
Sponsors: Institute of Electrical and Electronics Engineers
Funding Number(s)
WBS: 452582.81.72
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Long-duration spaceflight
Mars
Entry
Descent
Landing
Ascent
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