NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Update to Mars Ascent Vehicle Design for Human ExplorationAstronauts on a mission to Mars will require several vehicles working together to get to Mars orbit, descend to the surface of Mars, support them while they’re there, and return them to Earth. The Mars Ascent Vehicle (MAV) transports the crew off the surface of Mars to a waiting Earth return vehicle in Mars orbit and is a particularly influential part of the mission architecture because it sets performance requirements for the lander and in-space transportation vehicles. With this in mind, efforts have been made to minimize the MAV mass, and its impact on the other vehicles. A minimal mass MAV design using methane and in situ generated oxygen propellants was presented in 2015. Since that time, refinements have been made in most subsystems to incorporate findings from ongoing research into key technologies, improved understanding of environments and further analysis of design options. This paper presents an overview of the current MAV reference design used in NASA’s human Mars mission studies, and includes a description of the operations, configuration, subsystem design, and a vehicle mass summary.
Document ID
20190001229
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Polsgrove, Tara P.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Percy, Thomas K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Rucker, Michelle
(NASA Johnson Space Center Houston, TX, United States)
Thomas, Herbert D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
March 4, 2019
Publication Date
March 2, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
MSFC-E-DAA-TN62438
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 2, 2019
End Date: March 9, 2019
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
propulsion
power
spacecraft
No Preview Available