Abstract
As part of the 2023 strategic analysis cycle to explore the trade space, the NASA Mars Architecture Team wanted to explore what it takes to produce in situ on Mars many hundreds of tons of propellants for a large all-chemical transportation system. The conceptual operations and design of the LO2/LCH4 in situ resource utilization (ISRU) water acquisition, propellant production and liquification system was assigned to the NASA Compass concurrent engineering team with support from various NASA ISRU, cryogenic fluid management, and surface power experts. The conceptual point design examined one case producing 300 t of LO2/LCH4 from the Mars atmosphere and delivered water in 20 months and storing the liquified propellants in a to-be-reused lander. Several of these large single-stage, all-chemical class large vertical landers would deliver the required ISRU equipment. The required 150 t of water stock for the ISRU system was traded between three options: delivered, pumped from subsurface ice deposits or extracted from surface soils. The large propellant production systems consist of atmospheric CO2 collection scroll pumps, a combined solid oxide electrolysis and methanation system to convert the CO2 and water into gaseous O2 and CH4, and various dryers, scrubbers, and separators to remove the excess water, CO2 and H2. The liquefaction system consisted of 90 K cryocoolers to provide cold Ne to the launch vehicle tanks to liquify these CH4 and O2 gases and store them as rocket propellants. The systems are deployed using a 6 t (payload) capable chassis derived from conceptual pressurized rover designs. In total, the propellant production and liquefaction systems required three propellant production pallets, two liquefaction pallets, two water tankers, and six 40 kW-fission surface power systems (FSPS) with cabling. All this equipment was found to notionally fit inside two- 75 metric ton payload capacity Mars ascent and landing vehicles (MALV). For the case where 150 t of water delivered from Earth, four cargo MALVs are required for the full system. The same is true when the 150 t of water is extracted through surface mining. For the borehole system, only 3 cargo MALVs are necessary. A comparison of approaches in terms of number of landers, number and type of elements, power and time is made.
Recommended Citation
S. R. Oleson and E. Turnbull and J. Kleinhenz and W. Johnson and R. Grotenrath and N. Uguccini and B. Abshire and L. Mason and T. Packard and A. Colozza and J. Z. Gyekenyesi and J. Fittje and S. Hoffman and L. S. Gertsch, "Kiloton Class Isru Systems for Lo2/lch4 Propellant Production on the Mars Surface," AIAA SciTech Forum and Exposition, 2024, American Institute of Aeronautics and Astronautics, Jan 2024.
The definitive version is available at https://doi.org/10.2514/6.2024-2536
Department(s)
Geosciences and Geological and Petroleum Engineering
Publication Status
Full Access
International Standard Book Number (ISBN)
978-162410711-5
Document Type
Article - Conference proceedings
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 2024 American Institute of Aeronautics and Astronautics, All rights reserved.
Publication Date
01 Jan 2024
