Human exploration beyond LEO relies on a suite of propulsive elements to: (1) Launch elements into space, (2) Transport crew and cargo to and from various destinations, (3) Provide access to the surface of Mars, (4) Launch crew from the surface of Mars. Oxygen/Methane propulsion systems meet the unique requirements of Mars surface access. A common Oxygen/Methane propulsion system is being considered to reduce development costs and support a wide range of primary & alternative applications.
Methane Propulsion Elements for Mars
2017
16 pages
Report
No indication
English
Space Technology , Manned space flight , Mars exploration , Methane , Oxygen , Propulsion , Propulsion system configurations , Propulsion system performance , Cislunar space , Cost reduction , Cryogenic tanks , Landing modules , Launching , Mars (manned reusable spacecraft) , Mars surface , Payloads
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