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The effect of mars surface and phobos propellant production on earth launch mass
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stump, William R. Babb, Gus R. |
| Copyright Year | 1986 |
| Description | Fuel and oxidizer produced on the surface of Mars and on the Martian Moon Phobos can reduce the cumulative mass of fuel and oxidizer which must be launched to low Earth orbit for Mars exploration missions. ||||||||A scenario in which ten conjunction class trajectory missions over a twenty year period land a surface base and propellant production facilities on the Martian surface and on Phobos was examined. Production of oxygen on Phobos provides the greatest benefit. If all the propellant for Mars operations and Earth return is produced at Phobos and on Mars, a 30% reduction in cumulative low Earth orbit mass can be achieved at the end of the 20 year period. |
| File Size | 461930 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870008302 |
| Archival Resource Key | ark:/13960/t0fv3fs65 |
| Language | English |
| Publisher Date | 1986-05-01 |
| Access Restriction | Open |
| Subject Keyword | Astronautics (general) Oxygen Orbit Calculation Fuel Consumption Mars Exploration Fuel Production Low Earth Orbits Orbital Launching Space Commercialization Mission Planning Mars Surface Space Exploration Orbital Maneuvers Mars Landing Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
