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Deploytech: mars sample return concept study delta results
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Russell, Tiffany |
| Copyright Year | 2012 |
| Description | Agenda for this presentation is Exhaust options to reduce the launch numbers from 3 to 2: (1) Mass Reduction of Max-C Rover, ACO Orbiter, and or ACO ERS (2) Eliminate Max-C Rover (3) Launch vehicle options (4) Solar Sail for all interplanetary propulsion, chemical for maneuvering Goal would be to: (1) Brainstorm any other alternatives we have not considered (2) Eliminate any of the options listed above (3) Go forward with a possible viable option that is identified. |
| File Size | 905440 |
| Page Count | 19 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20120016901 |
| Archival Resource Key | ark:/13960/t2f81bt4b |
| Language | English |
| Publisher Date | 2012-09-28 |
| Access Restriction | Open |
| Subject Keyword | Lunar And Planetary Science And Exploration Solar Sails Earth-mars Trajectories Cost Reduction Weight Reduction Interplanetary Spacecraft Mars Sample Return Missions Mission Planning Alternatives Spacecraft Design Mars Exploration Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Presentation |
