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Exomars mission analysis and design - launch, cruise and arrival analyses
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Cacciatore, Francesco Cano, Juan L. |
| Copyright Year | 2007 |
| Description | ExoMars is ESA s next mission to planet Mars. The probe is aimed for launch either in 2013 or in 2016. The project is currently undergoing Phase B1 studies under ESA management and Thales Alenia Space Italia project leadership. In that context, DEIMOS Space is responsible for the Mission Analysis and Design for the interplanetary and the entry, descent and landing (EDL) activities. The present mission baseline is based on an Ariane 5 or Proton M launch in 2013 of a spacecraft Composite bearing a Carrier Module (CM) and a Descent Module (DM). A back-up option is proposed in 2016. This paper presents the current status of the interplanetary mission design from launch up to the start of the EDL phase. |
| File Size | 263954 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080012678 |
| Archival Resource Key | ark:/13960/t9n34tm6m |
| Language | English |
| Publisher Date | 2007-09-24 |
| Access Restriction | Open |
| Subject Keyword | Spacecraft Design, Testing And Performance Deimos European Space Agency Ariane 5 Launch Vehicle Mars Planet Mission Planning Launching Design Analysis Mars Missions Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
