Schiaparelli EDM lander
Schiaparelli EDM lander [skjapaˈɾɛlːi] was the Entry, Descent and Landing Demonstrator Module (EDM) of the ExoMars programme—a joint mission of the European Space Agency (ESA) and the Russian space agency Roscosmos . [4] It was built in Italy and was intended to test technology for future soft landings on the surface of Mars . [5] It also had a limited but focused science payload that would have measured atmospheric electricity on Mars and local meteorological conditions. [2] [6] [7]
Page Revisions
| Year | Metadata | Sections | Top Words | First Paragraph |
| 2018 |
377674 characters 26 sections 56 paragraphs 46 images 618 internal links 126 external links |
4. Entry, descent, and landing events sequence |
edm 0.413 lander 0.260 schiaparelli 0.258 exomars 0.244 tgo 0.213 landing 0.203 descent 0.203 deca 0.177 module 0.136 parachute 0.131 2016 0.125 entry 0.112 dreams 0.103 static 0.098 esa 0.088 |
Schiaparelli EDM lander [skjapaˈɾɛlːi] was the Entry, Descent and Landing Demonstrator Module (EDM) of the ExoMars programme—a joint mission of the European Space Agency (ESA) and the Russian space agency Roscosmos . [4] It was built in Italy and was intended to test technology for future soft landings on the surface of Mars . [5] It also had a limited but focused science payload that would have measured atmospheric electricity on Mars and local meteorological conditions. [2] [6] [7] |
| 2017 |
344486 characters 26 sections 58 paragraphs 46 images 525 internal links 127 external links |
4. Entry, descent, and landing events sequence |
edm 0.414 lander 0.261 schiaparelli 0.250 exomars 0.244 tgo 0.214 descent 0.203 landing 0.199 deca 0.177 module 0.136 parachute 0.132 2016 0.126 entry 0.112 dreams 0.103 static 0.099 esa 0.088 |
Schiaparelli EDM lander [skjapaˈɾɛlːi] was the Entry, Descent and Landing Demonstrator Module (EDM) of the ExoMars programme—a joint mission of the European Space Agency (ESA) and the Russian space agency Roscosmos . [4] It was built in Italy and was intended to test technology for future soft landings on the surface of Mars . [5] It also had a limited but focused science payload that would have measured atmospheric electricity on Mars and local meteorological conditions. [2] [6] [7] |
| 2016 |
336759 characters 26 sections 57 paragraphs 47 images 520 internal links 122 external links |
4. Entry, descent, and landing events sequence |
edm 0.429 lander 0.261 exomars 0.245 schiaparelli 0.216 tgo 0.214 descent 0.211 landing 0.195 deca 0.178 module 0.144 parachute 0.132 2016 0.131 entry 0.105 dreams 0.103 esa 0.102 static 0.099 |
Schiaparelli EDM lander [skjapaˈɾɛlːi] was the Entry, Descent and Landing Demonstrator Module (EDM) of the ExoMars programme—a joint mission of the European Space Agency (ESA) and the Russian space agency Roscosmos . [4] It was built in Italy and was intended to test technology for future soft landings on the surface of Mars . [5] It also had a limited but focused science payload that would have measured atmospheric electricity on Mars and local meteorological conditions. [2] [6] [7] |
| 2015 |
38496 characters 5 sections 8 paragraphs 6 images 36 internal links 13 external links |
edm 0.417 dreams 0.245 descent 0.242 will 0.231 microares 0.222 payload 0.165 ods 0.164 sensor 0.155 deca 0.148 methumi 0.148 humboldt 0.139 humidity 0.133 dust 0.128 electrification 0.127 landing 0.124 |
Schiaparelli EDM lander , the the Entry, Descent and Landing Demonstrator Module (EDM) of the ExoMars mission, [1] will provide the European Space Agency (ESA) and Russia's Roscosmos with the technology for landing on the surface of Mars with a controlled landing orientation and touchdown velocity; key technologies for the 2018 mission. [2] After entering the Martian atmosphere , the module will deploy two parachutes and will complete its landing by using a closed-loop guidance, navigation and control system based on a Radar Doppler Altimeter sensor and on-board Inertial Measurement Units. The final stages of the landing will be performed using pulse-firing liquid-fuel engines. About a metre above ground, the engines will turn off. The platform will land on a crushable structure, designed to deform and absorb the final touchdown impact. [2] [3] Throughout the descent, the Entry and Descent Science Team will perform investigations using various sensors to record a number of atmospheric parameters. [3] |