RT Journal Article
T1 The MetNet vehicle: a lander to deploy environmental stations for local and global investigations of Mars
A1 Vázquez, Luis
A1 Valero Rodríguez, Francisco
A1 Romero Pérez, Mª Pilar
AB Investigations of global and related local phenomena on Mars such as atmospheric circulation patterns, boundary layer phenomena, water, dust and climatological cycles and investigations of the planetary interior would benefit from simultaneous, distributed in situ measurements. Practically, such an observation network would require low-mass landers, with a high packing density, so a large number of landers could be delivered to Mars with the minimum number of launchers. The Mars Network Lander (MetNet Lander; MNL), a small semi-hard lander/penetrator design with a payload mass fraction of approximately 17 %, has been developed, tested and prototyped. The MNL features an innovative Entry, Descent and Landing System (EDLS) that is based on inflatable structures. The EDLS is capable of decelerating the lander from interplanetary transfer trajectories down to a surface impact speed of 50-70 ms(-1) with a deceleration of < 500 g for < 20 ms. The total mass of the prototype design is approximate to 24 kg, with approximate to 4 kg of mass available for the payload. The EDLS is designed to orient the penetrator for a vertical impact. As the payload bay will be embedded in the surface materials, the bay's temperature excursions will be much less than if it were fully exposed on the Martian surface, allowing a reduction in the amount of thermal insulation and savings on mass. The MNL is well suited for delivering meteorological and atmospheric instruments to the Martian surface. The payload concept also enables the use of other environmental instruments. The small size and low mass of a MNL makes it ideally suited for piggy-backing on larger spacecraft. MNLs are designed primarily for use as surface networks but could also be used as pathfinders for high-value landed missions.
PB Copernicus Gesellschaft MBH
SN 2193-0856
YR 2017
FD 2017-02-24
LK https://hdl.handle.net/20.500.14352/17746
UL https://hdl.handle.net/20.500.14352/17746
LA eng
NO © Author(s) 2017. This work is distributed under the Creative Commons Attribution 3.0 License. Artículo firmado por 32 autores. The authors would like to express their gratitude to the MetNet development teams at the Finnish Meteorological Institute (Finland), Lavochkin Association (Russia), the Russian Space Research Institute (IKI, Russia) and the Instituto Nacional de Técnica Aeroespacial (INTA, Spain) for their great work in the implementation of the MetNet landing vehicle. Ari-Matti Harri and Hannu Savijarvi are thankful for the Finnish Academy grants no. 132825 and no. 131723.
NO Finnish Academy grants
DS Docta Complutense
RD 30 abr 2024