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The objective of the study was twofold: i) to analyse the new dynamics of desertification in Southern African region (southern Mozambique, southern Zimbabwe and Northern South Africa) through main achievements of the DesertWatch-Extension; ii) to propose new methods for integration of EO data with different spatial and spectral resolutions, namely the new ESA Proba-V mission, and new field data, in particular, the map of risks on natural disasters in Mozambique.
Instituto Superior...
Motivation:
To investigate the combination of thermal and photovoltaic effects towards an high efficient photo-to-energy conversion device.
Methodology:
We used numerical simulations based on FEM technique. In particular, we addressed the charge cloud issue in a fully 3D fashion to be able to design and simulate devices as close as possible to reality.
After initial tests based on analytical and 1D numerical techniques, we moved to the 3D device where we investigated the role of cathode-anode
Istituto Fondazione...
The project summarized here was conceived to support the definition of applications, products and user requirements, as well as the hardware design and ground processing design of a companion satellite mission which will carry aboard a "passive" radar working in tandem with the Argentinian L-band radar developed by CONAE and denoted as SAOCOM. The primary objective (i.e., science driver) of the SAOCOM companion satellite mission (SAOCOM-CS) is forest tomography, which will be carried out by exploiting small baselines between active and passive systems (order of km) changing with time.
UNIV ROMA LA SAPIENZA
Space debris mitigation requirements specific to propulsion systems are scrutinized and compliance of OHB reference propulsion architectures is assessed. The risk of generating debris due to a failure in a propulsion system is assessed with a focus on the specific risk of a hypervelocity impact on a propulsion tank containing residuals.
The engineering activities, delta-qualifications or hardware development which can support the recommended propulsion passivation strategies are presented and prioritized.
OHB System AG
Generally speaking DIAMS has been an opportunity to secure the feasibility of the IOD in technical, programmatic and financial terms. More specifically DIAMS has allowed to define the end-to-end mission concept for this IOD, covering the design of various associated segments : Space Segment (Payload, Platform), and Ground Segment. Both interest and programmatic aspects have also been consolidated.
- On the technical plane :
Both the requirements and the design of the system have been refined to validate the IOD concept :
Airbus Defence &...
Satellite based optical communications in space is rapidly progressing, involving an increasing number of flight validations in LEO, GEO and beyond. Various space agencies successfully demonstrated both, optical Inter-Satellite communication Links (ISL's) which have been validated in flight experiments since 2001 and direct-to-Earth (DTE) optical communications.
RUAG SPACE
Scope of the MImOSA2 (Monitoring Ionosphere Over South America to support high precision applications) study was to support high-precision GNSS based applications in South America, analysing, through an original method, GNSS data acquired by a dense network of 50 Hz receivers to assess possible improvements on positioning accuracy when ionospheric degradation is taken into account.
Inst. Geografico Nacional
The depletion of stratospheric ozone due to anthropogenic emissions of long-lived substances containing chlorine and other halogens was first identified as a matter of international concern in the mid-1970s and has received increasing attention since the mid-1980s after the discovery of the ozone hole. Today, in spite of the successful application of the Montreal Protocol and its amendments, the atmospheric halogen loading is still above natural levels and will remain so until the middle of this century.
BELG INST SPACE AERONOMY
The activities carried out in the phase 0 deal with the mission concept and, in particular, with the interplanetary analysis and contributions to the mission requirements. The activities can be summarized as follows:
- study of the state of the art of Mars landers, with focus on issues such as the launcher, the interplanetary trajectory, the type of planetary approach, the design of the spacecraft, the layout, the mass and power budgets, the aerodynamic parameters, the entry, descent & landing strategy;
Ali SCARL
The MASCOT (Mobile Asteroid Surface Scout) lander onboard JAXA's Hayabusa 2 sample return mission to C-type Near Earth asteroid Ryugu is a lightweight (~ 10 kg) and compact (0.3 x 0.3 x 0.2 m3 ) landing platform with the capability to carry various in-situ experiments with a total mass of up to ~3 kg. Thus a system to payload mass ratio of 7:3 can be achieved.
DLR
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