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Preparation of enabling space technologies and building blocks: BBK for Low Power PPU

TAS-B has high heritage on PPU for HET ranging from 1,35 kW up to 4,5 kW. In the frame another project, TAS-B  develops New Space PPU modules to drive thrusters in the same power range, for platforms with 100 V regulated power bus. In the frame of the project “BBK for Low Power PPU”, TAS-B addresses the low range of the New Space market: smaller thrusters for smaller platforms with lower unregulated bus.

Belgium

GT17-137TIt

THALES ALENIA SPACE...
Model Based Avionics

SAVOIR has produced a set of generic specification under the form of documents, based on some physical architecture of equipment that was state of the art at that time. The new functional model based approach is more based on functional chains and models. It is expected that modelling the SAVOIR avionics architecture and generic specification using the MBSE techniques, in particular Arcadia method and Capella tool, will allow to have an innovative standpoint on the SAVOIR standardisation.

France

20-D-T-TEC-05

Thales Alenia Space
Artificial intelligence (AI) and natural language processing (NLP) to support space engineering activities

Model based approaches have proved to be efficient in supporting engineering activities, models replacing traditional document-based approaches. Nevertheless even in most advanced deployments, a lot of engineering artifacts are textual either because the return on investment of introducing models is too low on this particular case or because the information is more efficiently expressed in natural language even if consistency and correctness issues appears.

France

20-D-T-TEC-04-n

Thales Alenia Space
MBSE Deployment for EnVision Science Mission Study
  • Enforce the use of the physical engineering model that TAS-F already has by sub-system architects in order to have the model as a central source of truth
  • Produce an interactive representation of the model allowing its consultation without having to install dedicated modelling tools
  • Produce trend graphs on system budgets
  • Produce document generation capability to export graphs and tables to the system and subsystem budget reports
France

20-P-M-SCI-02

Thales Alenia Space
OMAR – On orbit manufactured spacecraft

The objective of this activity is to assess the system level and design impacts of optimising a satellite design for on-orbit manufacturing and assembly, as well as preparing it to be refurbished, reused or recycled on orbit afterwards, and to identify the technologies needed.

Italy

19-D-S-TEC-05

Thales Alenia Space
Mars Surface Platform Capabilities

The objective of this study was to help define how to maintain and further develop European access to the surface of Mars, the major destination for European exploration, following the most recent approved and developed (or currently in development) missions (ExoMars 2016, ExoMars RSP).

Italy

20-P-M-HRE-01-a

Thales Alenia Space
Small Satellite Missions to Mars – S2M2

The focus of this study was the system-level assessment of potential small mission architectures that could operate at Mars in the 2030s, after or potentially in parallel with MSR mission.

In particular two cases were evaluated:

  • Mission 1: Mars Communications Constellation (MCC), for supporting assets on the surface and providing science
  • Mission 2: Mars Science Orbiter (MSO), a science-driven mission, remote sensing
Italy

20-P-M-HRE-02-b

Thales Alenia Space
Space Debris Deflection by Space-Based Laser

The study takes place in the context of the space environment remediation. Tackling the issue of space debris is becoming more and more critical as it becomes more dangerous for existing and future space missions. Solutions must be found to ensure the security of space missions security and a clean space environment. Laser pressure solutions are considered promising as they only using momentum transfer to perform debris manoeuvres to avoid collisions. This means that no additional debris is generated using this technique.

France

19-D-T-OPS-01

Thales Alenia Space
Active Optics in deployable systems for future EO and Science missions

Increasingly demanding space-based applications require a large primary mirror diameter, on which the optical instrument resolution depends. However, the mass and volume of a monolithic primary mirror would dramatically increase along with its size, which, in addition to cost and technical issues, is also limited by the available volumen in the launch vehicle fairing.

France

15/131

Thales Alenia Space
Innovative security concepts, mechanisms and architectures for future space missions

This study aimed to achieve the following objectives:

  • To anticipate the security needs and requirements of future space missions (Earth observation, communication, navigation, science, exploration, etc.) with respect to architectures considered for future missions.

  • To build an advanced security architecture portfolio embedding state-of-the-art security concepts, technics, technologies, components and solutions.

France

15/018

Thales Alenia Space

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