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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
M4 Phase A/B1 XIPE PHASE A

XIPE is designed to be launched with a VEGA-C vehicle into an orbit of 550 km and <6° inclination. With this orbit, eclipses last about 35 minutes. Due to remaining spacecraft fragments the mission is planned to end by controlled re-entry. The baseline ground station is Kourou either for S/S or S/X telemetry band, albeit Malindi (or Singapore) is additionally available, if necessary, for additional downloading capability in case of particularly bright sources. The mission duration is 3+2 years.

Italy

15/M23-a-2

Thales Alenia Space
Small Mars Satellite

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;

Italy

15/714

Ali SCARL
COBRA Extension of the IRIDES Experiment 13/702

The COBRA (COntactless deBRis Action) concept was studied under ESA contract and then internally by ESA, as part of ESA ́s SysNova technology assessment scheme which uses “technology challenges” and competitions to survey a comparatively large number of alternative solutions. The concept was originally proposed by an industrial consortium led by GMV form Spain with Politecnico di Milano and Thales Alenia Space from Italy. The concept came first in response to a challenge for mission concepts and technologies capable of providing a contactless Earth-bound object orbit modification system.

Spain

13/702

GMV
Active Debris Removal for a small satellite mission

In recent years the concern about the future exploitation of space has been growing due to the risk that uncontrolled space debris poses to the space environment and therefore to the survivability of operational spacecraft. Two main regions of concern exist, GEO, where most of the commercial telecommunications satellites orbit, and LEO, where many scientific missions observing the Earth fly. Of special concern is the sun synchronous orbit, a natural resource of special interest for Earth sciences.

Spain

13-700

GMV
Pre-Phase A Study of Earth Re-entry Vehicle / Capsule
France

2003-33

EADS Launch Vehicles
PHASE A STUDY OF EXOMARS MISSION
France

2003-29

Alcatel Alenia Space
PHASE A STUDY OF EXOMARS MISSION
France

2003-28

EADS Astrium SAS
Pre-Phase A Study of Earth Re-entry Vehicle / Capsule
UK

2003-32

Surrey Satellite...
SOLAR SYSTEM: MERCURY ORBITER (rider to 97/S50)
Italy

1999-7

Alenia Aerospazio

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