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Mobile – Selective Laser Melting (M-SLM) for Construction on the Moon

When setting up a lunar station, technologies for the use of locally available materials are crucial. Such technologies drastically reduce the need for transportation from Earth. This project idea aims to provide proof of a key technology, namely Mobile – Selective Laser Melting (M-SLM) for building large structures on the Moon.

Germany

20-D-T-TEC-03-f

Technische Universität...
Test automation exchange framework
Large aerospace projects require the collaboration from many partners, which often use their own development tools and frameworks. The validation of such projects relies heavily on test automation to increase the quality and reduce the costs. Unfortunately, the automated tests developed by each partner typically only address their specific activity and rely on specific tool. Over the past few years, several frameworks to support the automated testing and validation of the different parts of a space project have been produced and deployed.
Germany

GT1O-311GD

Etamax Space GmbH
Enabling Continuity: from Design to Operations

The D2OPS activity started with the goal of applying MBSE practices to enable digital continuity between design and operations. This study involves the following main activities:

Germany

20-D-T-TEC-04-a

VISIONSPACE TECHNOLOGIES...
MBSE enhanced by Semantic DataLake integration and Machine Learning

The Integrated MBSE Analytics Platform (IMAP) has been developed in the course of the OSIP [OSIP] MBSE campaign’s MBSE2DataLake project. It demonstrates how MBSE data can be downstreamed from early phases and integrated with Telemetry data or system operations data. Applying MachineLearning analytics and customized visualization on these sets of integrated data provides seamless analysis capabilities and data browsing experience for the user. The approach leads to linking the former separated domains of System Design and AIT/Operations.

Germany

20-D-T-TEC-04-h

ScopeSET
Space To Ground ICD Modeling And Generation

The MBSE and Space to Ground ICD activity started with the goal of applying MBSE practices to the preparation of the Space to Ground ICD (S2GICD). This study involves the following main steps:

Germany

20-D-T-TEC-04-e

VISIONSPACE TECHNOLOGIES...
On the Use of Mega-Constellation Services in Space

This activity investigates how mega-constellations can be used to provide low-Earth orbit (LEO) spacecraft with broadband low-latency services, a novel Concept with potential to disrupt spacecraft design, operation, and performance by allowing spacecraft to access mega-constellations’ enormous resources (Tbit/s throughputs) and global coverage at a lower cost than traditional data relay systems and ground station networks (two to fifty times cheaper, that is, a few hundred to a few thousand dollars per month for a daily net capacity from hundredths of Gbit up to almost ten Tbit).

Germany

S 2020-03

Vyoma
End-to-End System Engineering Portal (ESEP)

Space system engineering is a complex activity, spanning multiple phases and involving different stakeholders using a variety of engineering approaches and tools. ESA has been investing in Model-Based System Engineering (MBSE) research for many years, developing different MBSE frameworks and Domain Specific Tools (DSTs). Recently, a broader need has been recognized to focus the MBSE efforts on semantic interoperability and associated model integration.

Germany

20-D-T-TEC-04-d

Spacecube GmbH
Application of MBSE to reverse-engineer OPS-SAT and improve OPS-SAT2

The main objective of the project is the reverse engineering of the OPS-SAT system, creating a model of the existing system design. The model aims to be built in a way that it is most useful for OPS-SAT engineers to understand and discuss the existing design and use this as a basis for further development of the OPS-SAT system.

Germany

20-D-S-OPS-01-b

OHB System AG
Design for Recycling - Mission architectures to manufacture, refurbish and recycle satellites on-orbit

The main objective of the OMAR Mission Architecture study is to identify and trade-off different mission architectures, to provide different services on-orbit. For each of the relevant scenarios, this objective shall be achieved by defining the associated system functional analysis and by trading-off different architectures and concepts of operations. Furthermore, the impact of aspects such as: operational orbit, type of serviced satellites, services provided, different levels of autonomy, and any other relevant factors is to be assessed.

Germany

19-D-S-TEC-02

OHB System AG
Fast development of kinetic impactor for short-warning asteroid deflection

The study demonstrates that in an emergency situation, with only a very short warning time, the launch of a fast asteroid kinetic deflection mission is feasible (targeting launch-readiness in six months!), given that certain identified pre-requisites have been prepared well in advance. The capabilities and requirements of 'hijacking' and modifying a commercial spacecraft platform in order to perform asteroid kinetic deflection in the shortest possible time were consequently assessed.

Germany

19-D-S-TEC-01

Airbus

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