Research

Simulating hypervelocity impact and spacecraft breakup with discrete elements

© Fraunhofer EMI

The impact of a piece of space debris and an orbiting satellite usually results in the breakup and fragmentation of the satellite into thousands of new fragments of space debris. This complex phenomenon is being studied with a unique type of numerical simulation based on millions of small particles.

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Augmented-reality-based remote assistance for satellite integration and test campaigns

© Fraunhofer EMI

Advanced automation of satellite integration, test campaigns and operations is becoming a key factor in the New Space domain. Augmented reality can maximize the level of telepresence for complex remote assistance tasks.

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ERNST update — new launcher, new launch date

© Fraunhofer EMI

While we completed the ERNST flight model and prepared it for acceptance testing in 2022, we face a delay of the launch to 2024.

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On-board data processing for the New Space

© Fraunhofer EMI

Following the successful demonstration of EMI’s data processing technology on the International Space Station, the next generation is now on the horizon.

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A reliable heat shield for ESA’s Space Rider mission

© ESA

Fraunhofer EMI contributes to the ESA’s Space Rider re-entry design with hypervelocity impact tests and impact damage modeling.

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ERNST — integrating the flight model

© Fraunhofer EMI

The development of the ERNST nanosatellite is entering the final phase in 2022 with the integration, testing and delivery of the flight model.

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ERNST on the finish line

© Fraunhofer EMI

The Fraunhofer EMI is developing he nanosatellite ERNST to demonstrate the potential of CubeSat-based small satellites for ambitious Earth observation tasks. Following the successful verification of the engineering qualification model, the critical design review marked the transition to the production and testing phase of the ERNST flight model, which is scheduled for launch in June 2022. 

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Military utility of small satellites

© Fraunhofer EMI

In the Micro Satellite Military Utility Project Agreement (MSMU PA) project, which is performed under the umbrella of the Responsive Space Capability Memorandum of Understanding (RSC MoU), Fraunhofer EMI investigates the military utility of small satellites for the German Federal Armed Forces in cooperation with nine partner countries.

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Space qualification of the ERNST nanosatellite

© Fraunhofer EMI

Fraunhofer EMI is currently developing the first Fraunhofer satellite ERNST. ERNST is a 12U nano-satellite that will demonstrate the potential and agility of this satellite class for the German Federal Armed Forces with a kryo-cooled infrared payload.

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New equipment and services for space qualification

© Fraunhofer EMI

In the space sector, Fraunhofer EMI stands for comprehensive and high-quality experimental and numerical simulations of hypervelocity impact pro-cesses such as the ones occurring during collisions of space debris with spacecraft or of asteroids and planetary surfaces. As part of our activities regarding small satellites, we have expanded our test spectrum for space qualification for components and CubeSats.

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A treasure for science – investigation of the ISS protection shield

© NASA/ESA

The Columbus module of the International Space Station (ISS) has been orbiting Earth since 2008. Natural micrometeoroids and anthropogenic space debris are impacting the module ever since. Columbus is well protected against this threat, because the meteoroid and debris protection system (MPDS) has been developed and tested at EMI.

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Small impacts with major impact – how micrometeoroids can disturb sensitive satellite payloads

© NSF/LIGO/Sonoma State University/Aurore Simonnet

Hypervelocity impacts on spacecraft surfaces cause fragments to be ejected. The fragment tracking method developed at Fraunhofer EMI allows detailed measurements of the properties of these fragments for the first time. The model developed shall be used to predict the influence of the space particle environment on the orbit and attitude of satellites.

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Flexibly reconfigurable image processing onboard satellites

The EMI data processing unit (DPU) features the latest generation of FPGA-based processors and allows high-performance image processing onboard small satellites.

© Fraunhofer EMI

Impact tests onto protective shields for the planned chinese space station TianGong

© Fraunhofer EMI

Fraunhofer EMI experimentally analyzes the protective shield concept for the planned chinese space station TianGong.

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Deployable drag sail for nanosatellites

© Rocket Lab

Satellites have to be removed from orbit after the end of mission. In this case, a satellite requires a de-orbiting device for the maneuver. At EMI, we are developing such a device for our nanosatellite ERNST.

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ERNST - Technology development for the New Space

© Fraunhofer EMI

The space technology industry is currently undergoing major changes, which are termed “New Space” by its protagonists. These changes, propelled by considerable private investments, include the implementation of large constellations of small serially produced satellites. 

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Numerical analysis of satellite collisions in orbit

© Fraunhofer EMI

Space debris moves at a high orbital speed and presents a destructive risk for satellites. For the risk assessment for space missions, simulation methods for tracking the amount of space debris are used that are based on empirical databases and estimations. At Fraunhofer EMI, numerical methods for the virtual simulation of complex collision events in orbit are developed in order to gain a better and more realistic understanding of the risks.

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EMI together with ESA and NASA

© NASA
The Columbus module of the ISS.

On September 5, and two weeks later on September 21 and 22, 2018, the outer hull of the Columbus module of the International Space Station (ISS) was visually inspected. These robotic camera screenings were the first systematic inspection since the module has been docked to the ISS more than ten years ago. The survey data will be utilized by Fraunhofer EMI and its project partners to improve our knowledge on the space debris population.

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