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24 results found
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
Detection of Ocean Litter Plastics with Hyper-to-multispectral Infrared Neural Networks (DOLPHINN)

Successfully mitigating the damage caused by marine litter requires large-scale, accurate mapping of oceanborne plastics across the globe. Quantifying where and how much plastic debris enters the marine environment in a global spatio-temporal sense is critical in formulating solutions to the plastic pollution problem. Satellite-based measurements can help to survey remote, isolated locations in which direct observations are sparse, costly, and difficult.

Canada

20-D-S-TEC-01-d

MDA systems
Small Satellite Missions to Mars – S2M2

The activity 'Small Satellite Missions to Mars (S2M2)' is an early-phase architecture study of a potential low-cost mission to Mars as further step in the Mars exploration roadmap developed by ESA.

A potential implementation from industry’s point of view was assessed, applying the strict design-to-cost philosophy by fostering strong reuse of an available OHB platform. Trade-offs were performed for assessing a low-cost mission profile targeting the programmatic constraints that were input to this study.

Germany

20-P-M-HRE-02-c

OHB System AG
Cyber Safety and Security Operational Centre (CSOC) Phase 1
Belgium

GT1Y-001IS

RHEA SYSTEM S.A.
Development of partitioned Prototype Application (IMA-SP application development and software maintenance)

Integrated Modular Avionics (IMA) is a concept developed for the aeronautics industry to manage the growth in functionality and efficiency required as the industry grows. Integrated Modular Avionics for Space (IMA-SP) is a spin-in of the corresponding concept for spacecraft avionics. 

Czech Republic

G617-150SW

EVOLVING SYSTEMS...
COOL ? Compact Optical clOck Laser
Optical atomic clocks are based on using lasers to measure very narrow and stable atomic transitions. Narrow refers to the fact that only a limited range of optical frequencies can be used to excite/measure the transition in the atom. ;For the target space based optical clock, this requires the laser frequency to be controlled to approximately one part in a trillion.
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Switzerland

GT27-017MM

MicroR Systems
De-risk assessment: Threat Risk Assessment on LEO Satellite Constellation (TRALEO)

n/a

Belgium

G617-241TAdd

RHEA SYSTEM S.A.
sat4EO

Developing a high-performance, but low cost satellite with very high resolution products would open the Earth Observation market to a new audience, creating a path for new applications and ultimately encouraging competitiveness.

These products are currently not often covered by the space industry and access is very limited. As such a new low cost satellite, with turnkey technology could open the market considerably. A new activity, with GSTP Element 2 and Spain, has developed a spacecraft to do just that. 

Spain

G621-053SY

DEIMOS ENGINEERING AND...
Improvement, Automated Source-code-based Testing
State-of-the-art in automated unit/integration testing is a semi-automated approach for which the test environment is established manually, while execution of tests is automated. In contrast to that, the FAST approach already automates building of the test environment and the stimulation of the software, complemented by recording of input-output vectors, observed properties, anomalies and evaluation by metrics and filtering algorithms.
Germany

G617-154SW

Dr. Rainer Gerlich BSSE...
Design of space hardware using a CDF like methodology (AMCDF)

The project aimed to establish a structured approach to an optimised part or component by applying Concurrent Design methods. It intended to incorporate all necessary disciplines and competencies that are required for a potential spacecraft part. Within the activity, advanced manufacturing included various novel techniques, not only additive manufacturing. It means that the Concurrent Design approach was developed for the engineering of units to be built with a broad range of advanced manufacturing technologies.

Germany

15/007

OHB System AG

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