These devices interact with the Earth’s magnetic field and create control torque, which can be adjusted to the required value. Combined with one or more reaction wheels, they provide all the control you need to maintain your spacecraft’s attitude, from low-Earth orbit up to geo-stationary orbit. And, unlike thrusters, torquers do not need valuable consumables, are low power components and high reliable.

Mass spectrometer for analysis of dust particles in the immediate surroundings of the comet

Joint research project with:
Eureka: Sensor Technology, Telematics
DLR: Remote Sensing
University Würzburg: Pico-Satellites
Zentrum für Telematik e.V.: Satellite Network

Execution of RAMS (Reliability, Availability, Maintainability, Safety) Analysis with focus on hazard analysis and FMEA.

Plans for software develoment, verification and verification, CM, design

• Definition of test concepts: test / integration / work instructions, circuit plans
• First article inspections, acceptance tests
• Equipment safety files
• Operational Tests
• Generation of verification documents, verification at hardware
• RAMS calculations and analyses
• Integrated Logistic Support / Logistic Support Analysis (ILS/LSA) plans
• LORA, LCC
• Technical Documentation

Definition of Security Test Cases covering all security aspects on system level
Analysis of impact of security requirements, accreditatin, certificatin
Definition and execution of security test procedures