ECSSMET 2026 Programme
The final programme for ECSSMET 2026 is now available.
10:00 – 13:00
Historische Maschinenhalle
Arrival and Registration
12:00 – 13:00
Historische Maschinenhalle
Networking Lunch
13:00 – 15:00
Historische Maschinenhalle
Welcome and Introduction
15:00 – 15:30
Historische Maschinenhalle
Break
15:30 – 16:00
Session M1, Composite Design, Historische Maschinenhalle
Development, Characterization and Full-Scale Validation of Integrated CFRP Ring Joints for Launcher Payload Adapters
15:30 – 16:00
Session M1, Structural dynamics, Nimes 2
Challenges and complexities for LISA LV/SC Coupled Load Analysis
15:30 – 16:00
Session M1, Demise, Kasan
Development of Demisable Structural Joints
15:30 – 16:00
Session M1, Material properties, Nimes 1
Then, now, and what lies ahead – a history and future vision for materials and manufacturing processes
16:00 – 16:30
Session M1, Composite Design, Historische Maschinenhalle
Development of an AFP manufactured CFRP launcher interface frame for ESA’s Harmony mission satellites
16:00 – 16:30
Session M1, Structural dynamics, Nimes 2
Enhanced data-based dynamic characterization of PLATO satellite through qualification testing
16:00 – 16:30
Session M1, Demise, Kasan
A Multi-Level Testing Framework for the Development of Demisable Satellite Structures
16:00 – 16:30
Session M1, Material properties, Nimes 1
Assessment of High Entropy Alloys for Space Applications
16:30 – 17:00
Session M1, Composite Design, Historische Maschinenhalle
Black Engine Technology - Design of a structural Health Monitoring system for a CFRP load jacket
16:30 – 17:00
Session M1, Structural dynamics, Nimes 2
Multi-axis Shock Synthesis for Spacecraft Qualification Testing
16:30 – 17:00
Session M1, Demise, Kasan
Optimizing a Representative LEO Satellite System Architecture for Demise
16:30 – 17:00
Session M1, Material properties, Nimes 1
Polyimide-Based Nanocomposite Coatings for Quartz Components in Deployable Space Antenna Structures
17:00 – 17:30
Session M1, Composite Design, Historische Maschinenhalle
Physics-Informed Machine Learning for Thermoplastic Induction Heating of CFRP Structures in Space Applications
17:00 – 17:30
Session M1, Structural dynamics, Nimes 2
Shock propagation in launcher and spacecraft structures – Numerical simulations and source characterization
17:00 – 17:30
Session M1, Demise, Kasan
In-Orbit Demonstration Mission Concept of Bio-Based Materials for Spacecraft Applications
17:00 – 17:30
Session M1, Material properties, Nimes 1
NanoWeld® Reinforced CFRP Laminates for Space Applications: Mechanical Performance and Diffusion Barrier Effects with Implications for Cryogenic Helium Permeability
17:30 – 18:00
Session M1, Structural dynamics, Nimes 2
Tightly Coiled Boom Deployment Dynamics
17:30 – 18:00
Session M1, Material properties, Nimes 1
A damage mechanics model for failure assessment of filament wound FRP materials on [±alpha]-ply level
18:00 – 20:30
Welcome reception at the conference Hotel
08:30 – 09:00
Session TS1, Structure design, Nimes 1
Structural and Thermal Design Study for the SPICE X-Ray Detector
08:30 – 09:00
Session TS1, DFAT, Kasan
Satellite modal survey testing with a DFAN setup: comparing acoustic and shaker excitation
08:30 – 09:00
Session TS1, Additve manufacturing, Nimes 2
Additive Manufacturing of an Optical Bench for NewATHENA: From Concept to Reality
08:30 – 09:00
Session TS1, Design and verification, Historische Maschinenhalle
Verification of the TANGO instrument Thermal-Mechanical Design through Analysis and Tests
09:00 – 09:30
Session TS1, Structure design, Nimes 1
Argonaut: The Mechanical Architecture of the Propulsion Subsystem
09:00 – 09:30
Session TS1, DFAT, Kasan
On the effect of a panel inclination during a Direct Field Acoustic Test
09:00 – 09:30
Session TS1, Additve manufacturing, Nimes 2
Multifunctional Battery Frame for Space Systems Enabled by Metal Additive Manufacturing: Design and Validation of the BatmAM 96‑Cells Demonstrator
09:00 – 09:30
Session TS1, Design and verification, Historische Maschinenhalle
IN-FLIGHT CALIBRATION OF OPTICS FOR OCEAN COLOR MISSION: QUALIFICATION OF A STEPPER MOTOR-HARMONIC DRIVE BASED MECHANISM WITHOUT HDRM
09:30 – 10:00
Session TS1, Structure design, Nimes 1
Structural design of the Wide Field Imager for the NewATHENA X-Ray Telescope
09:30 – 10:00
Session TS1, DFAT, Kasan
A Multi-SISO Fractional Octave Control Architecture for Direct Field Acoustic Noise Testing
09:30 – 10:00
Session TS1, Additve manufacturing, Nimes 2
Design-for-Additive-Manufacturing of RF Components: Integrated manufacturing Process Development for Maritime Surveillance Applications
09:30 – 10:00
Session TS1, Design and verification, Historische Maschinenhalle
Preliminary Design Study for Thin-layered Thermal Protection Systems for Future, Reusable Spacecraft Structures Exposed to Moderate Heat Loads
10:00 – 10:30
Session TS1, DFAT, Kasan
Evaluating the effect of stacked structures on their vibroacoustic response during acoustic testing using Direct Field Acoustic Testing (DFAT)
10:00 – 10:30
Session TS1, Additve manufacturing, Nimes 2
Developing Low-Binder Lunar Regolith-Based Geopolymers for Construction on the Moon Using Cement Contour Crafting Additive Manufacturing
10:30 – 11:00
Break
11:00 – 11:30
Session TS2, Structural analysis and simulation, Historische Maschinenhalle
Meshless FEM approach: Current status and road map - OHB industrial experience
11:00 – 11:30
Session TS2, Deployable structures, Nimes 2
Low-Cycle Fatigue Behaviour of a Deployable CFRP Lenticular Mast System for Small Satellite Applications
11:00 – 11:30
Session TS2, DFAT, Kasan
Developments in diffuse soundfield modelling and its application to Direct Field Acoustic Noise (DFAN) test performance quantification: metrics and case studies
11:00 – 11:30
Session TS2, Additve manufacturing, Nimes 1
How 4D printing can bring sustainability to space exploration?
11:30 – 12:00
Session TS2, Structural analysis and simulation, Historische Maschinenhalle
Dynamic Modelling of Fluid-Structure Interaction in Thin-Walled Liquid Propulsion Stages with the Real Coupled Modes Method
11:30 – 12:00
Session TS2, Deployable structures, Nimes 2
Novel Deployable Structure Consisting of a Convex Boom and a Bellows Structure
11:30 – 12:00
Session TS2, DFAT, Kasan
The Importance of the Degree of Diffuseness of the Achieved Acoustic Field on the Vibroacoustic Response of a Test Article from Direct Field Acoustic Testing
11:30 – 12:00
Session TS2, Additve manufacturing, Nimes 1
Continuous (recycled) fiber - filaments printed in large scale additve manufacturing
12:00 – 12:30
Session TS2, Structural analysis and simulation, Historische Maschinenhalle
Launch Vehicle ascent phase loading: Comparing Traditional and CFD-Based Approaches
12:00 – 12:30
Session TS2, Deployable structures, Nimes 2
Application of Metamaterials for Vibration Attenuation in Space Structures: A Case Study on a simplified Large Deployable Reflector ring
12:00 – 12:30
Session TS2, DFAT, Kasan
The INVAP Methodology for High-Fidelity Vibro-Acoustic Correlation of a Stowed Solar Array via DFAT
12:00 – 12:30
Session TS2, Additve manufacturing, Nimes 1
Modelling and Experimental Validation of a Laser Powder Bed Fusion-Manufactured Aluminium Lattice Sandwich Panel
12:30 – 13:00
Session TS2, Structural analysis and simulation, Historische Maschinenhalle
EVALUATION OF STRUCTURAL ANALYSES FOR METUCUBE SATELLITE: LESSONS LEARNED
12:30 – 13:00
Session TS2, Deployable structures, Nimes 2
DEPLOYMENT DEMOSTRATOR FOR STACKED TRIBAND ANTENNA
12:30 – 13:00
Session TS2, DFAT, Kasan
Recent upgrades to the Large Electro Acoustic Facility at ESA ESTEC
12:30 – 13:00
Session TS2, Additve manufacturing, Nimes 1
Application of thermoplastic composite technology for satellites manufacturing
13:00 – 14:00
Lunch
14:00 – 14:30
Session TS3, Structure design, Historische Maschinenhalle
Trifilar helicoid antenna design, prototyping and testing
14:00 – 16:00
Session TS3, Sustainable Spacecraft Structures, Kasan
Workshop 1: Load Derivation: Safety Factors and Margin Policies !!!NEW ROOM: Nîmes 2!!!
14:00 – 14:30
Session TS3, Sustainable Spacecraft Structures, Kasan
Evolution of perforation kinetic energy in hypervelocity impact on Whipple shield bumpers
14:00 – 14:30
Session TS3, Acoustic testing, Nimes 1
Towards a true Digital Twin: Validation of a high-fidelity Numerical Model of a Direct Field Acoustic Test
14:30 – 15:00
Session TS3, Structure design, Historische Maschinenhalle
ARIEL Primary Mirror Mounting Re-design
14:30 – 15:00
Session TS3, Sustainable Spacecraft Structures, Kasan
Demisable Krypton Tank – Final Presentation
14:30 – 15:00
Session TS3, Acoustic testing, Nimes 1
High-Precision Microphones Localization for DFAN Testing Through a High-Accuracy TDOA Algorithm
15:00 – 15:30
Session TS3, Structure design, Historische Maschinenhalle
A lander and transfer stage’s structural design concept study for asteroid sample return missions
15:00 – 15:30
Session TS3, Sustainable Spacecraft Structures, Kasan
Integrating Demisability and Atmospheric Impact into Sustainable Spacecraft Material Selection
15:00 – 15:30
Session TS3, Acoustic testing, Nimes 1
Integrating DFAN and Vibration Testing in a Shared Facility: Engineering Solutions for RAL Space's New Environmental Test Center
15:30 – 16:00
Session TS3, Structure design, Historische Maschinenhalle
PLANETARY PROTECTION PLATFORM RE-USE: OHB INDUSTRIAL EXPERIENCe
15:30 – 16:00
Session TS3, Sustainable Spacecraft Structures, Kasan
Polymeric composite contributions to eco-design and advanced concept for space
15:30 – 16:00
Session TS3, Acoustic testing, Nimes 1
Case Study of a Large Scale DFAN Test: Part Two
16:00 – 17:00
Break
17:00 – 17:30
Session TS4, Material, Nimes 2
AMoCSiS: Development of a Cutting Process for CFRP Tubes in Automated In-Orbit Manufacturing
17:00 – 17:30
Session TS4, Shock testing, Nimes 1
Relevant parameters for improved transient shock analysis and testing of a satellite structure
17:00 – 17:30
Session TS4, Design and verification, Historische Maschinenhalle
Dynamic Test Model Correlation and Load Assessments for the ROSE-L Spacecraft Lessons Learned from Sine and Acoustic Qualification
17:00 – 17:30
Session TS4, ALM Design, Kasan
3D printed SiSiC free-form optic mirror for S2NG
17:00 – 18:30
City Tour in Brunswick
This tour will start and end at the Steigenberger Hotel (venue).
17:30 – 18:00
Session TS4, Material, Nimes 2
ICME-driven design of functionally graded materials for advanced space applications
17:30 – 18:00
Session TS4, Shock testing, Nimes 1
Shock subsystem qualification testing: Secondary notching approach
17:30 – 18:00
Session TS4, Design and verification, Historische Maschinenhalle
Qualification of Oxford Space Systems large deployable offset reflector
17:30 – 18:00
Session TS4, ALM Design, Kasan
3D printed SiSiC for space applications
18:00 – 18:30
Session TS4, Material, Nimes 2
Stress Rupture
18:00 – 18:30
Session TS4, Shock testing, Nimes 1
Shock prediction enabled by artificial intelligence techniques
18:00 – 18:30
Session TS4, Design and verification, Historische Maschinenhalle
Structural Architecture and Mechanical Design Optimization of the HAWK PLUS Modular Platform for High-Cadence Production
19:00
Rooftop terrace Soldekk
08:30 – 09:00
Session W1, Structure design, Historische Maschinenhalle
Landing Leg System Development for Reusable Launchers
08:30 – 09:00
Session W1, Material imperfections, Kasan
Influence of Deterministic & Probabilistic Verification Methods on Failure Probability & Margin of Safety for Ceramic Space Structures
08:30 – 09:00
Session W1, Material properties, Nimes 1
Fatigue and Fracture Behaviour of Al2618–TiB₂ Metal Matrix Composite Produced by PBF-LB
08:30 – 09:00
Session W1, Shaker Test Predicition and Testing, Nimes 2
REASSESSING DYNAMIC MODEL PREDICTIONS THROUGH TESTING OF INVAP MODULAR ELECTRONIC UNITS
09:00 – 09:30
Session W1, Structure design, Historische Maschinenhalle
A Simplified and Robust Approach for Preliminary Torque Margin Sizing of Large and Deployable Space Structures
09:00 – 09:30
Session W1, Material imperfections, Kasan
Probabilistic assessment of space components manufactured by L-PBF
09:00 – 09:30
Session W1, Material properties, Nimes 1
Healing Materials for Harsh Space Environments: Intrinsic Self-Healing Copolyimides for Lunar Exploration
09:00 – 09:30
Session W1, Shaker Test Predicition and Testing, Nimes 2
Experimental Validation of a Semi-Defined SD2DOF Impedance-Based Approach for Horizontal Satellite Vibration Testing
09:30 – 10:00
Session W1, Structure design, Historische Maschinenhalle
STRUCTURAL ARCHITECTURE, MECHANISM DESIGN, AND INTEGRATION METHODOLOGY FOR METUCUBE SATELLITE
09:30 – 10:00
Session W1, Material imperfections, Kasan
Probabilistic Fatigue Design of Additively Manufactured Structures Using Cumulative Probabilities of Critical Defects (CPoCD)
09:30 – 10:00
Session W1, Material properties, Nimes 1
Development and Space Qualification of a Cost-Efficient FFF-Printable Thermoplastic for structural and non-structural Low Earth Orbit Applications
09:30 – 10:00
Session W1, Shaker Test Predicition and Testing, Nimes 2
Mechanical Breadboard Vibration Testing and Structural Valida-tion of the Detector Electronics Subsystem (DES) for the NewAthena WFI Instrument
10:00 – 10:30
Session W1, Material imperfections, Kasan
Investigation of the Influence of Laser Powder Bed Fusion (LPBF) Processing Parameters (Contour Scan) on Microstructural Properties and Resulting Crack Initiation Behavior under Cyclic Loading for AlSi7Mg0.6 Material.
10:00 – 10:30
Session W1, Shaker Test Predicition and Testing, Nimes 2
Shock Response Prediction of a Spacecraft Structure Using Explicit Finite Element Analysis: Model Conversion, Damping Identification, and Test Correlation
10:30 – 11:00
Break
11:00 – 11:30
Session W2, Structure engineering, Nimes 1
SemaNtic dAta exchange capabilities in the space Supply Chain to remove barriers in intEroperability processes by deploying opeN sTandards (NASCENT)
11:00 – 11:30
Session W2, Deployable structures, Historische Maschinenhalle
Experimental and Analytical Study on CFRP Bistable Booms Considering Time- and Temperature-Dependence
11:00 – 13:00
Session W2, Nimes 2
Workshop: Thermo-elastic Design and Verification Methodologies
11:00 – 11:30
Session W2, Margin policies, Kasan
A Framework for Structural Margin Assessment of Aerospace Structures under Time-Consistent Combined Load States
11:30 – 12:00
Session W2, Structure engineering, Nimes 1
CALLISTO VEB Structures Engineering – Lessons Learned
11:30 – 12:00
Session W2, Deployable structures, Historische Maschinenhalle
DEPLOYABLE VHF ANTENNA FOR REMOTE RADAR SENSING APPLICATION
11:30 – 12:00
Session W2, Margin policies, Kasan
Updating the ECSS standard for structural design and verification of pressurized hardware
12:00 – 12:30
Session W2, Structure engineering, Nimes 1
Prediction of shock injection levels using normalized energy representation of the source
12:00 – 12:30
Session W2, Deployable structures, Historische Maschinenhalle
A Manufacturing-Oriented Geometrically Nonlinear Procedure for Identifying the Optimal Zero-Stress Configuration of Cable Nets and Meshes in Large Deployable Reflectors
12:30 – 13:00
Session W2, Structure engineering, Nimes 1
Design Principles of a Spacecraft Structural Digital Twin
12:30 – 13:00
Session W2, Deployable structures, Historische Maschinenhalle
Kinematics-Driven Deployment Analysis of an Inflatable Lunar Habitat with Nonlinear Membrane Response
13:00 – 14:00
Lunch
14:00 – 14:30
Session W2, Vibration testing, Kasan
Decoupling Spacecraft Dynamics from Shaker Table Interactions for Fixed-Base Modal Characterization
14:00 – 14:30
Session W2, Production, Nimes 2
Quantitative Assessment of Peel Ply Performance on CFRP Substrates
14:00 – 16:00
Session W2, Nimes 1
Workshop: Acoustic Testing and DFAN
14:00 – 14:30
Session W2, Thermoelastic, Historische Maschinenhalle
Composite Metering Structure Optimization based on Genetic Algorithm for a High-Resolution Spaceborne Electro-Optical Camera
14:30 – 15:00
Session W2, Vibration testing, Kasan
Smart Compliant Mechanism for improved Environmental Testing
14:30 – 15:00
Session W2, Production, Nimes 2
Data‑Driven Process Control for High-Tech Composite Manufacturing
14:30 – 15:00
Session W2, Thermoelastic, Historische Maschinenhalle
Aeolus-2 PLH Thermo-Elastic Analysis and Temperature Mapping for Preliminary Design Review
15:00 – 15:30
Session W2, Vibration testing, Kasan
Phase-Locked Loop-Based Vibration Testing: A Versatile Framework for Advanced Structural Testing
15:00 – 15:30
Session W2, Production, Nimes 2
Series Production of Optical Instrument Structures for Medium-Sized Satellites: Challenges Arising from Designs Not Conceived for High-Rate Manufacturing
15:00 – 15:30
Session W2, Thermoelastic, Historische Maschinenhalle
A Sensitivity-Driven Thermoelastic Methodology for Robust Assessment of Payload Distortions in Satellite Structures
15:30 – 16:00
Session W2, Vibration testing, Kasan
Globally optimal multi-axis vibration test inputs via convex programming
15:30 – 16:00
Session W2, Production, Nimes 2
Manufacturing the PLATO Optical bench: a large, stable and lightweight structure for 26 telescopes
15:30 – 16:00
Session W2, Thermoelastic, Historische Maschinenhalle
Thermal Design and Simulation of the High-Resolution Spaceborne Electro-Optic Camera for Thermo-Elastic Stability
16:00 – 17:00
Break
17:00 – 17:30
Session W3, Shock testing, Nimes 2
Energy-Based Severity Metric for Transient Shock Characterization
17:00 – 17:30
Session W3, Shaker Test Predicition and Testing, Nimes 1
Predicting nonlinear vibrations of thin plates: the Comet-I case-study
17:00 – 17:30
Session W3, Thermal testing, Historische Maschinenhalle
Development and Validation of a Thermal Control System for the Large Space Test Chamber Loading Trolley
17:00 – 17:30
Session W3, Micro vibration, Kasan
Frequency Domain Methodology for Microvibration Analysis
17:30 – 18:00
Session W3, Shock testing, Nimes 2
Improved shock specification tool using Artificial Intelligence and spacecraft surrogate models
17:30 – 18:00
Session W3, Shaker Test Predicition and Testing, Nimes 1
Virtual shaker testing for test de-risking: notch predictions on a full-scale spacecraft setup
17:30 – 18:00
Session W3, Thermal testing, Historische Maschinenhalle
TCS Performance of the new Thermal Vacuum Facility at IABG’s Competence Centre Optics
17:30 – 18:00
Session W3, Micro vibration, Kasan
Hybrid Microvibration Damping Platform with Data-driven Robust Disturbance Rejection Control
18:00 – 18:30
Session W3, Shock testing, Nimes 2
Prediction and Optimization of Shaker Shock Tests of Optical Units
18:00 – 18:30
Session W3, Thermal testing, Historische Maschinenhalle
Sun simulator mirror alignment using laser radar
18:00 – 18:30
Session W3, Micro vibration, Kasan
MVIS Micro-Vibration Isolator - OHB Industrial Application
19:00 – 22:00
Conference Dinner
08:30 – 09:00
Session TH1, Mechanism Testing, Nimes 2
Main Functional Tests of CALLISTO’s Landing System – Touchdown and Deployment
08:30 – 09:00
Session TH1, Buckling, Nimes 1
Post-buckling dynamics as a passive isolation mechanism in a deployable telescopic baffle
08:30 – 09:00
Session TH1, Additive layer manufacturing process, Historische Maschinenhalle
Application of a Methodology for Void Structure Control in Continuous Fiber Additive Manufacturing for Space Structures
09:00 – 09:30
Session TH1, Mechanism Testing, Nimes 2
Experimental Characterization of a Deployable Piezoelectric Polymer Reflector for CubeSat Applications
09:00 – 09:30
Session TH1, Buckling, Nimes 1
Post-Buckling Analysis and Sizing of a Space Structure: Application to Inter-Tanks Skirt
09:00 – 09:30
Session TH1, Dynamic, Kasan
Flow induced vibrations in flexible lines – phenomenon and methods to assess associated risks
09:00 – 09:30
Session TH1, Additive layer manufacturing process, Historische Maschinenhalle
AM compliant mechanisms: warpage compensation to improve guiding performances
09:30 – 10:00
Session TH1, Mechanism Testing, Nimes 2
Studies on preload release mechanisms for shock reduction
09:30 – 10:00
Session TH1, Buckling, Nimes 1
Non-linear Buckling Analysis of the Inter-Tank Structure for the CALLISTO Reusable Rocket Demonstrator: Structural Stability Assessment of the LOX/LH2 Interface
09:30 – 10:00
Session TH1, Dynamic, Kasan
Compliance Of Spacecraft Units to Random Vibration Environment: Assessment Methodology and Practical Applications
09:30 – 10:00
Session TH1, Additive layer manufacturing process, Historische Maschinenhalle
Powder boundary conditions in Directed Energy Deposition simulations and the relevance of particle size
10:00 – 10:30
Session TH1, Mechanism Testing, Nimes 2
Frangible Joint: Overview of Design, Validation and Qualification Test Programme
10:00 – 10:30
Session TH1, Buckling, Nimes 1
Progress in non-destructive buckling prediction of real-scale thin-walled structures by vibration
10:00 – 10:30
Session TH1, Dynamic, Kasan
Satellite Materials Outgassing: Impact of Environmental Conditions
10:30 – 11:00
Break
11:00 – 11:30
Session TH2, Deployable structures, Nimes 1
Structural Design Trade-Offs for a Deployable Rollable Solar Array
11:00 – 13:00
Session TH2, Nîmes 2
Workshop: Digitalisation in Structures Development, Manufacturing and Testing
11:00 – 11:30
Session TH2, In flight experiments, Kasan
Flight correlation status of ESA Coupled Loads Analysis tool for Vega-C
11:30 – 12:00
Session TH2, Composite Design, Historische Maschinenhalle
Development of Composite Sandwich Intertank and Interstage Structures
11:30 – 12:00
Session TH2, Deployable structures, Nimes 1
Design of a deployable structure that can be rolled up for storage
National Defense Academy of Japan, Prof. Dr. Hiroaki Tanaka
11:30 – 12:00
Session TH2, In flight experiments, Kasan
In-Orbit Test of a DLR Camera SpaceMast System
12:00 – 12:30
Session TH2, Composite Design, Historische Maschinenhalle
Design, Analysis, and Testing of Grid-Stiffened Composite Multi-Payload Adapters as an Alternative to Metallic ESPAs
12:00 – 12:30
Session TH2, Deployable structures, Nimes 1
Nanomagsat: an ultra-compact deployable boom for smallsat and cubesat missions.
12:00 – 12:30
Session TH2, In flight experiments, Kasan
Tightly Coiled Boom Deployment Dynamics
12:30 – 13:00
Session TH2, Deployable structures, Nimes 1
Development of the Bistable Asymmetric Collapsible Booms for Roll-Out Mechanisms
13:00 – 14:00
Lunch
14:00 – 14:30
Session TH3, Postersession
- A Methodology for Investigating Shock Propagation through CubeSat Structures Subject to Hyper-Velocity Impacts of Small Debris - European Space Agency ESTEC
Anushka Dongare
- Compression Behavior of Composite Sandwich Structures with Aluminum and Foam Cores in Diameter Transition Regions
Korea Aerospace Research Institute, Dr JONGWOONG LEE
Anushka Dongare
Korea Aerospace Research Institute, Dr JONGWOONG LEE
14:00 – 14:30
Session TH3, Postersession
- Environmental testing of a constellation: Constellr SkyBee-A satellites. Evolution
Constellr Gmbh, Jesús Crespo González - Calero
- Pycnometer-Based Assessment of 3D Volumetric Measurements System for Nanosatellite Debris Characterization
R.Tech RTECH / STERADIAN RTECH / STERADIAN, Martin Spel
Constellr Gmbh, Jesús Crespo González - Calero
R.Tech RTECH / STERADIAN RTECH / STERADIAN, Martin Spel
14:00 – 14:30
Session TH3, Postersession
- Automating TQCM Data Evaluation to Improve TVAC Contamination Monitoring: Demonstrated on the FORUM OBA Bake-Out Campaign
OHB System AG, Florian Reineke
- Analysis and design of anisogrid type structures for science missions applications -
Space Composite Structures DENMARK ApS, Damir Ljubicic
OHB System AG, Florian Reineke
Space Composite Structures DENMARK ApS, Damir Ljubicic
14:00 – 14:30
Session TH3, Postersession
- Electrospun Hydrogen-Rich Nanofibrous Mats for Lightweight Radiation-Shielding Concepts in EVA Suits -
Sapienza University of Rome, Lorenzo Ferri
- Experimental Validation and FEA Correlation of Aluminum Skin-Stringer Panels under Compression with Increased Rivet Pitch -
Korea Aerospace Research Institute, Dr Hae-Won Jang
Sapienza University of Rome, Lorenzo Ferri
Korea Aerospace Research Institute, Dr Hae-Won Jang
14:30 – 15:00
Session TH3, Composite Design, Historische Maschinenhalle
Feasibility study of structural shielding concepts from space radiation using functional hydrogen-rich composite materials
14:30 – 15:00
Session TH3, Mechanism Testing, Nimes 1
Separation Mechanisms and Ejection Kinematics Verification for Rosalind Franklin Mission
14:30 – 15:00
Session TH3, Design and verification, Nimes 2
A structure for HENON, the first stand-alone Deep Space CubeSat
15:00 – 15:30
Session TH3, Composite Design, Historische Maschinenhalle
Automation-Oriented Structural Analysis of a Large Deployable Reflector Antenna Using OpenSeesPy for Modal Identification and Data-Driven Modelling
15:00 – 15:30
Session TH3, Mechanism Testing, Nimes 1
ExoMars Landing Leg Mechanism Qualification Testing
15:00 – 15:30
Session TH3, Cryogenic, Kasan
Structural supports for optical systems in cryogenic environments
15:00 – 15:30
Session TH3, Design and verification, Nimes 2
Optimized Gas Expansion Tube for Frangible Joint Applications: Design and Verification Approach
15:30 – 16:00
Session TH3, Mechanism Testing, Nimes 1
Qualification of Tape Spring Hinges under Microgravity environment: The TAGES Parabolic Flight Experiment
15:30 – 16:00
Session TH3, Cryogenic, Kasan
Healable composite structures for tank applications and beyond
Bertrand Gresle
(CompPair Technologies Ltd.)
15:30 – 16:00
Session TH3, Design and verification, Nimes 2
CFRP Sandwich Inserts Design, Test & Verification Methods
17:00 – 17:30
Session TH4, Thermal testing, Nimes 1
AUTOMATED THERMAL CYCLING TESTS WITH RADIATIVE TRANSFER UNDER HIGH VACUUM ENVIRONMENT
17:00 – 17:30
Session TH4, Static load test & Test data evaluation, Nimes 2
Static load test of HARMONY spacecraft´s lower compartmen
Luca Marinangeli (OHB System AG)
17:00 – 17:30
Session TH4, Test Predicition and Testing, Historische Maschinenhalle
Recovery of Interface Loads in Shaker Sine Tests without Load Cells or Structural Models
17:30 – 18:00
Session TH4, Thermal testing, Nimes 1
Development of a full-range temperature calibrator for sensors to be used in thermal-vacuum testing for space qualification
17:30 – 18:00
Session TH4, Static load test & Test data evaluation, Nimes 2
Operational Modal Analysis – A robust processing scheme to extract damping properties from measured timeseries
17:30 – 18:00
Session TH4, Test Predicition and Testing, Historische Maschinenhalle
QUASI-STATIC FREQUENCY RESPONSE analysis
18:00 – 18:30
Session TH4, Thermal testing, Nimes 1
A software tool for 3D thermal and dimensional measurement data with solution finding for true surface temperature; integrated with thermos-elastic deformation outputs and export to compare to modelled data.
18:00 – 18:30
Session TH4, Static load test & Test data evaluation, Nimes 2
Static Qualification Test Campaign of the ROSE-L Satellite Structure Subsystem - Innovative Approaches and Results
18:00 – 18:30
Session TH4, Test Predicition and Testing, Historische Maschinenhalle
Vibroacoustic Prediction of the Internal Acoustic Environment in a Launch Vehicle Payload Fairing
18:30 – 20:30
City Bus Tour
This tour will start and end at the Steigenberger Hotel (venue).
08:30 – 09:00
Session F1, Structural dynamics, Nimes 1
Quantifying Vibro-Impact Uncertainty in Lunar Rover Structures: A Comparative Study of Numerical Methodologies within the CHERI Project
08:30 – 09:00
Session F1, Micro vibration, Kasan
Integrated Modelling and Experimental Validation of Reaction Wheel–Induced Micro-Vibrations on Optical Payload Line-of-Sight Stability
08:30 – 09:00
Session F1, Mechanism Testing, Nimes 2
Qualification Testing of the MMX Push-Off Mechanism
08:30 – 09:00
Session F1, Stucture optimaziation, Historische Maschinenhalle
ECSS-Compliant Insert Analysis and Optimization: An Automated Software Approach
09:00 – 09:30
Session F1, Structural dynamics, Nimes 1
Optimally damped nonlinear energy sink to mitigate satellite vibrations.
09:00 – 09:30
Session F1, Micro vibration, Kasan
A comparison of available methodologies for harmonics extrapolation and summation rules in micro-vibration analysis
09:00 – 09:30
Session F1, Mechanism Testing, Nimes 2
Design, analysis and experimental validation of a deployable architecture for very large solar arrays
09:00 – 09:30
Session F1, Stucture optimaziation, Historische Maschinenhalle
Visco-elastic vibration damper design using topology optimization
09:30 – 10:00
Session F1, Structural dynamics, Nimes 1
Compliant structure with integrated passive damping
09:30 – 10:00
Session F1, Micro vibration, Kasan
Launch Vibroacoustic Pressure Differential Across a Thin Space Optical Filter
10:00 – 10:30
Break
10:30 – 11:30
Closing Session
11:30 – 13:00
Networking Lunch and End of Conference
14:00 – 17:00
Guided Tour to the German Aerospace Center in Brunswick
