Space Structures GmbH. Your competent partner for mechanical subsystems for space application. FEM Analysis (NASTRAN, ANSYS), Thermal Analysis (ESAtan, Thermica), CAD Design (SOLIDWORKS), Fracture Control (NASGRO), Vibro-Acoustic Analysis (VA One), Optimisation (Optistruct). We consult you from the first draft until the manufactured and tested product. Profit from our vast experience with Prime and Subcontractors, Spacecraft Operators and Launch Service Providers.

Space Structures GmbH . Mechanical Subsystems for Space Application

We are hiring engineers, innovators, project managers and more!

Discover current job vacancies!

Certified according to EN 9100:2018 and ISO 9001:2015 Quality Management System standards.

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Quality Management System

2D and 3D CAD model building

Parametric models

Multibody simulations (pure kinematic and dynamic)

- Design for manufacturing - also for additive manufacturing methods
- Design to cost and/or schedule
- Design for functionality
- Surface treatments
- following assembly and inspection processes
- Design rules for structures that astronauts will interact with

Consideration of all relevant constraints & boundary conditions

All relevant drawings including manufacturing and assembly drawings

Interface Control Documents (ICD)

DML, DPL

Assembly procedures

Data exchange with manufacturers and customers in all relevant data formats

Our offer includes**:**

ECSS-E-ST-30 standards series

ECSS-E-HB-32 handbook series

NASA-STD-5000 standards series

ECSS-Q-ST-70C standard

Standards and processes followed**:**

Dassault Systèmes Solidworks®

The tools that we use**:**

Would you like to know more about this **service?**

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Space Structures GmbH has designed and manufactured rideshare multi-payload adapters for SpaceX Transporter Missions 1 to 7. 
More than 100 satellites have been launched on our LVA family.

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Rideshare Payload Adapters 

Leading a German-Romanian SME consortium, Space Structures GmbH is responsible for the development of the internal secondary structures for the International Habitation Module (IHAB). 

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Lunar Gateway

Internal Secondary Structures

I-HAB Habitation Module

CMMU MMS

Electronic units

CAD Design

Any space mission is a complex system and requires according system engineering know-how.

Space System Engineering

Our extensive design know-how and experience helps designing complex parts and assemblies for extreme applications.

Lightweight structures for space applications with their complex details often require more than a standard analysis.
This is where our special structural engineering know-how comes in.

Structure Engineering

Our team has extensive expertise in providing fatigue and fracture control for a wide variety of projects ranging from small satellites, pressurised life support systems on the ISS to secondary structures of the Orion European service module.


Fatigue & Fracture Control

Extreme temperatures and vacuum make thermal control in space a huge challenge.

Thermal Engineering

What is the most severe environment for a spacecraft? The tests! Because of additional margins to ensure the flight environments are covered.

Test Engineering

Craig-Bampton Model Condensation and Coupled Load Analysis (CLA) are essential steps to verify a spacecraft is compatible with launching on a particular launcher.

Model Condensation & Coupled Load Analysis (CLA)

Helping you navigate **decisions**

We provide deep subject matter expertise over the **space project Phases B2, C & D**

We approach each mission individually, selecting optimized solutions, that will be best suited for the specification and your business needs.

Optimised solutions

Our strategy is to always employ the best manufacturing technology for the given design task.

Best technologies

We deliver goals within the given constraints by breaking down the work into clearly defined work packages that come from the overall project plan.

CAD Design

Custom automated post-processing routines for certain CAD process steps allow efficiency and a smooth workflow.

Our offer includes:

Standards and processes followed: