Space

Sonaca’s core business consists of design, development, manufacturing, assembly, testing and qualification of space flight structures thermal systems and MGSE. It is actively involved in space applications since three decades, covering mainly satellite platforms, payloads and launchers.

Structures

Design, development, manufacturing, assembly and testing aerospace structures and their associated systems.

Satellite platform

State-of-the-art and advanced structural solutions for satellites platforms, from nano- and micro satellites to large satellites (6+ meters), from design to delivery

Characteristics:
- Sandwich panels structures
- Metallic and composite
- Full metallic structures (Isogrid) for small satellites and constellations
Launchers and space vehicles

Large experience in design, development and manufacture of structures for launchers structures, re-entry vehicles, crew vehicles or space station

Characteristics:
- Complex metallic machined structures
- Composite structures
- 3D Orthogonal weaving for space launchers (Composite - RTM)
- Large sizes
Instruments structures

Experience in design, development and manufacture of structures for large instruments. Including: optical benches, bipods, cylinder baffles or secondary and tertiary components

Characteristics:
- CFRP Sandwich panels complex shape for optical benches
- Cylinder CRFP structures
- Metallic structures for cylinder baffles (thin milling and chemical milling)
Static tests

Custom test services to meet specific customer challenges, conducted to international standards

Characteristics:
- Certified and experienced experts team members
- International Standards and ECSS compliant tests
- Large scale fully adaptable set-ups
- Materials, structural and thermal tests complete portfolio

Thermal systems

Ground support equipment & test services for satellites, instruments, launchers and their components.

Thermal control systems

Design, development and delivery of complete thermal control systems, applications for landers, instruments and satellites

Characteristics:
- Conceptual design and development of special solution (switching heat pipes, thermoelectric cooling…)
- Thermal architecture (from phase A to E) and analysis (ESATAN, Thermica, Thermal desktop)
- Hardware selection and procurement or manufacturing (MLI)
- Assembly and integration (ISO 8), testing and qualification
Thermal hardware

Single-stop provider for all thermal hardware needs for a space system, can be either produced in-house or procured by a series of globally-distributed vendors

Products:
- Radiators with embedded heat pipes (conventional, switching), metallic and composite
- SLI and MLI
- Thermal straps
- OSR
- Heaters
- Thermometers, thermostats, heat capacitors
- Advanced thermal technologies
Thermal tests and qualification

Thermal testing and qualification according to ECSS and NASA standards, in vacuum and ambient pressure, up to cryogenic conditions

Characteristics:
- MTVAC, Medium Thermal Vacuum Chamber, high vacuum tests (p <10-6 mbar) (air or CO2/N2 atmosphere), 50x50x50cm³, configurable
- Thermally controlled shroud with Liquid nitrogen/heater system (-190°C, 200°C)
- Thermally controlled cold plate (-70°C/+150°C), with LN2 cooling (optional (-190°C, 200°C)
- Cryogenic thermal chamber (-135°C, 135°C) with purging capabilities, for life cycle tests
- Support to testing in external facilities, including test plans, procedures, predictions, correlation
- Test management activities, with on and off-site support of experienced test engineers

GSE & AIT

Design, development, manufacturing, assembly and testing of thermal systems and their associated systems and components, with a 15-years strong thermal analysis background.

Transport containers

Transport and storage container for flight hardware and sensitive equipment , available in a variety of sizes and configurations (e.g. for satellites, systems, instruments, with active controls or fully passive)

Characteristics:
- Robust and lightweight body with modular elements construction (easy and economic to adapt to various dimensions)
- Shock/vibration absorption system, GN2 purging, equalization and relief system
- Integrated closed circuit environmental control system and environmental monitoring (e.g. pressure, temperature, humidity, acceleration)
- Active Thermal Control (optional)
- Full ECSS- or industrial-level documentation
Handling MGSE

Lifting, handling and assembly Ground Support Equipment, for sizes ranging to small satellites and Equipment to fully loaded satellites

Characteristics:
- Lifting devices for complete satellites, for weights up to 7000 kg, with full ECSS verification
- Handling devices for small satellites, with an excellent price/quality ratio
- Tooling for production of launcher parts and for assembly of complete satellites
GSE instruments

Design, development and realization of testing and calibration of ground support equipment for scientific instruments

Characteristics:
- Thermally controlled enclosures
- Calibration targets
- Ad-hoc dedicated software
- Monitoring and control systems
- Including Vacuum, pneumatic, cryogenic and/or fluidic systems
- Compatible with clean room operations
- With tailorable documentation level, from scientific development level up to full ECSS-level (e.g. for Qualification and Ground Reference activities)

Instruments & Mechanisms

Industrial prime for the realization of bespoke scientific instruments and mechanisms for exploration and observation missions. The Sonaca group can provide support in project management, engineering, realization and qualification of instrumentation and mechanisms.

Scientific instruments

Industrial support to scientific institutions for the development, industrialization, production and qualification of scientific instruments in different domains: in situ planetary exploration (Mars, Moon, asteroids…), Earth observation or Solar system exploration

Characteristics:
- Project management support
- Technical coordination
- Systems engineering
- AIT (Assembly Integration and Testing)
- Mechanical and thermal engineering
- Product and Quality Assurance
- Configuration management on the instrument and its subsystems
ISS instruments

Development of experiments for use on the International Space Station. Engineering, project Management and MAIT support up to launch and operations, with a vast network of suppliers and partners

Characteristics:
- Development of full functional 3D printer breadboard capable to print with PEEK polymer
- Printer fulfills the majority of ISS safety requirement
- Printer is qualified for parabolic flight experiment
- Printer is capable of printing with inverted g vector (upside down) simulating zero g environment
- Functional parts printed are showing good functional performance and mechanical properties