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SPACE LOGISTIX / Space Cargo applications / CONCEPT

The payload defines the solution.

Every payload has its own geometric, environmental and operational requirements. The application matrix suggests a model; final selection requires a complete specification.

Applications. From requirements to workflow.

Select a scenario to explore physical and digital infrastructure roles. This is the ILS development scope, without a claim of operational service availability.

CONCEPT / PLANNED CAPABILITY

Electronics, avionics and sensors

Logistics challenge

Sensitive components pass through multiple suppliers and integration facilities. They require protection against ESD, identification errors and handling damage.

Example cargo

Control boards, sensors, radio modules and satellite subsystems.

Indicative SLX BOX selection

MICRO for individual components; STANDARD for sets with dedicated inserts. Selection depends on actual internal geometry and fixtures.

Environment and integration

ESD protection and humidity, cleanliness and shock control. Transport conditions and insert materials must be agreed with the recipient.

ILS workflow

Parts list → insert design → packing and inspection → ground transport → acceptance at the integration facility.

Role of SLX CONTROL

SLX ID associates serial numbers, component revisions, packing records and handover confirmations.

Limitations and qualification

ESD testing, material compatibility and vibration testing require an engineering plan. Ground transport does not establish flight qualification.

Indicative selection: external dimensions are known. Internal geometry, tare, payload capacity and fixtures require documentation and qualification.

Electronics, avionics and sensors

Control boards, sensors, radio modules and satellite subsystems.

Explore application context ↗

CubeSats and small satellites

An integrated CubeSat, small satellite or set of modules before integration.

Explore application context ↗

Optics and measurement instruments

Cameras, spectrometers, telescope components and precision instruments.

Explore application context ↗

Experiments and biological samples

Experiment cassettes, research materials and sealed sample sets.

Explore application context ↗

Geological materials

Rock, soil and experimental material samples; future lunar samples.

Explore application context ↗

Orbital infrastructure supplies

Equipment, consumables, tools and spare parts.

Explore application context ↗

Robotics and servicing modules

Arms, robotic tools, mechanisms and servicing assemblies.

Explore application context ↗

Power systems and structural components

Power modules, structural segments and technical equipment.

Explore application context ↗

Future lunar infrastructure

Tools, robotic components, equipment and surface demonstrator kits.

Explore application context ↗

Sample and component recovery

Experiment results, samples and components for post-mission analysis.

Explore application context ↗

Ground aerospace logistics

Precision equipment moving between manufacturers, laboratories and integration facilities.

Explore application context ↗

Potential dual-use applications

Sensors, electronics and research equipment with potential civil and defense applications.

Explore application context ↗
INDICATIVE SELECTION

SLX BOX STANDARD

The recommendation indicates a typical application scale, not engineering compatibility. Dimensions, mass, environment, fixtures and recipient requirements may change the model selection.

Explore model ↗

Satellites and avionics

Electronics, sensors and small satellites require ESD protection, vibration control and documented fixtures. MICRO suits small components; STANDARD and HEAVY address larger assemblies after geometry review.

Scientific research

Biological samples, optics and instruments require cleanliness procedures, temperature control and traceability. Inserts and storage conditions must be engineered for each experiment.

Orbital supplies

Equipment, spares and supplies require coordination with the station and cargo vehicle operators. Hatch access and crew procedures are separate requirements from transport beneath a fairing.

Robotics and infrastructure

Robots, power systems and structural components may require HEAVY or consolidated transport. Centre-of-mass, fixture, release and installation access analyses are essential.

Lunar logistics

Lunar delivery requires a transfer vehicle and lander, dust control and unloading provisions. ILS describes a long-term architecture; lunar delivery services are not currently offered.

Return cargo

A return plan covers recovery vehicle integration, sample preservation and post-landing acceptance. Container configuration depends on thermal conditions, shock and safety requirements.

Ground aerospace logistics

A proposed process for precision cargo moving between manufacturers, laboratories and integration facilities. Ground process validation is a separate stage of ILS development.

Dual-use applications

Potential civil and defense applications require separate eligibility, information protection and engineering assessments. No defense certification is claimed.

Concept in development. Parameters, interfaces and applications require documentation, testing and mission-specific approval.

Discuss requirements ↗