Space Solar Cells & CIC Assemblies
Triple-junction GaAs cells and cell-interconnect-coverglass assemblies for array integration.
View detailsSpace Power Solutions for Small Satellites & Spacecraft
From triple-junction GaAs cells and CIC assemblies to satellite panels and project-specific deployable solar arrays.
Space Power Products
Satellite Solar Panels
Fixed, body-mounted and custom panels, with electrical layout and installation interfaces reviewed for your platform.
View detailsDeployable Solar Arrays
Discuss single-wing, dual-wing, multi-wing and multi-panel configurations against your mission requirements.
FULLSUNS configuration guide | Configuration Example
View details
Flexible GaAs for Space
4080 | 40 × 80 mm | space application configuration. Request model-specific electrical data, integration guidance and applicable test information.
Flexible GaAs technical reference.
View detailsFrom Cell to Array
GaAs Cell
Select the model against mission electrical and environmental requirements.
CIC
Cell, interconnect and coverglass configuration for array integration.
Solar Panel
Define cell layout, strings, substrate, harness and mounting interfaces.
Deployable Array
Evaluate single-wing, dual-wing, multi-wing or folding concepts.
Spacecraft Interface
Close the mechanical, electrical, stowed-envelope and verification interfaces.
Supply scope is defined project by project.
Power for Higher-Demand Space Payloads
Emerging spacecraft payloads such as high-rate communications, optical inter-satellite links, Earth observation and onboard processing can increase spacecraft power demand. FULLSUNS evaluates GaAs cell, CIC, panel and deployable-array configurations against available area, mass, voltage, stowed envelope and mission requirements.
Start with Your Mission Power Budget
- Orbit / mission
- Required BOL power
- Required EOL power
- Bus / MPPT voltage
- Available mounting area
- Maximum array mass
- Stowed envelope
- Mission lifetime
- Deployment configuration
- Radiation / environmental requirements
- Qualification expectation
These are engineering inputs for project review. Output at beginning and end of life is assessed under agreed mission conditions.
Engineering Verification & Qualification Support
Electrical
I–V, AM0 and temperature-dependent evaluation where applicable.
Radiation
Electron / proton testing where required by the project.
Mechanical
Vibration, shock and deployment verification where applicable.
Environment
Thermal-vacuum and thermal-cycling requirements by project.
Acceptance
Agreed project test plan, criteria and documentation.
Test scope, facility and acceptance criteria are defined per project. External accredited facilities may be used where required. Website descriptions do not establish qualification or flight heritage.
Existing Model Details
Cell model details
Panel model details
Technical documents
Available datasheet
30% triple-junction GaAs solar cell reference data. Electrical values are model-specific and subject to stated test conditions.
Download datasheet (PDF)Project documentation
Request configuration-specific drawings, an interface control document (ICD) and applicable test documentation. Availability and deliverables are agreed during technical review.
Request a Technical ProposalExport & End-Use Review
Availability of certain products, configurations or technical data may be subject to applicable export-control, end-use and destination review.
Request a Technical Proposal
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