VES16 Cell
SaftSpace-qualified D-size 16 Wh lithium-ion cell designed for LEO and GEO satellite applications.
315 satellite platforms, components and ground equipment from manufacturers worldwide.
Space-qualified D-size 16 Wh lithium-ion cell designed for LEO and GEO satellite applications.
Scalable rigid honeycomb-panel solar arrays from 50 W to over 15 kW per wing for LEO, MEO, GEO,…
Airbus offers four product lines of space-qualified Lithium-Ion batteries (ASTRO-BATT, COSMO-BATT, STELLAR-BATT, LAUNCHER-BATT) designed for diverse space missions,…
Airbus offers advanced power conditioning and distribution units (PCDUs) optimized for space applications, ensuring reliable power conversion, regulation,…
A fully qualified, fault-tolerant power supply regulator developed by Airbus Defence and Space for telecom satellites under an…
A compact, end-to-end power processing unit subsystem for satellite electric propulsion, developed for New Space and constellation applications…
The D-SP6X-L-1W is a deployable solar panel with a single wing lateral configuration, compatible with 6U/12U CubeSat structures,…
The SP3X is a solar panel designed for 3U/6U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells…
The PCU-110 by Berlin Space Technologies is a power control unit for small satellites, providing power regulation, switching,…
Blue Canyon Technologies offers flight-proven, high-efficiency solar arrays for various satellite platforms, providing reliable power for onboard systems.
GaAs solar panel with built-in electromagnetic coil for CubeSat side surfaces. 98×82.6 mm, 28% efficiency, 480–520 mA Isc,…
GaAs solar panel with integrated electromagnetic coil for CubeSat top/bottom edges. 98×98 mm, 28% efficiency, 480–520 mA Isc,…
The STARBUCK-NANO is a flight-proven Electrical Power System (EPS) for CubeSats, supporting 2U to 16U missions with features…
High-power power conditioning and distribution unit for deep-space avionics and demanding satellite bus power architectures.
SADA-compatible rigid solar array wing built for ESPA-class electric propulsion smallsat missions, using metallic tape-spring hinges.
The SP8X is a solar panel designed for 8U/16U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells…
The SP6X is a solar panel designed for 6U/12U CubeSat structures, featuring high-efficiency triple-junction UTJ solar cells and…
The SP2X is a solar panel designed for 2U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells…
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