1U Solar Panel - Endurosat
EnduroSat
- Efficiency:
- 29.5 %
- Solar Cell Thickness:
- 150 μm ± 20 μm
- Solar Cell Mass:
- 81-89 mg/cm^2
- Temperature Sensor Accuracy:
- (±1.5°C from -25°C to 85°C) ; (±2.0°C from -55°C to 125°C)
- Voltage:
- 16.31 V (Optimal for 7 cells)
- Current:
- 517 mA (Optimal for 7 cells)
- PCB Thickness:
- 1.6 mm
- Mass:
- 127g (155g with MTQ); (<300 g for Deployable variant)
- Efficiency 29.5%
- Triple Junction Solar Cells InGaP/GaAs/Ge for Space Applications
- Internal By-pass diode for reverse bias protection
- Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
- High Radiation Resistance
- Multiple panels can be connected in series or parallel
- Plated, countersink mounting holes with ground connection
- Available with integrated magnetorquer (MTQ)
- Deployable Stowed configuration thickness: 6.2 mm
- Deployable Hinge: Short side, 90 degrees
- Dual burnwire deployment mechanism
- Deployable array includes: 1 Fixed panel + 1 Deployable panel
- Cover glass
- Sun Sensor
- Gyroscope (optional)
- Connector for external magnetorquer
- Plated, countersink mounting holes with ground connection
- Packed in a custom box
- 5 hours of engineering support
- Full warranty
- Technical information (Datasheet)
EnduroSat's 3U Solar Panels utilize seven highly efficient triple junction solar cells. The variant 3U Deployable Solar Array utilizes fourteen highly efficient triple junction solar cells arranged into 1 fixed + 1 deployable panels. The deployable solar array doubles the energy generation capability of your satellite.
The 3U Solar Panels support multiple integrated sensors and it are fully compliant with the CubeSat standard. The high power generation capabilities, radiation and temperature resilience ensure smooth space operations.
Features:
Includes:
Qualification:
Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.
3U Solar Panel - Endurosat
EnduroSatEnduroSat's 3U Solar Panels utilize seven highly efficient triple junction solar cells. The variant 3U Deployable Solar Array utilizes fourteen highly efficient triple junction solar cells arranged into 1 fixed + 1 deployable panels. The deployable solar array doubles the energy generation capability of your satellite.
The 3U Solar Panels support multiple integrated sensors and it are fully compliant with the CubeSat standard. The high power generation capabilities, radiation and temperature resilience ensure smooth space operations.
Features:
- Efficiency 29.5%
- Triple Junction Solar Cells InGaP/GaAs/Ge for Space Applications
- Internal By-pass diode for reverse bias protection
- Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
- High Radiation Resistance
- Multiple panels can be connected in series or parallel
- Plated, countersink mounting holes with ground connection
- Available with integrated magnetorquer (MTQ)
- Deployable Stowed configuration thickness: 6.2 mm
- Deployable Hinge: Short side, 90 degrees
- Dual burnwire deployment mechanism
- Deployable array includes: 1 Fixed panel + 1 Deployable panel
Includes:
- Cover glass
- Sun Sensor
- Gyroscope (optional)
- Connector for external magnetorquer
- Plated, countersink mounting holes with ground connection
- Packed in a custom box
- 5 hours of engineering support
- Full warranty
- Technical information (Datasheet)
Qualification:
Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.
- Efficiency:
- 29.5 %
- Solar Cell Thickness:
- 150 μm ± 20 μm
- Solar Cell Mass:
- 81-89 mg/cm^2
- Temperature Sensor Accuracy:
- (±1.5°C from -25°C to 85°C) ; (±2.0°C from -55°C to 125°C)
- Voltage:
- 16.31 V (Optimal for 7 cells)
- Current:
- 517 mA (Optimal for 7 cells)
- PCB Thickness:
- 1.6 mm
- Mass:
- 127g (155g with MTQ); (<300 g for Deployable variant)
- Efficiency 29.5%
- Triple Junction Solar Cells InGaP/GaAs/Ge for Space Applications
- Internal By-pass diode for reverse bias protection
- Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
- High Radiation Resistance
- Multiple panels can be connected in series or parallel
- Plated, countersink mounting holes with ground connection
- Available with integrated magnetorquer (MTQ)
- Deployable Stowed configuration thickness: 6.2 mm
- Deployable Hinge: Short side, 90 degrees
- Dual burnwire deployment mechanism
- Deployable array includes: 1 Fixed panel + 1 Deployable panel
- Cover glass
- Sun Sensor
- Gyroscope (optional)
- Connector for external magnetorquer
- Plated, countersink mounting holes with ground connection
- Packed in a custom box
- 5 hours of engineering support
- Full warranty
- Technical information (Datasheet)
EnduroSat's 3U Solar Panels utilize seven highly efficient triple junction solar cells. The variant 3U Deployable Solar Array utilizes fourteen highly efficient triple junction solar cells arranged into 1 fixed + 1 deployable panels. The deployable solar array doubles the energy generation capability of your satellite.
The 3U Solar Panels support multiple integrated sensors and it are fully compliant with the CubeSat standard. The high power generation capabilities, radiation and temperature resilience ensure smooth space operations.
Features:
Includes:
Qualification:
Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
Space qualification tests are performed on the Qualification Engineering Model. Qualification test levels and duration will follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.
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