1U CubeSat Solar Panels Z

29.5% efficiency Space-grade solar cells
Optimal voltage - 4.66 V
Optimal current - 517 mA
Series or parallel connection of multiple panels
High accuracy gyroscope, temp and sun sensors
Loading...Please click to play
Slow connection?
Disable video

1U CubeSat Solar Panels Z

  • 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;
  • Solar cells thickness 150 μm ± 20 μm;
  • Very low solar cell mass (81-89 mg/cm2);
  • High Radiation Resistance;
  • Cover glass;
  • Gyroscope (Optional);
  • Temperature Sensor (Accuracy: ±1.5°C from -25°C to 85°C (max), ±2.0°C from -55°C to 125°C (max));
  • Sun Sensor;
  • Multiple panels can be connected in series or parallel;
  • Plated, countersink mounting holes with ground connection;
  • Connector for external magnetorquer;
  • Optimal Voltage – 4.66V (for 2 cells);
  • Optimal Current – 517mA;
  • Top solar panel weight: 45 g;
  • PCB Thickness 1.6 mm;

Included with 1U Solar Panels Z

Package

Custom box

Engineering Support

5 hours

Tech and User information

USB Drive

Qualification tests

Space qualification tests are performed on the Qualification Engineering Model. Qualification tests level and duration follow the ESA standard ECSS-E-ST-10-03C and GEVS: GSFC-STD-7000A.

Functional Test
Random Vibration
Sinusoidal Vibration
Pyroshock Test

Thermal Cycling
Thermal Vacuum
Total Ionizing Dose

TECHNICAL SPECIFICATIONS

Click on the button below to download the complete technical specifications of the Solar panel Z.

Choose a color

white-solar-panels-button

Solar PanelsWhite

black-solar-panels-button

Solar PanelsBlack

Images

Solar Panel_Z-min
Solar Panel_Z-min
Solar Panel_Z-min
Solar Panel X_Y
Solar Panel X_Y
Solar Panel X_Y
Solar Panel X_Y
Solar Panel X_Y
Solar Panel X_Y
Instagram ProfileYoutube profile