/

Payload

The HUNITY satellite carries multiple scientific payloads and experiments to conduct research and demonstrate new technologies in space.

Győr Széchenyi István University SZESAT team

The SZESAT is a satellite within the NMHH-1 mission, developed by Széchenyi István University of Győr, featuring advanced technological demonstrations and experiments.

  • Satellite within HUNITY
  • Technological demonstration
  • Laser communication experiment
  • Orientation detection with semiconductor sensor

More information:

Visit SZESAT Website
SZESAT satellite boards

High School Experiments

The HUNITY satellite features experiments designed by high school students, providing educational opportunities and fostering interest in space technology among younger generations.

Capysat

Light spectrum measurement with a semiconductor-based sensor (350-988 nm)

Capysat PCB design

Celeritas

Measurement of gamma rays using a semiconductor sensor

Celeritas PCB design

Kulinsat

Investigation of radiation immunity of semiconductor memories (RAM, FLASH

Kulinsat PCB design

Onionsat

Radiation measurement (artificial) based on variation of specific gel resistance

Onionsat PCB design

Seat

Orientation sensing with 6-axis MEMS and light sensor

Seat PCB design

Seraph

Temperature transient measurement (with different coloured thermocouple coatings)

Seraph PCB design

Futher Experiments

The HUNITY satellite includes additional 40x30 mm form factor scientific experiments and technological demonstrations.

CSPD

Temperature transient measurement

CSPD PCB design

spASIC

Testing ASIC module in space.

spASIC PCB design

WLR

Testing WLR089 module in space.

WLR PCB design

CAM

Selfie camera

CAM PCB design

Other Experiments

The HUNITY satellite includes additional scientific experiments and technological demonstrations to advance our understanding of space environments and test new capabilities

Rotating Mass Principle Orientation Control

Payload #1

Active Magnetic Orientation Control

Payload #2

GPS Satellite Identification

Payload #3

Earth horizon and Sun Camera (ELKH CSFK)

Payload #5

Ionizing Dosimetry (27G)

Payload #6

Solar Panel Lifetime Study

Payload #9

Orientation Determination with MEMS Sensors

Payload #10

Serbian Experiment

Payload #11

Solar Panel Wings

Payload #12
Back to Home