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HiakaSat (HawaiiSat 1)

HiakaSat [University of Hawaii]

HiakaSat (Hyperspectral Imaging, Aeronautical Kinematic Analysis Satellite), also known as HawaiiSat 1, is a microsat mission developed by students of the University of Hawaii, Honolulu (Ma-noa).

The mission has following goals:

  • Demonstrate a cost effective on-orbit platform for performing technology demonstrations
  • Perform remote sensing with the newly designed space ultra-compact hyper-spectral imager (SUCHI)
  • Perform imaging with two HSFL color cameras which are co-aligned with SUCHI
  • Provide workforce development opportunities for students and recent graduates
  • Further develop infrastructure for sustainable satellite development, integration and test, and operations

Originally the HawaiiSat 1 mission was to be built on a larger bus and was to feature the THI (Thermal Hyperspectral Imager) payload. It was to weight 80 kg. Later during development, the available mass was cut to 40 kg, later raised again to 55 kg. Therefore the HawaiiSat 1 structure was cut in half and the THI payload was replaced by the light weight SUCHI. This redesigned satellite was renamed HiakaSat.

HiakaSat was launched as the prime payload of the ORS-4 mission in November 2015 on the new low-cost Super-Strypi launch vehicle from Kauai, but was lost in a launch failure.

Nation: USA
Type / Application: Vehicle evaluation, Earth observation
Operator: University of Hawaii, Hawai`i Space Flight Laboratory, Honolulu
Contractors: University of Hawaii, Hawai`i Space Flight Laboratory, Honolulu
Equipment: SUCHI
Configuration: HawaiiSat bus
Propulsion: None
Power: Solar cells, batteries
Lifetime: 1-2 year
Mass: 55 kg
Orbit: 415 km × 490 km, 94.7 (planned)
Satellite COSPAR Date LS Launch Vehicle Remarks
HiakaSat (HawaiiSat 1) 2015-F03 04.11.2015 Kau LP-41 F Super-Strypi with Supernova-Beta, STACEM, Argus, EDSN 1, EDSN 2, EDSN 3, EDSN 4, EDSN 5, EDSN 6, EDSN 7, EDSN 8, PrintSat

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