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TRSI-Sat (TRSI 1), TRSI 2, 3

TRSI-Sat [My Radar]

TRSI-Sat or TRSI 1 is a picosatellite developed by ACME AtronOmatic (MyRadar) to the 1P PocketQube form factor.

TRSI-Sat features two experiments:

  • First is a waterfall experiment which will show an image in the waterfall diagram by hopping the frequency within its transmission band (image-type beacon). The experiment will try out correlation algorithms on this signal to find out if it can be detected under weak signal conditions.
  • The second experiment is to analyze RF reception capabilities from LEO with a novel detector receiver and a small patch antenna. It was designed to test if small satellite receivers which don´t need deployable antennas are feasible.

The satellite was launched on 6 December 2019 together with other PocketQubes and other satellites on an Electron KS launch vehicle.

Nation: Germany
Type / Application: Technology
Operator: ACME AtronOmatic (MyRadar)
Contractors: ACME AtronOmatic (MyRadar)
Equipment:
Configuration: PocketQube (1P)
Propulsion: None
Power: Solar cells, batteries
Lifetime:
Mass: 0.2 kg
Orbit:
Satellite COSPAR Date LS Launch Vehicle Remarks
TRSI-Sat (TRSI 1) 2019-084H 06.12.2019 OnS LC-1A Electron KS with ALE 2, NOOR 1A, NOOR 1B, ATL 1, FossaSat 1, SMOG-P
TRSI 2 2022-047 02.05.2022 OnS LC-1A Electron KS (R) with E-Space Demo 1, 2, 3, BRO 6, AuroraSat 1, SpaceBEE 140, ..., 155, SpaceBEENZ 15, ..., 22, Unicorn 2, MyRadar 1, TRSI 3, Copia
TRSI 3 2022-047 02.05.2022 OnS LC-1A Electron KS (R) with E-Space Demo 1, 2, 3, BRO 6, AuroraSat 1, SpaceBEE 140, ..., 155, SpaceBEENZ 15, ..., 22, Unicorn 2, MyRadar 1, TRSI 2, Copia

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