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GRBBeta


Visualisation of GRBBeta in orbit

The GRBBeta mission is a 2U Cubesat proof-of-concept mission for a small gamma-ray burst detector and is a follow on from GRBAlpha. It was launched on July 9, 2024 on an Ariane 6 rocket from the Kourou Spaceport in French Guiana. The satellite weighs 2.26 kg and is 10 x 10 x 22.7 cm in size. GRBBeta is an international collabration between various research institutions, including the Konkoly Observatory (Hungary), Technical University of Košice (Slovakia), Masaryk University (Czech Republic), and Hiroshima University (Japan). Primary funding was provided by the Ministry of Education, Research, Development and Youth of the Slovak Republic.

It is a proving ground for the future “Cubesats Applied for Measuring and Localising Transients” (CAMELOT), a planned constellation of 3U Cubesats to provide continuous all-sky coverage and accurate localization. GRBBeta carries the same undersized (1/8 size: 75 x 75 x 5 mm) version of the detectors intended for CAMELOT: sufficient to demonstrate the mission concept and intercalibrate observed light curves with existing operational GRB missions. It differs from GRBAlpha in carrying some new subsystems, such as an advanced positioning module and Iridium satellite communications network through deployed antennae. The mission also has a secondary science payload named LuvCAM, a miniature UV camera for astrophysics. It is primarily an instrumentation testbed to track degradation of the imaging chip in the space environment

Mission Characteristics

* Lifetime :9 July 2024 with one year nominal mission.

* Energy Range : 30–900 keV

* Special Features : 2U Cubesat configuration for ridesharing launch.
1/8th effective area design to prove CAMELOT mission concept.
Follow on of successful GRBAlpha with new subsystems.

* Payload :

  • Gamma-ray Detector. A single CsI(Tl) crystal measuring 75 x 75 x 5 mm. The scintillation is observed by low voltage lightweight silicon photomultipliers. The detector is covered with a dark polyvinyl fluoride (tedlar) film in 1 mm aluminium sheet box mounted on the exterior surface of the satellite.

* Science Highlights:

  • Charactization of peak intensity and time of bright burst events;
  • Prove operational concepts of future CAMELOT satellite constellation, especially supporting sub-systems;
  • Co-observe with gravitational wave detectors and other observatories as part of multimessenger astronomy.