We propose to monitor the bursts from the hyperactive repeating fast radio burst FRB 20240619D over six months using the Murriyang UWL receiver. The primary aim is to study the evolution of burst activity and polarization properties with frequency and time, and to discover any potential periodicity in the burst activity. These insights will enhance our understanding of the progenitor, emission physics, and the immediate magneto-ionic environment of FRB 20240619D, thereby informing the general FRB population. A total of 15 hours of observing between August and November 2024 resulted in over 1300 bursts detected using the UWL receiver. Some bursts exhibit complex spectro-temporal emission patterns. The burst rate, based on Murriyang and MeerKAT observations, indicates that the source was active until September 2nd, after which it became inactive. Given that two other repeating FRBs have exhibited periodic activity cycles, it is reasonable to expect that FRB 20240619D could become active again, making continued monitoring crucial. The UWL receiver's broad frequency coverage and sensitivity are essential for detecting many bursts and enabling simultaneous observations at different frequencies. This is important for understanding the burst activity evolution with time and frequency, spectral properties, and underlying emission mechanisms. The combination of sensitivity and wide bandwidth makes Murriyang the ideal telescope for monitoring this FRB. Results from these observations will be pivotal in understanding FRB 20240619D's place within the broader repeater population and its potential connection to broader FRB progenitor models.

Pioneer 10 plasma analyzer 1 hour data.

The PLASMAG-1 instument package included six different sensors: A0 plasma impact detector for measuring neutral particle flux, (manufactured by R. Grard, ESA/ESTEC, Noordwijk, The Netherlands) A1 Faraday cup for measuring integral ion flux from solar direction, A2 Faraday cup for measuring integral ion flux and neutral particles from ram direction, A3 spherical electrostatic analyzer for measuring ions from ram direction in the energy range of 15 eV - 3.6 keV in 120 logarithmically spaced channels, A4 spherical electrostatic analyzer for measuring ions from solar direction in the energy range of 60 eV - 30 keV in 60 logarithmically spaced channels, A5 cylindrical electrostatic analyzer for measuring ions perpendicular to the ecliptic plane in the energy range of 2 eV - 10 keV in 30 logarithmically spaced channels.

The PLASMAG-1 instument package included six different sensors: A0 plasma impact detector for measuring neutral particle flux, (manufactured by R. Grard, ESA/ESTEC, Noordwijk, The Netherlands) A1 Faraday cup for measuring integral ion flux from solar direction, A2 Faraday cup for measuring integral ion flux and neutral particles from ram direction, A3 spherical electrostatic analyzer for measuring ions from ram direction in the energy range of 15 eV - 3.6 keV in 120 logarithmically spaced channels, A4 spherical electrostatic analyzer for measuring ions from solar direction in the energy range of 60 eV - 30 keV in 60 logarithmically spaced channels, A5 cylindrical electrostatic analyzer for measuring ions perpendicular to the ecliptic plane in the energy range of 2 eV - 10 keV in 30 logarithmically spaced channels.

Pioneer 11 plasma analyzer trajectory data.

The PLASMAG-1 instument package included six different sensors: A0 plasma impact detector for measuring neutral particle flux, (manufactured by R. Grard, ESA/ESTEC, Noordwijk, The Netherlands) A1 Faraday cup for measuring integral ion flux from solar direction, A2 Faraday cup for measuring integral ion flux and neutral particles from ram direction, A3 spherical electrostatic analyzer for measuring ions from ram direction in the energy range of 15 eV - 3.6 keV in 120 logarithmically spaced channels, A4 spherical electrostatic analyzer for measuring ions from solar direction in the energy range of 60 eV - 30 keV in 60 logarithmically spaced channels, A5 cylindrical electrostatic analyzer for measuring ions perpendicular to the ecliptic plane in the energy range of 2 eV - 10 keV in 30 logarithmically spaced channels.

The PLASMAG-1 instument package included six different sensors: A0 plasma impact detector for measuring neutral particle flux, (manufactured by R. Grard, ESA/ESTEC, Noordwijk, The Netherlands) A1 Faraday cup for measuring integral ion flux from solar direction, A2 Faraday cup for measuring integral ion flux and neutral particles from ram direction, A3 spherical electrostatic analyzer for measuring ions from ram direction in the energy range of 15 eV - 3.6 keV in 120 logarithmically spaced channels, A4 spherical electrostatic analyzer for measuring ions from solar direction in the energy range of 60 eV - 30 keV in 60 logarithmically spaced channels, A5 cylindrical electrostatic analyzer for measuring ions perpendicular to the ecliptic plane in the energy range of 2 eV - 10 keV in 30 logarithmically spaced channels.

Pioneer 10 plasma analyzer trajectory data.

 The FWMI prototype development is underway at USU/SDL. To develop the FWMI, USU/SDL is leveraging the successful implementation of a rocket-borne Michelson interferometer/spectrometer system that was designed by USU/SDL in the early 1980s and flown multiple times on sounding rockets. This sensor was designated the Rocket-Borne Field-Widened Interferometer-II (RBFWI-2). Utilizing modern designs, technologies, and components, the new prototype FWMI will significantly enhance the original RBFWI-2 to meet three technical goals: (1) extended spectral coverage, (2) higher spectral resolution, and (3) extended dynamical range. USU/SDL also intends to achieve large reductions in mass, volume, and power. The resultant prototype FWMI will then be a pathfinder for future missions that focus on addressing key scientific objectives and critical supporting science questions in auroral ionosphere-thermosphere energetics.

The successful flight of RBFWI-2 established a solid foundation for the development of the prototype FWMI. Based on that heritage, the current effort focuses on the development of a new optical detector system, a new sensor signal-conditioning system based on modern electronics, as well as extending the displacement of the optics to increase spectral resolution. These new techniques and other modern technologies will be added to the proven RBFWI-2 legacy design to allow the prototype FWMI to serve as the foundation for a flight FWMI version capable of meeting the targeted instrument specifications that are summarized below:

1. Spectral bandpass of 1300-8100 cm-1

2. Spectral resolution of ≤ 1.0 cm-1

3. Dynamic range characterized by a 10-13 W cm-2 sr-1(cm-1)-1 NER.

Pioneer 11 plasma analyzer trajectory data.