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A year in orbit: ISS deployment tests radiation detectors for future space missions
The predawn darkness on a cool Florida night was shattered by the ignition of nine Merlin engines on a SpaceX Falcon 9 rocket. The thrust of the engines shook the ground miles away. From a distance, the rocket appeared to slowly rise above the horizon. For the cargo onboard, the launch was anything but gentle, as the ignition of liquid oxygen generated more than 1.5 million pounds of force. After the rocket had been out of sight for several minutes, the booster dramatically returned to Earth with several sonic booms in a captivating show of engineering designed to make space travel less expensive and more sustainable.
Ao Zhang, Li Chen, Chunlei Wang, Jingmin Li
Nuclear Technology | Volume 211 | Number 8 | August 2025 | Pages 1809-1822
Research Article | doi.org/10.1080/00295450.2024.2430124
Articles are hosted by Taylor and Francis Online.
Micro nuclear batteries are primarily designed to provide long-term, stable power supplies for microdevices operating in extreme environments. Currently, increasing the power output of nuclear batteries is essential for their broader application. This study investigates the output characteristics of the gallium nitride (GaN)-based PIN junction betavoltaic battery powered by 147Pm radioactive sources. Based on Monte Carlo (Geant4) and technology computer-aided design (TCAD), we calculate the J-V characteristics of the betavoltaic battery under various radioactive source and transducer structural parameters. Notably, we analyze the impact of traps in the GaN on the battery output.
The results indicate that when the 147Pm source thickness approaches 10 μm, the surface power output density nearly reaches its maximum. Under irradiation from a source of this thickness, and without considering transducer traps, the device achieves a maximum output power density Pmax of 35.68 ± 0.3 μW/cm2 and a device energy conversion efficiency ηd of 6.69% ± 0.06%, significantly surpassing the output of 63Ni-based cells. Considering transducer traps, Pmax decreases to 22.81 μW/cm2. The acceptor trap H1 (energy level: Ev + 0.86 to 0.88) formed during the growth process is found to be the primary factor reducing battery performance.