Alfonso-Corcuera Daniel, Ogueta-Gutiérrez Mikel, Fernández-Soler Alejandro, González-Bárcena David, Pindado Santiago
Instituto Universitario de Microgravedad "Ignacio Da Riva" (IDR/UPM), ETSI Aeronáutica y del Espacio, Universidad Politécnica de Madrid, Plaza. del Cardenal Cisneros 3, 28040 Madrid, Spain.
Sensors (Basel). 2022 Jul 26;22(15):5575. doi: 10.3390/s22155575.
This paper shows wind speed measurements from the TASEC-Lab experiment in a stratospheric balloon mission. The mission was launched in July 2021 from León (Spain) aerodrome. Measurements of horizontal wind speed in relation to the balloon gondola were successfully carried out with a cup anemometer. According to the available literature, this is the first time a cup anemometer has been used in a stratospheric balloon mission. The results indicate the need to consider the horizontal wind speed from the balloon ascent phase for thermal calculations of the mission.
本文展示了平流层气球任务中TASEC实验室实验的风速测量结果。该任务于2021年7月从西班牙莱昂机场发射。使用杯式风速计成功地进行了与气球吊篮相关的水平风速测量。根据现有文献,这是杯式风速计首次用于平流层气球任务。结果表明,在任务的热计算中需要考虑气球上升阶段的水平风速。