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1.
Preventing School Failure ; : 1-5, 2023.
Artículo en Inglés | Web of Science | ID: covidwho-2323642

RESUMEN

School closures resulting from the COVID-19 pandemic have brought the issue of learning loss to the forefront in what has been called the "COVID slide." Data from the pandemic show a decline in student achievement in the areas of reading and mathematics for school districts that shifted to virtual learning platforms. However, it is unclear whether students experienced a loss of learning, or if they progressed at a slower rate while adapting to a new and unfamiliar learning modality. We propose that the latter may be especially true for younger students (i.e. K-3) as well as students with disabilities, who likely required additional support to engage in virtual learning. We offer recommendations as K-12 students return to in-person learning.

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IAF Space Exploration Symposium 2021 at the 72nd International Astronautical Congress, IAC 2021 ; A3, 2021.
Artículo en Inglés | Scopus | ID: covidwho-1782250

RESUMEN

The Astrobotic M1 mission, as the first mission of NASA s Commercial Lunar Payload Services (CLPS) program, is scheduled to land in the Lacus Mortis region of the Moon in early 2022. Among its payloads it will carry the Peregrine Ion Trap Mass Spectrometer (PITMS), an instrument supplied by NASA GSFC that is dedicated to the investigation of the lunar exosphere, and which includes as its core component the ESA-provided Exospheric Mass Spectrometer (EMS). EMS was developed under an ESA contract by an academic/industrial consortium led by Open University (UK) using a fast track development approach that aimed at delivery of a Proto-Flight Model (PFM) instrument with drastically reduced development time. The chosen development approach and the demanding project schedule (18 months from contract start to flight hardware delivery) posed a number of specific project management challenges for successful development of the instrument within the ESA flight hardware development framework and under constraints imposed by the Covid-19 pandemic. With an as-built envelope of HWD of 168 149 127mm, a mass of 1.48kg and a typical power consumption during measurement not exceeding 9.5 Watts the instrument has modest resource requirements. EMS can be re-used in different future application scenarios, including investigations of the lunar exosphere, analysis of gases evolved from acquired samples, and monitoring aspects of the environmental impact of landers and robotic and human activities on the lunar environment. © 2021 International Astronautical Federation, IAF. All rights reserved.

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