Wyszukiwarka
ISSN:
eISSN:
Dyscypliny:
- automatyka, elektronika, elektrotechnika i technologie kosmiczne (Dziedzina nauk inżynieryjno-technicznych)
- astronomia (Dziedzina nauk ścisłych i przyrodniczych)
Punkty Ministerialne: Pomoc
| Rok | Punkty | Lista |
|---|---|---|
| Rok 2024 | 140 | Ministerialna lista czasopism punktowanych 2024 |
| Rok | Punkty | Lista |
|---|---|---|
| 2024 | 140 | Ministerialna lista czasopism punktowanych 2024 |
| 2023 | 140 | Lista ministerialna czasopism punktowanych 2023 |
| 2022 | 140 | Lista ministerialna czasopism punktowanych (2019-2022) |
| 2021 | 140 | Lista ministerialna czasopism punktowanych (2019-2022) |
| 2020 | 140 | Lista ministerialna czasopism punktowanych (2019-2022) |
| 2019 | 140 | Lista ministerialna czasopism punktowanych (2019-2022) |
| 2018 | 35 | A |
| 2017 | 35 | A |
| 2016 | 35 | A |
| 2015 | 35 | A |
| 2014 | 25 | A |
| 2013 | 25 | A |
| 2012 | 25 | A |
| 2011 | 25 | A |
| 2010 | 20 | A |
Model czasopisma:
Punkty CiteScore:
| Rok | Punkty |
|---|---|
| Rok 2022 | 6.3 |
| Rok | Punkty |
|---|---|
| 2022 | 6.3 |
| 2021 | 5.7 |
| 2020 | 5.4 |
| 2019 | 5.1 |
| 2018 | 4.4 |
| 2017 | 3.8 |
| 2016 | 3.4 |
| 2015 | 2.7 |
| 2014 | 2.7 |
| 2013 | 2.5 |
| 2012 | 2.1 |
| 2011 | 1.6 |
Impact Factor:
Sherpa Romeo:
Prace opublikowane w tym czasopiśmie
Filtry
wszystkich: 2
Katalog Czasopism
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Mechanical simulation of artificial gravity in torus-shaped and cylindrical spacecraft
PublikacjaLarge deformations and stress analyses in two types of space structures that are intended for people to live in space have been studied in this research. The structure under analysis is assumed to rotate around the central axis to create artificial gravitational acceleration equal to the gravity on the Earth's surface. The analysis is fully dynamic, which is formulated based on the energy method by using the first-order shear deformation...
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Preliminary results from HEDGEHOG REXUS project – A sounding rocket experiment on accelerations, vibrations and heat flow
PublikacjaDuring flight, a sounding rocket is subject to a unique environment - severe vibrations and substantial heat flux. In order to design payloads, precise measurement of these conditions is required. This paper presents preliminary results from HEDGEHOG REXUS Project, whose scientific goal was to characterise the thermal and dynamic environment of REXUS sounding rockets. For this purpose, two new sensors have been designed - mechanical...
wyświetlono 670 razy