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Details
- Project's acronym:
- HEDGEHOG
- Financial Program Name:
- INNY
- Organization:
- Ministerstwo Nauki i Szkolnictwa Wyższego (MNiSW)
- Agreement:
- z dnia 2019-05-14
- Realisation period:
- 2018-06-01 - 2020-09-30
- Project manager:
- Adam Dąbrowski
- Team members:
-
- leader dr inż. Adam Dąbrowski
- member Jacek Goczkowski
- member Karol Pelzner
- member Szymon Rafał Krawczuk
- member Agnieszka Elwertowska
- Realised in:
- Department of Mechanics and Mechatronics
- Request type:
- Different
- Domestic:
- Domestic project
- Verified by:
- Gdańsk University of Technology
Papers associated with that project
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total: 4
Catalog Projects
Year 2020
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Preliminary results from HEDGEHOG REXUS project – A sounding rocket experiment on accelerations, vibrations and heat flow
PublicationDuring 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...
Year 2019
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Preliminary results from HEDGEHOG REXUS Project - sounding rocket experiment on accelerations, vibrations and heat flow
PublicationAs access to space conditions becomes more available, both technically and economically, scientists' interest in launching finer and more sophisticated experiments grows. This applies now more than ever to fragile by nature biological and chemical experiments. To be qualified for launch, such experiments need to be carefully tested prior to the event. The tests should represent actual launch conditions as closely and in as detailed...
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Projekt urządzenia do odtwarzania warunków panujących w rakiecie kosmicznej
PublicationElementy wynoszone w przestrzeń kosmiczną rakietami są poddawane wymagającym warunkom takim jak przyspieszenia, drgania, przepływ ciepła, próżnia. Zanim ładunek, np. satelita zostanie zakwalifikowany do lotu, musi przejść szereg testów, które zweryfikują jego zdolność do przetrwania procesu wyniesienia. Wadą typowych testów jest oddzielne symulowanie reżimów: dynamicznego, termicznego i próżniowego, przez co warunki panujące podczas...
Year 2018
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Introducing concurrent engineering to space and satellite technology undergraduate course
PublicationIn recent decade concurrent engineering has become a de facto leading methodology of work in space, aeronautics and sometimes even automotive industry. It has been used in designing ESA space missions for 20 years now, with rst Concurrent Design Facility (CDF) built in ESTEC in 1998. Still, it has not become a universal standard in engineering, and universities are specically reluctant to adopt it into their curricula. As a result,...
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