Quasi-static structural test of satellites

Autor:	Ozan Oguz Haktanir, Fatih Yilmaz, Ahmet Bilge Uygur
Rok vydání:	2015
Předmět:	Engineering business.industry Emphasis (telecommunications) Phase (waves) Aerodynamics Structural engineering computer.software_genre Vibration Load testing Acceleration Satellite Aerospace engineering business computer Quasistatic process
Zdroj:	2015 7th International Conference on Recent Advances in Space Technologies (RAST).
DOI:	10.1109/rast.2015.7208381
Popis:	Satellites are exposed to simultaneous static and dynamic loads during the launch phase due to launcher acceleration and aerodynamics. Therefore, they are designed and tested to withstand all these loads. From design perspective, a common approach is to combine static and dynamic loads into an equivalent static load which is referred to as quasi-static loads [1]. The validation of the structural design of the satellite is performed by tests and/or analysis. This paper discusses the static load test methods with an emphasis on the acceleration tests performed on vibration test systems.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::120194de41f1d2414a1fbcb3efbc182d https://doi.org/10.1109/rast.2015.7208381 Zobrazit plný text záznamu