TY - GEN
T1 - Ground based test verification of a nonlinear vibration isolation system for cryocoolers of the soft X-ray spectrometer (SXS) onboard ASTRO-H (Hitomi)
AU - Allen, Bradley
AU - Borst, Catherine
AU - Kidney, Scott
AU - Mimovich, Mark
AU - Paavola, Chris
AU - Pargett, Timothy
AU - Wilke, Paul
AU - Smith, Christian
AU - Ishimura, Kosei
AU - Takei, Yoh
AU - Yasuda, Susumu
PY - 2017/6/7
Y1 - 2017/6/7
N2 - Inherently nonlinear vibration isolation systems offer compelling analytical performance advantages over their linear alternates. Verification testing followed by post-test correlation is essential to convincing otherwise conservative project management teams to adopt these technologies for their mission. This paper details a comprehensive test verification program developed and executed for a novel vibration isolation system developed for the Soft X-ray Spectrometer (SXS) onboard ASTRO-H (named Hitomi after launch). More specifically, the dual-stage / thermally conductive / nonlinear vibration isolation system developed for on-orbit amelioration of cryocooler-induced mechanical vibration, needed to undergo ground testing to demonstrate both on-orbit performance and launch induced response level rejection to protect sensitive payload temperature control components. The system, referred to as the VIS, realizes both small signal transmissibility at high frequency and small acceleration and displacement against vibration during launch and ground testing.
AB - Inherently nonlinear vibration isolation systems offer compelling analytical performance advantages over their linear alternates. Verification testing followed by post-test correlation is essential to convincing otherwise conservative project management teams to adopt these technologies for their mission. This paper details a comprehensive test verification program developed and executed for a novel vibration isolation system developed for the Soft X-ray Spectrometer (SXS) onboard ASTRO-H (named Hitomi after launch). More specifically, the dual-stage / thermally conductive / nonlinear vibration isolation system developed for on-orbit amelioration of cryocooler-induced mechanical vibration, needed to undergo ground testing to demonstrate both on-orbit performance and launch induced response level rejection to protect sensitive payload temperature control components. The system, referred to as the VIS, realizes both small signal transmissibility at high frequency and small acceleration and displacement against vibration during launch and ground testing.
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U2 - 10.1109/AERO.2017.7943840
DO - 10.1109/AERO.2017.7943840
M3 - Conference contribution
AN - SCOPUS:85021186304
BT - 2017 IEEE Aerospace Conference
PB - IEEE Computer Society
T2 - 2017 IEEE Aerospace Conference, AERO 2017
Y2 - 4 March 2017 through 11 March 2017
ER -