We have been developing our original space X-ray optics by combining space- and ground-based technologies for a solar sounding rocket experiment, FOXSI-4. We completed two Flight Models (FM), soft and hard X-ray optics. Vibration tolerance is one of the most important launch environmental tolerance and thus we established our experimental setup for the two FMs. The imaging quality was evaluated before and after the vibration tests. As a result, no significant changes were detected. In addition, we checked the effect of shims needed for the angle alignment between the optics and detectors integrated into the sounding rocket. We confirmed that the shims do not affect the angle alignment significantly before and after vibration tests.
Access to the requested content is limited to institutions that have purchased or subscribe to SPIE eBooks.
You are receiving this notice because your organization may not have SPIE eBooks access.*
*Shibboleth/Open Athens users─please
sign in
to access your institution's subscriptions.
To obtain this item, you may purchase the complete book in print or electronic format on
SPIE.org.
INSTITUTIONAL Select your institution to access the SPIE Digital Library.
PERSONAL Sign in with your SPIE account to access your personal subscriptions or to use specific features such as save to my library, sign up for alerts, save searches, etc.