DocumentCode :
1882024
Title :
The Astro-H soft X-ray mirror
Author :
Robinson, David ; Okajima, Takashi ; Serlemitsos, Peter ; Soong, Yang
Author_Institution :
Goddard Space Flight Center, NASA, Greenbelt, MD, USA
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
9
Abstract :
The Astro-H is led by the Japanese Space Agency (JAXA) in collaboration with many other institutions including the NASA Goddard Space Flight Center. Goddard´s contributions include two soft X-ray telescopes (SXTs). The telescopes have an effective area of 562 cm2 at 1 keV and 425 cm2 at 6 keV with an image quality requirement of 1.7 arc-minutes half power diameter (HPD). The engineering model has demonstrated 1.1 arc-minutes HPD error. The design of the SXT is based on the successful Suzaku mission mirrors with some enhancements to improve the image quality. Two major enhancements are bonding the X-ray mirror foils to alignment bars instead of allowing the mirrors to float, and fabricating alignment bars with grooves within 5 microns of accuracy. An engineering model SXT was recently built and subjected to several tests including vibration, thermal, and X-ray performance in a beamline. Several lessons were learned during this testing that will be incorporated in the flight design. Test results and optical performance are discussed, along with a description of the design of the SXT.
Keywords :
X-ray astronomy; astronomical telescopes; mirrors; Astro-H soft X-ray mirror; Goddard contributions; Japanese Space Agency; NASA Goddard Space Flight Center; Suzaku mission mirrors; X-ray mirror foils; X-ray performance; alignment bars; effective area; engineering model; engineering model SXT; flight design; half power diameter error; image quality requirement; optical performance; soft X-ray telescopes; thermal test; vibration test; Adaptive optics; Assembly; Bars; Fasteners; Mirrors; Optical imaging; X-ray imaging;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187155
Filename :
6187155
Link To Document :
بازگشت