DocumentCode :
2908300
Title :
Current technology development efforts on the international X-ray Observatory
Author :
Robinson, David
Author_Institution :
NASA Goddard Space Flight Center, Greenbelt, MD, USA
fYear :
2011
fDate :
5-12 March 2011
Firstpage :
1
Lastpage :
11
Abstract :
The International X-ray Observatory (IXO) is a collaboration between NASA, ESA, and JAXA which is under study for launch in 2021. IXO will be a large 6600 kilogram Great Observatory-class mission which will build upon the legacies of the Chandra and XMM-Newton X-ray observatories. There is an extensive ongoing effort to raise the technology readiness level of the X-ray mirror from TRL 3 to TRL 6 in the next decade. Improvements have recently been made in the area of positioning and bonding mirrors on the nanometer scale and developing metals and composites with a matching coefficient of thermal expansion to the glass X-ray mirrors. On the mission systems side, the NASA reference design has been through a preliminary coupled loads analysis and a STOP analysis of the flight mirror assembly has been initiated. An impact study was performed comparing launching IXO on an Ariane 5 or a U.S. EELV. This paper will provide a snapshot of NASA´s current observatory configuration and summarize the progress of these various technology and design efforts.
Keywords :
astronomical instruments; astronomical observatories; mirrors; thermal expansion; Ariane 5; Chandra observatory; ESA; Great Observatory-class mission; International X-ray Observatory; JAXA; NASA reference design; STOP analysis; TRL 3; TRL 6; U.S. EELV; XMM-Newton X-ray observatory; bonding mirrors; coupled load analysis; flight mirror assembly; glass X-ray mirrors; matching coefficient; nanometer scale; thermal expansion; Adaptive optics; Bonding; Glass; Mirrors; Observatories; Optical distortion; Solid modeling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2011 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4244-7350-2
Type :
conf
DOI :
10.1109/AERO.2011.5747380
Filename :
5747380
Link To Document :
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