New Frontiers in Stellar Interferometry 2004
DOI: 10.1117/12.551966
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MAXIM science and technology

Abstract: The Micro Arcsecond X-ray Imaging Mission (MAXIM) has been proposed to NASA in response to the Black Hole Imager line in the newly created "Beyond Einstein" program. Meeting the scientific goals of event horizon imaging has created a new set of technical challenges for the Maxim team. Certainly the most difficult of these is the need for 0.1 micro-arcsecond resolution imaging in the x-ray. We will review the key scientific challenges and show how they flow down into instrument requirements. We will then review… Show more

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Cited by 9 publications
(6 citation statements)
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“…-Mirrors: X-ray mirrors require grazing incidence for effective reflection, where incidence angles θ g of typically less than a degree are needed, depending on photon energy and mirror material. Various studies have been performed, ranging from a single spacecraft approach [73] with a relatively modest resolution of 100 μas, a basic two spacecraft configuration [13] at a separation of a few hundred km, to a full constellation of collecting spacecraft plus a detector spacecraft [12], extending over 20,000 km and providing an angular resolution of 0.1 μas. The latter separations sound extreme but might be significantly mitigated by the optics design (see below).…”
Section: Interferometry Approachmentioning
confidence: 99%
“…-Mirrors: X-ray mirrors require grazing incidence for effective reflection, where incidence angles θ g of typically less than a degree are needed, depending on photon energy and mirror material. Various studies have been performed, ranging from a single spacecraft approach [73] with a relatively modest resolution of 100 μas, a basic two spacecraft configuration [13] at a separation of a few hundred km, to a full constellation of collecting spacecraft plus a detector spacecraft [12], extending over 20,000 km and providing an angular resolution of 0.1 μas. The latter separations sound extreme but might be significantly mitigated by the optics design (see below).…”
Section: Interferometry Approachmentioning
confidence: 99%
“…• Mirrors: X-ray mirrors require grazing incidence for effective reflection, where incidence angles θ g of typically less than a degree are needed, depending on photon energy and mirror material. Various studies have been performed, ranging from a single spacecraft approach [71] with a relatively modest resolution of 100 µas, a basic two spacecraft configuration [13] at a separation of a few 100 km, to a full constellation of collecting spacecraft plus a detector spacecraft [12], extending over 20,000 km and providing an angular resolution of 0.1 µas. The latter separations sound extreme but might be significantly mitigated by the optics design (see below).…”
Section: Interferometry Approachmentioning
confidence: 99%
“…At the expense of an extra reflection, the size of the optical constellation can be brought down from the focal length (depending on desired angular resolution several 10's to 10's of thousands km, see e.g. [5] and [6]). An optical test of the concept was already performed in 2005 [7], but a proper X-ray demonstration has never taken place.…”
Section: Introductionmentioning
confidence: 99%