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MAXIM Periscope Module

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X-ray imaging can pierce the dusty centers of galaxies in order to study some of ... you see with micro arc-second imaging in the x-ray region of the spectrum? ... – PowerPoint PPT presentation

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Title: MAXIM Periscope Module


1
MAXIM Periscope Module
  • Science Liaison
  • H. John Wood
  • (Read by Jennifer Bracken)
  • 25 April 2003

2
Structure and Evolution of the Universe
  • In order to study the structure and evolution of
    the universe micro arc-second imaging will be
    required
  • X-ray imaging can pierce the dusty centers of
    galaxies in order to study some of the most
    energetic events in creation
  • What can you see with micro arc-second imaging in
    the x-ray region of the spectrum?
  • accretion disks of black holes
  • stellar coronae and interacting binaries
  • Cataclysmic variables and X-ray binaries
  • Distant Active Galactic Nuclei

3
Two globular clusters
These globular clusters both have giant black
holes at their centers
4
The Event Horizon can be Imaged by MAXIM
5
Purpose of the Study
  • An optics oriented study
  • Are the mirrors impossible to make?
  • Are actuators available to move the mirrors by nm
    steps over microns of range?
  • Can the thermal and structural environment be
    benign enough to maintain mirror figure and
    stability?
  • Is internal metrology needed if so how to
    implement?
  • What would the alignment procedures be?
  • Trade study on the mirror sizes and the impact on
    the number and sizes of the spacecrafts
  • What are the cost, mass and power inputs?

6
The Collecting Area of Chandra for 1/10 The Cost
  • Chandra has 0.5 arc sec resolution and its
    mirrors cost 400M
  • This study has shown that it is possible to build
    a microarcsec imaging telescope with the same
    collecting area as the current Chandra for 1/10
    its cost
  • The study has also shown how the engineering can
    be done to allow X-ray imaging and spectroscopy
    in formation flying
  • The nature of the detector allows imaging over a
    large range of energies simultaneously

7
Full MAXIM Design Overview
  • Configuration at L2
  • Hub and 25 free-flyers form an objective over a
    one-kilometer diameter area
  • 4-mirror grazing-incidence periscopes in each
    spacecraft reflect x-rays to a detector ship
    20,000 km away
  • Alignment of the optical beams and phasing of
    them on the detector allows formation of an image
  • Collecting area is 1000 square centimeters the
    entrance aperture is 18.25 by 0.489 cm for each
    periscope
  • Thus, each of the 25 free flyers will have 4
    periscopes and the hub will have 12 periscopes
    for a total of 112 periscopes

8
Full MAXIM Design Overview cont
  • Optical design
  • 4-mirror grazing-incidence periscope design
    simulates the properties of a thin lens optical
    tolerances are relaxed in comparison to a typical
    two-mirror X-ray design
  • In the periscope, each flat mirror is used at 1
    degree angle of incidence
  • Mirrors are known by their numbers in sequence
    they are hit by X-rays (1 entrance, 2, 3 and
    4 exit)
  • Flat mirrors are 30 x 20 x 5 cm with the optical
    reflection on the 30 x 20 face (gold coat)
  • Graze direction is in the 30 cm direction and
    requires figure quality of lambda/300 (633nm)
  • Orthogonal direction only requires lambda/10
  • Beam steering with roll and pitch of the exit
    mirror (4)
  • Optical path length phasing by motion of a
    daughter bench carrying mirrors 2 and 3
    relative to the main optical bench which hold 1
    and 4 with its actuators

9
Side View of a Periscope Module
Mirrors in lilac bench in fuchsia daughter
bench in orange with its actuator in gold
10
A Dual-Periscope Module
Note the entrance slots right with one shutter
open one closed
11
Up Next
  • The Systems Engineering Report will be presented
    by Deborah Amato
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