Abstract
New demands for space and earth observations drive the need for large apertures of 10 m and higher in telescopes. This requires new types of alternative lightweight and deployable primary reflector or lens concepts with aerial densities of <3 kg/m2. Some syntheses between optical and especially mechanical and material aspects for large planar photon sieves and non-imaging telescopes are discussed. Focus is put on large planar and highly perforated membranes for photon sieves and shell-membrane type deployable (parabolic) reflectors, respectively. The reflecting surface of the latter is composed of specific C-fiber reinforces silicone (CFRS) material. In addition to possible shape control, emphasis is also given to reflective coating of CFRS. Engineering challenges requiring future activities are identified.
Original language | English |
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Pages (from-to) | 117-124 |
Number of pages | 8 |
Journal | CEAS Space Journal |
Volume | 5 |
Issue number | 3-4 |
DOIs | |
State | Published - Dec 2013 |
Keywords
- Deployable structures
- Large telescopes
- Photon sieve
- Shape control
- Shell-membranes, dimensional stability
- Surface coating