Reflective Optics for Space Applications

Reflective optical components developed for space applications where optical performance, thermal stability, and structural integrity are critical under launch and on-orbit conditions.

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Reflective Optics

Precision mirror

Lightweighted mirror

SiC mirror

Precision Mirrors

flat / spherical mirror

aspheric reflective surface

Factory Standard of Spherical Mirrors

(typical, defined per application)

Parameter

Standard Range

Diameter Tolerance

Defined per application

Clear Aperture

Typically ≥ 90% of diameter

Surface Quality

ISO 10110 (typ. 40–20)

Surface Figure

Defined per wavelength and aperture

Radius of Curvature

Tolerance defined per design

Thickness

Defined per structural requirements

Edge Treatment

Bevel, typical


Specification definitions and acceptance criteria are defined per application.

Materials

Zerodur®, Silicon Carbide (SiC), Fused Silica

* Material selection is defined based on thermal stability, structural requirements, and mission environment.

Manufacturing Capability

  • Ultra-precision mirror polishing
  • Surface figure and roughness control
  • Coating compatibility for space environment

Space Qualification Considerations

  • Thermal stability and CTE management
  • Launch load compatibility
  • Documentation and traceability available

Off-Axis Parabolic (OAP) Mirrors

off-axis geometry)

Standard Specifications

(to be defined per application)

Parameter

Standard Range

Diameter

defined per application (typ. up to several hundred millimeters)

Diameter tolerance

defined per application

Clear aperture

typically ≥ 95%

Surface quality

ISO 10110 (typ. 60–40)

Surface figure

defined per wavelength and aperture

Focal length tolerance

defined per optical design

Off-axis geometry

defined per parent parabola and extraction

Material Selection

Aluminum, Zerodur®, Silicon Carbide (SiC)

Reflective Coatings (space-qualified)

  • Protected Aluminum
  • Enhanced Aluminum (UV / VIS optimized)
  • Protected Silver
  • Protected Gold

*Coating selection is defined per spectral band, environmental conditions, and contamination control requirements.

Manufacturing Capability

  • Parent parabola generation and off-axis extraction
  • Figure error control for off-axis geometries
  • Metrology adapted to non-symmetric surfaces

Space Qualification Considerations

  • Alignment stability under thermal cycling
  • Surface stability under launch environment
  • Configuration control maintained

Silicon Carbide (SiC) Mirrors

SiC mirror Front

lightweighted SiC structure

Standard Specifications

(to be defined per application)

Parameter

Standard Range

Size

Defined per application (including large-format SiC mirrors)

Surface geometry

Flat (typical), Spherical or  Aspheric

Surface figure

defined per aperture and application

Reflective coatings

selected per spectral and environmental requirements


Note: SiC mirrors are selected where high stiffness-to-mass ratio and thermal stability are critical to system performance.

 

Manufacturing Capability

  • SiC machining and finishing
  • Surface preparation for optical coating
  • Dimensional stability management

Space Qualification Considerations

  • High stiffness-to-mass optimization
  • Thermal stability for cryogenic or variable environments
  • Inspection and traceability maintained

Lightweighted Mirrors

lightweight Mirror backside

ribbed / pocketed structure

Standard Specifications

(to be defined per application)

Parameter

Standard Range

Substrate material

Zerodur® (typical), SiC (case-dependent)

Lightweighting

pocketed / ribbed structures (design-dependent)

Mass reduction

defined per stiffness and launch-load requirements

Clear aperture

defined per optical design

Reflective coatings

selected per spectral and environmental requirements

 

Manufacturing Capability

  • Structural lightweighting strategies
  • Mass-to-stiffness optimization
  • Deformation control under launch loads

Space Qualification Considerations

  • Vibration and shock compatibility
  • Structural integrity verification
  • Configuration documentation available

MEMS Mirrors

Standard Specifications

(to be defined per application)

Parameter

Standard Range

Mirror aperture

mm-class, geometry-defined

Surface coating

selected per spectral requirements

Actuation and control

defined per reliability and environmental constraints

Environmental compatibility

vacuum-compatible, hermetically sealed options

Interface definition

defined per system architecture

 

Manufacturing Capability

  • Microfabrication and assembly readiness
  • Interface definition for actuation and control
  • Optical surface quality verification

Space Qualification Considerations

  • Radiation and thermal environment considerations
  • Mechanical robustness under launch conditions
  • Documentation and traceability available

Reflective optics are defined in response to mission-specific optical and environmental constraints.