The present invention relates to a compact, lightweight, cost-efficient ultraviolet-visible-far infrared (UV-VIS-IR) telescope system, covering the 300 nm to 2500 nm (0.3 μm to 2.5 μm) spectral range, based on a fast focal-ratio, reflective optics design, and an optical coupling interface appropriate for COTS spectrometers, commensurate with about 1U-2U CubeSat payload volume.
Carbon nano-tube polymer composite mirrors for CubeSat telescope
2024-04-30
Patent
Electronic Resource
English
IPC: | G01J Messen der Intensität, der Geschwindigkeit, der spektralen Zusammensetzung, der Polarisation, der Phase oder der Pulscharakteristik von infrarotem, sichtbarem oder ultraviolettem Licht , MEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRA-RED, VISIBLE OR ULTRA-VIOLET LIGHT / B64G Raumfahrt , COSMONAUTICS / G02B Optische Elemente, Systeme oder Geräte , OPTICAL ELEMENTS, SYSTEMS, OR APPARATUS |
Optical Design for a Cubesat: Unobscured Telescope, Using Freeform Mirrors and a Curved Detector
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