We report the development of space qualified three-channel bistatic Laser Detection and Ranging (LADAR) system capable of working up to 2.2 km which includes Master oscillator power amplifier (MOPA) based on High Power Fiber Lasers with specifications of 5W Peak power, 4-millisecond pulse-width at 1550 nm central wavelength. Transmitter-Receiver collimators are aligned in Bistatic configuration within 3.6 arc second accuracy. Doppler shift measurement is estimated using all-fiber optical heterodyne interferometry and thereby highly accurate velocity detection is achieved with 3 sigma accuracy of ±3.108, ±4.063, and ±3.3903 mm/s. The developed LADAR sensor system for velocity measurement is space qualified and has shown nominal performance during all phases of thermal and vibration tests.
The solar ultraviolet imaging telescope (SUIT) is an imaging telescope on-board the Aditya-L1 satellite, which is India’s maiden space mission dedicated solely to solar observations. The spatially resolved, high cadence observations are designed to be taken in eleven science filters with full width half maxima ranging between 0.1–58 nm and spread over the near-ultraviolet (NUV) domain of the solar spectrum (200–400 nm). The huge incoming solar flux, limited by the linearity regime performance of the charge coupled device (CCD) as well as the thermal operational constraints, mandate the use of an entrance aperture filter, the thermal filter (TF), for SUIT. The design of this filter is, further, constrained by exposure time and enhanced emission of the sun during eruptive events. From performance perspective, the TF reflects ∼50% of the incident radiation and allows only 0.1–0.45% of the incoming flux to pass within 200–400 nm. The transmission on either side of the operational range is satisfactorily reduced, so as to ensure minimum unwanted light leaking into the imaging system. Therefore, the TF plays a significant role in increasing the photometric efficiency as well as maintaining the operational temperature of the telescope. To the best of our knowledge, this is the first time any attempt of designing and manufacturing any such rejection filter aiming optimized performance in the NUV range is being done for a space-based imaging solar telescope. The choice of materials for substrate and coating for the filter poses several challenges in terms of contamination, corrosion/ oxidation, durability during manufacturing process, long-term exposure to harsh space environment as well as formation of pinholes. The transmission and reflection profiles of the fabricated TF is satisfactory to meet our design and technical constraints. The TF is also qualified for various environmental and radiation conditions. The transmission of the TF is seen to be well within our allowed margins (±10% of the design value) even after being exposed to these qualification tests.
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