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T. Mistry

Publications and source records attributed to T. Mistry.

2 recordsLinked to original sources

Radiation Tolerance of Low-Noise Photoreceivers for the LISA Space Mission

This study investigates the effects of space environmental radiation on the performance of InGaAs Quadrant Photodiodes (QPDs) and assesses their suitability for the Laser Interferometer Space Antenna (LISA) mission. QPDs of 1.0, 1.5 and 2.0 mm have been irradiated with 20 and 60 MeV protons, 0.5 and 1 MeV electrons, and Co$^{60}$ gamma. An exposure corresponding to a displacement damage equivalent fluence of $1.0 \times 10^{+12}$ p/cm$^2$ for 20 and 60 MeV protons and a total ionizing dose of 237 krad were applied, surpassing the anticipated radiation levels for the LISA mission by a factor of approximately five. Experiments were conducted to measure changes in QPD dark current, capacitance, and responsivity. The QPDs are integrated with a low-noise DC-coupled transimpedance amplifier to form the Photoreceiver (QPR). QPR noise and performance in an interferometric system like LISA were also measured. Although radiation impacted their dark current and responsivity, almost all QPDs met LISA's validation criteria and did not demonstrate any critical failure. These findings prove that the tested QPDs are promising candidates for LISA and other space-based missions.

physics.ins-det

A Pseudo Plane-wave Gravitational Calibrator for Gravitational Wave Observatories

The precisions of existing gravitational calibrators for gravitational wave observatories are limited by their dependence on the relative position between the calibrators and the observatory's test masses. Here we present a novel geometry consisting of four quadrupole rotors placed at the vertices of a rectangle centered on the test mass. The phases and rotation directions are selected to produce a pseudo plane-wave sinusoidal gravitational acceleration with amplitude of ~ 100 fm/s^2. We show that this acceleration only has minimal dependence on the test mass position relative to the rotor array and can yield 0.15% acceleration amplitude uncertainty while tolerating a 1-cm test mass position uncertainty. The acceleration can be directed precisely along the optical axis of the interferometer arm and applies no torque on the test mass. In addition, the small size of the rotors has significant engineering and safety benefits.

gr-qc