Projects
Laser Link in Space
The CLICK (CubeSat Laser Infrared CrossLinK) mission demonstrates high-speed data transfer between two satellites in low Earth orbit using infrared lasers at 20 Mbps. By employing pulse-position modulation, the satellites encode information based on the precise timing of laser pulses, synchronized using chip-scale atomic clocks (CSACs) for nanosecond-level accuracy. This precise synchronization enables the satellites to achieve 50 cm ranging precision and reliable time-of-flight measurements, essential for future space communication networks.
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Charge Management – Verification Testing and Flight Hardware Development
Cosmic rays will charge the Test Masses inside the LISA satellites. Interaction with electric fields then creates acceleration noise that can limit the sensitivity of the Gravitational Wave measurement. To prevent this, we discharge the Test Masses with ultraviolet (UV) light via the photoelectric effect, a technique successfully employed in the LISA Pathfinder mission. However, the Charge Management Device (CMD) for LISA will utilize UV LEDs, a departure from LISA Pathfinder’s approach.
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Apparent Yield Measurements using a LISA-like Gravitational Reference Sensor and the University of Florida Torsion Pendulum
Space-based gravitational missions rely on the pure free-fall of isolated test masses (TM). Charge build-up on these TMs will incur spurious electrostatic forces which ultimately spoil the high-precision measurements necessary to reach the required mission performance.
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Characterization of the LISA Fiber Optic Harness: Modeling the UV Light Transmission in the LISA CMD
The LISA fiber optic harness (FOH) transmits UV LED light onto the LISA test masses to release built up charge from the space environment. A model of the UV light transmission through the FOH and optical feedthrough (OFT) has been developed as an input to an end-to-end simulation of the photoelectric discharging process.
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LISA Test Mass Glitches: Maximum Likelihood Detection & Subtraction in TDI Data
LISA Pathfinder observed several unexpected test mass acceleration events during its flight. These “glitches” have been attributed to sudden releases of trapped gas from within the electrode housings. We examine the effect of similar glitches on LISA’s TDI outputs, and demonstrate a maximum likelihood technique for removing them in post-processing.
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End-to-End Multiphysics Simulation of PhotoelectricCharge Management: Application to Free-falling Test Masses
We present a simulation for the charge management process in its entirety using the COMSOL Multiphysics modeling software. We recover the UV absorption map inside GRS, the quantum yield (QY), and work functions of both test mass and electrode housing surfaces through an MCMC fit of the model and empirical AY results.
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Laser communication, timing transfer, rangingand PAT in the CLICK B/C mission
LISA's laser link requires Pointing, Acquisition and Tracking (PAT) and deploys laser data communication, timing transfer and ranging. CLICK (CubeSat Laser Infrared CrosslinK) is an independent demonstrator for these concepts.
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CubeSat Handling of Multisystem Precision Time Transfer
CHOMPTT is emitting StenSat packets, an AX.25 UI frame sent using AFSK1200 modulation. You can help us keep track of CHOMPTT's status by uploading these packets. Listen for the beacon at a carrier frequency of 437.56 MHZ with 1200 baud AFSK modulation. There are "Bus packets" (CHOMPTT) and "Opti packets" (OPTI). Since StenSat cannot send binary data, all telemetry is encoded in ASCII85.
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