KEYWORDS: Global Positioning System, Clocks, Vacuum, Temperature metrology, Data conversion, Calibration, Satellites, Data modeling, Space operations, Physics
We report the results from the ground and on-orbit verification of the XRISM timing system when the satellite clock is not synchronized to the GPS time. XRISM carries a GPS receiver which synchronizes the main satellite clock to the GPS time but in a rare case that the satellite fails to receive the GPS signal, the clock runs freely and its frequency changes depending on its temperature. In this case, we correct the time drift considering the temperature dependency of the clock frequency measured in advance. To confirm that the accuracy of the time assignment in the GPS unsynchronized mode satisfies the requirement (within a 350 us error in the absolute time, for the satellite bus system plus ground system), we have performed the ground and on-orbit tests. In the thermal vacuum test performed in 2022, we obtained the GPS unsynchronized mode data and the temperature versus clock frequency trend. Comparing the time values assigned to the data and the true GPS times when the data were obtained, we confirmed that the requirement was satisfied in the temperature condition of the thermal vacuum test. We also simulated the variation of the timing accuracy in the on-orbit temperature conditions, using the Hitomi on-orbit temperature data and the dependency of the timing error on the temperature gradient obtained in the thermal vacuum test. We found that the error remained within the requirement over ∼ 300000 s without any time calibration data. After the launch, we performed on-orbit tests in 2023 September and October as part of the bus system checkout. The temperature versus clock frequency trend was found to remain unchanged from that obtained in the thermal vacuum test and the observed time drift was consistent with that expected from the trend.
The XRISM is the newly born X-ray satellite led by JAXA and NASA in collaboration with ESA, aiming to perform high-resolution spectroscopy of many astronomical X-ray objects. In the era of multi-messenger astronomy, where observations are performed in various wavelengths and include neutrino and gravitational data, it is important for the observatories to assign precise time of photons. To achieve the science goals of the XRISM mission, an absolute timing accuracy of 1.0 ms is required for the Resolve. The timing system, including both onboard instruments and off-line data-processing tools, is designed to meet this requirement. Following the lessons of the previous X-ray mission of Hitomi, comprehensive list of items that affect the accuracy of the timing are listed together with the timing error budget. During the system design and verification phases on the ground, all elements are controlled and verified to be within the budgets at the component level. After the launch of the satellite on 7 September 2023, in the initial commissioning phase, the overall timing performance of the timing system is scheduled to be confirmed to satisfy the timing requirements using a millisecond pulsar. The XRISM spacecraft carries the GPS receiver and the timing system uses the GPS signals in the nominal operation mode. In this presentation, we summarize the detailed design of the timing system of the XRISM, and the results of the timing verification tests both on ground and in orbit in the nominal operation mode. Detailed results on the failure mode of the GPS receiver will be presented in another presentation.
KEYWORDS: Space operations, Data processing, Photovoltaics, Equipment, Calibration, Source mask optimization, Information technology, Data archive systems, Satellites, X-rays
The X-Ray Imaging and Spectroscopy Mission (XRISM) is an international X-ray observatory developed by Japan Aerospace Exploration Agency (JAXA) and National Aeronautics and Space Administration (NASA) in collaboration with European Space Agency (ESA), successfully launched in September 2023. Since the early stage of the project, the XRISM science operations team (SOT) was organized independently of the spacecraft bus system and mission instrument development teams, having prepared for the in-orbit science operations to maximize the scientific outputs. During about half year for the initial operation phase after launch, operations for the mission instruments were started, and the quick-look and the pipeline processes were carried out by SOT in order to check the functions of the instruments. After transition to the nominal operation phase, we started the target observations in the performance verification phase, whose short and long-term observation plans are considered by SOT, including planning the target of opportunity observations. The information on the observation modes of the mission instruments and the status of the data processing is maintained collectively in database synchronized between JAXA and NASA. We also performed the performance verification and optimization activities which provide the well-calibrated data, appropriate tools, and analysis methods for the users and established a help desk that supports the XRISM data analysis. The publicly solicited observation for the guest observer will be started from August or September 2024. These daily science operations are being carried out by dedicated scientists belonging to JAXA in collaboration with the other SOT members, the mission operations team and the instrument teams. This paper will introduce the ground system for the XRISM science operations and report on the activities of the SOT from the launch to today and plans for future science operations.
Xappl is a software framework written in Python to build pre-pipelines for the X-Ray Imaging and Spectroscopy Mission (XRISM) scheduled to be launched in the Japanese fiscal year 2022. Xappl chains software tasks in the order specified in configuration files in the INI format, enabling us to reduce the telemetry data to First FITS Files, which originate datasets ready for analysis. Since the functionalities of Xappl are highly generalized, it is reusable for future missions. In this paper, we present the design of Xappl and report the developmental progress of the pre-pipeline for XRISM.
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