2020
DOI: 10.1093/ptep/ptaa083
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The Taiji program: A concise overview

Abstract: Taiji is a Chinese space mission to detect gravitational waves in the frequency band 0.1 mHz to 1.0 Hz, which aims at detecting super (intermediate) mass black hole mergers and extreme (intermediate) mass ratio in-spirals. A brief introduction of its mission overview, scientific objectives, and payload design is presented. A roadmap is also given in which the launching time is set to the 2030s.

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Cited by 120 publications
(72 citation statements)
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“…In the future, TianQin (Luo et al 2016) and Taiji (Luo et al 2020) could also join the multimessenger observation strategies. The sensitive frequency of Taiji is slightly lower than LISA, which allows the joint observation of Taiji and SKA to detect more PSR-NS systems with a bit larger P b .…”
Section: Scalar-tensor Theorymentioning
confidence: 99%
“…In the future, TianQin (Luo et al 2016) and Taiji (Luo et al 2020) could also join the multimessenger observation strategies. The sensitive frequency of Taiji is slightly lower than LISA, which allows the joint observation of Taiji and SKA to detect more PSR-NS systems with a bit larger P b .…”
Section: Scalar-tensor Theorymentioning
confidence: 99%
“…The noise level of Taiji is 8 pm=Hz 1=2 over an inter-satellite distance of 3 × 10 6 km. The measurement frequency band is about 10 −4 Hz to 1 Hz [18][19][20] . Achieving such high performance of laser interferometry in space is a huge challenge, and the performance of laser interferometry directly determines the sensitivity of space-based GW detection.…”
Section: Introductionmentioning
confidence: 99%
“…Missions for micro-Newton thruster applications have become prosperous in recent years, and one of the greatest challenges comes from searching for gravitational waves in space [1,2]. To cancel the non-gravitational effects and compensate for the non-symmetric disturbance on the spacecraft, micro thrusters used for the attitude and orbit control are required to achieve high precision of 0.1 µN resolution and wide dynamic range between 1 µN-50 µN, and low thrust amplitude spectral density (ASD) down to 0.1 µN/Hz 1/2 within 0.1 mHz-1 Hz [3,4]. Accordingly, a more accurate thrust measurement system is in need to measure the variance of the micro-Newton thrusters on the ground, which is hard for the case of an ultra-low thrust-to-weight ratio (TWR) less than 10 −9 .…”
Section: Introductionmentioning
confidence: 99%