1. First result of orbit verification of Taiji-1 hall micro thruster
- Author
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Lu-Xiang Xu, Lin-Xiao Cong, Cong-Feng Qiao, Yong-Gui Li, and Shu-Yan Xu
- Subjects
010302 applied physics ,Physics ,Nuclear and High Energy Physics ,Spacecraft ,business.industry ,Dual mode ,Astronomy and Astrophysics ,02 engineering and technology ,Plasma ,021001 nanoscience & nanotechnology ,Space (mathematics) ,01 natural sciences ,Atomic and Molecular Physics, and Optics ,0103 physical sciences ,Aerospace engineering ,Orbit (control theory) ,0210 nano-technology ,business ,Altitude control - Abstract
The Hall Micro Thrusters (HMTs) use cold gas or accelerated plasma dual mode to provide ultra-precise spacecraft altitude control. They were operated in space for the first time as part of the demonstration payloads on Chinese Academy of Science’s (CASs) Taiji-1 spacecraft since September 2019. Hall Micro Thruster Assemblies (HMTAs) were the actuators in drag-free control, and will compensate the nonconservative force for gravity wave observatories. The HMTAs meet the requirements of operating at 5–100 [Formula: see text] N of thrust with 0.7 [Formula: see text] N resolution and [Formula: see text]0.6 [Formula: see text] N/Hz[Formula: see text] (0.01–1 Hz) noise to deliver the nanometer-level precision control as fast as 30 ms measured by Gravitational Reference Sensor (GRS). A transfer function model in z-domain was fit and used to filter HMTs cathode voltage to predict GRSs thrust noise response. Simulations of a single or dual-frequency disturbance and the corresponding compensation demonstrated that HMTAs could deliver the required thrust profile expected. The capability to meet the requirements of thruster noise in drag-free control is critical for future missions because the acceleration noise on test mass directly relates to the gravity wave signa l. Preliminary in-orbit verification of Taiji-1 has showed HMTAs’ great potential in future, and the data in the experiments are presented in this paper.
- Published
- 2021