YANG Fu-quan, SUN Yun-kui, GAO Jun. PERFORMANCES TEST OF THE THERMAL THROTTLEERS FOR ION THRUSTERS FLOW REGULATED[J]. VACUUM AND CRYOGENICS, 2011, 17(3): 170-175. DOI: 10.3969/j.issn.1006-7086.2011.03.010
Citation: YANG Fu-quan, SUN Yun-kui, GAO Jun. PERFORMANCES TEST OF THE THERMAL THROTTLEERS FOR ION THRUSTERS FLOW REGULATED[J]. VACUUM AND CRYOGENICS, 2011, 17(3): 170-175. DOI: 10.3969/j.issn.1006-7086.2011.03.010

PERFORMANCES TEST OF THE THERMAL THROTTLEERS FOR ION THRUSTERS FLOW REGULATED

  • Propellant flow rate is very low for ion thrusters,commonly between 0.1~2.0mg/s,and its high stability is required.It is significant that the test and evaluation of the performances and longtime working stability of thermal throttleers.In this paper,the test facility,the test methods,the test process and the estimates to test results are presented.
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