Electric propulsion spacecraft plume parameter acquisition method
A parameter acquisition and spacecraft technology, applied in the aerospace field, to achieve the effect of increasing accuracy, reducing the risk of test operation, and improving sensitivity
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[0035] The electric propulsion spacecraft plume parameter acquisition method of the present invention, it comprises the following steps:
[0036] Step 1, such as figure 1As shown, assemble the various parts of the plume parameter acquisition device of the electric propulsion spacecraft: set the vacuum chamber observation window 1 at the head end of the vacuum chamber 2; Communication; the ignition control cabinet 8 is connected with the electric thruster 4, and the computer 7 is respectively connected with two electric thruster multi-parameter diagnostic equipment (3, 6). A mounting plate is arranged inside the vacuum chamber 2, and the first electric thruster multi-parameter diagnostic equipment 3 is installed on one end of the mounting plate, and the movable support 5 is fixed at the other end, and the electric thruster 4 is installed on the fixed movable support 5; the electric thrust is fixed on the mounting plate The second electric thruster multi-parameter diagnostic eq...
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