Rocket engine ground ignition test system and method, terminal equipment and medium
A rocket engine and ignition test technology, which is applied in the direction of rocket engine devices, mechanical equipment, machines/engines, etc., can solve problems that affect the operation of rockets, engine failure, etc., and achieve the effect of increasing test coverage and wide application range
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Embodiment 1
[0032] Please refer to figure 1 It is a functional block diagram of a rocket engine ground ignition test system in the first embodiment of the present application. The system includes an ignition test tooling 10, a comprehensive control machine 20 for simulating the control equipment on the rocket, and a pre-embedded cable 32 to communicate with the system. The integrated control unit 30 connected with the signal of the integrated control machine 20, the integrated control unit 30 simulates the ground control terminal in the measurement and control room of the rocket launch, and the measurement and control room is provided with the first control power supply 31 for supplying power to the integrated control unit 30; A measurement and control device 80 is provided, and the measurement and control device 80 is a device used to collect signals in the engine ignition test. No need to repeat them here, the signals of each sensor in the engine are merged into the pre-embedded cable 32...
Embodiment 2
[0041] Such as figure 2 Shown is the flow chart of the second embodiment of the present application, the present embodiment is based on the test method of the rocket engine ground ignition test system in embodiment one, comprises the following steps, the default subject of the following steps is the comprehensive control machine:
[0042] s10. Receive an ignition instruction sent by the integrated control unit through the embedded cable;
[0043]Sending control instructions according to the control sequence of the rocket to be applied by the engine, specifically including:
[0044] S20. Sending a separation ignition instruction to the separation system, after the separation system 50 receives the separation ignition instruction, it is about to ignite the separation pyrotechnics in the tail section, and the tail section 51 is exploded;
[0045] s30. Send the upper end surface sub-insertion electrical sub-command to the separation system; the upper end-face sub-insertion elect...
Embodiment 3
[0050] This embodiment provides a terminal device, including a memory, a processor, and a computer program stored in the memory and operable on the processor. When the processor executes the computer program, any one of the above items can be realized. Steps in the method for processing data without buried point interpolation. Such as Figure 4 As shown, the terminal device is, for example, a computer, and the computer system includes a central processing unit (CPU) 501, which can be loaded into a random access memory (RAM) 503 according to a program stored in a read-only memory (ROM) 502 or from a storage part. Various appropriate actions and processing are performed by the program. In RAM 503, various programs and data necessary for system operation are also stored. The CPU 501 , ROM 502 , and RAM 503 are connected to each other through a bus 504 . An input / output (I / O) interface 505 is also connected to the bus 504 .
[0051] The following components are connected to th...
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