2021
DOI: 10.20944/preprints202111.0259.v1
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Study on Electromagnetic Radiation Interference Caused by Rocket Fuel

Abstract: During the launch and return of a spacecraft, the intense combustion of propellants generates strong electromagnetic radiation, which interferes with the operation of electronic equipment in the spacecraft. To improve the electromagnetic compatibility of electronic equipment in spacecraft, it is necessary to study the electromagnetic radiation characteristics of rocket fuel. An electromagnetic radiation measurement system based on antennas is designed to measure the electromagnetic radiation generated by rocke… Show more

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Cited by 3 publications
(2 citation statements)
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“…The maximum sampling rate is set to 3 GSa/s, the electromagnetic signal with the highest frequency of 1.5 GHz can be collected on basis of Nyquist sampling law, which matches the frequency bandwidth of antenna. The sampling duration is set to 810 ms, in which the sampling duration before the trigger is 10 ms, and the sampling duration after the trigger is 800 ms [17][18][19][20][21]. As shown in Figure 1…”
Section: Experimental Principlementioning
confidence: 99%
“…The maximum sampling rate is set to 3 GSa/s, the electromagnetic signal with the highest frequency of 1.5 GHz can be collected on basis of Nyquist sampling law, which matches the frequency bandwidth of antenna. The sampling duration is set to 810 ms, in which the sampling duration before the trigger is 10 ms, and the sampling duration after the trigger is 800 ms [17][18][19][20][21]. As shown in Figure 1…”
Section: Experimental Principlementioning
confidence: 99%
“…In a bunker where is 100 meters from the energetic material, thermal imaging instruments are placed to measure the temperature of the plasma during the detonation process. The thermal imaging instrument has a temperature measurement range of -40 to 2500 K and frame rate of 250 fps, and it has a thermal sensitivity of less than 15 mK with an accuracy of 1% of the reading value [26]. 4, from which it can be obtained that the duration of the detonation process is approximately 2.1 seconds, and the fireball gradually disappears after 1.0 seconds.…”
Section: Figure 2 Schematic Diagram Of Plasma Changes Caused By Deton...mentioning
confidence: 99%