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Application performance of a hydrazine decomposition catalyst based on a 200 N thruster device(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2024年05期
Page:
148-156
Research Field:
目次
Publishing date:

Info

Title:
Application performance of a hydrazine decomposition catalyst based on a 200 N thruster device
Author(s):
XU Tao; LI Ning; HE Zijun; JIA Meng; ZHANG Zhongzhu; XING Gang; ZHAO Mengchao; DU Zonggang
Xi'an Aerospace Propulsion Test Technology Institute, Xi'an 710100, China
Keywords:
hydrazine decomposition catalyst;  mono-propellant attitude and orbit control engine;  200 N thruster device;  hot-firing test and assessment
PACS:
V511
DOI:
10.3969/j.issn.1672-9374.2024.05.015
Abstract:
This study investigates the application performance of a hydrazine decomposition catalyst using a 200 N thruster device. On the basis that the physical and chemical properties of the catalyst meet the application requirements, the mechanical environment adaptability of the catalyst is investigated using a 200 N thruster device. The low-temperature cold start performance, low-temperature steady-state performance, normal temperature positive and negative bias steady-state performance, and pulse lifetime performance of the catalyst are also investigated. The results indicate that the catalyst has a hydrazine catalytic decomposition efficiency above 99%, excellent mechanical strength, good mechanical environment adaptability, and high hydrazine catalytic decomposition activity and stability. The test shows that the catalyst can meet the usage requirements of a 200 N thruster device.

References:

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