标准摘要
[中文适用范围]： 本文件规定了在试验台和飞行试验中测量的参数列表的要求。本文件的要求适用于所有类型的一次性液体火箭发动机：a) 使用各种推进剂（包括低温推进剂）；b) 带有燃烧室点火（带有逐渐燃烧）和不带燃烧室点火（没有逐渐燃烧）；c) 低推力发动机：单组元（单推进剂）和双组元（双推进剂）；d) 单次点火或多次点火。本文件未规定试验台测试准备、测试程序、测试结果处理和分析方法以及测量精度的要求。本文件规定了强制性和选择性参数。 [外文原描述]： This document specifies requirements for the list of parameters, measured during firing bench and flight tests. The requirements of the document apply to all the types of expendable liquid rocket engines supplied to the user: a) operating on all types of propellant (including cryogenic); b) with afterburning (with gradual burning) and without afterburning (without gradual burning); c) low-thrust engines: one component (monopropellant) and two-component (bipropellant); d) with a single firing or multiple firings. The document doesn’t specify firing bench test preparation and testing procedure, methods of test results processing and analysis, or requirements to measurement accuracy. The document specifies mandatory and optional parameters.
英文名称Space systems — Measured parameters at firing bench and flight tests of liquid rocket engines