International Standard
ISO 16694:2024
Space systems — Measured parameters at firing bench and flight tests of liquid rocket engines
Reference number
ISO 16694:2024
Edition 2
2024-09
© ISO 2024
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Published (Edition 2, 2024)

ISO 16694:2024

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Format
CHF 129
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Abstract

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.

General information

  • Status
     : Published
    Publication date
     : 2024-09
    Stage
    : International Standard published [60.60]
  • Edition
     : 2
    Number of pages
     : 19
  • Technical Committee :
    ISO/TC 20/SC 14
    ICS :
    49.140 
  • RSS updates

Life cycle

Sustainable Development Goals

This standard contributes to the following Sustainable Development Goal

9
Industry, Innovation and Infrastructure

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