• Shopping Cart
    There are no items in your cart

BS ISO 16694:2015

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Space systems. The measured parameters at firing bench and flight tests of liquid rocket engines

Available format(s)

Hardcopy , PDF

Superseded date

24-09-2024

Superseded by

BS ISO 16694:2024

Language(s)

English

Published date

31-03-2015

€231.38
Excluding VAT

Foreword
Introduction
1 Scope
2 Normative references
3 Symbols and abbreviations
4 General
5 The measured parameters at tests of LRE

Pertains to all types of liquid rocket engines for expendable launch systems and satellites: a) Combustible fuel (including cryogenic); b) Large-thrust, multiple component engines, with and without afterburning; c) Low-thrust engines, one component (mono-propellant) and two-component (bi-propellant).

Committee
ACE/68
DevelopmentNote
Supersedes 13/30235921 DC. (03/2015)
DocumentType
Standard
Pages
24
PublisherName
British Standards Institution
Status
Superseded
SupersededBy
Supersedes

This International Standard applies to all types of liquid rocket engines for expendable launch systems and satellites: Combustible fuel (including cryogenic); Large-thrust, multiple component engines, with and without afterburning; Low-thrust engines, one component (mono-propellant) and two-component (bi-propellant). This International Standard establishes a list of parameters to be measured and registered with the firing stand and flight tests of serial LRE. The order of preparation and carrying out of stand and flight tests, methods of processing, and analysis of tests results of liquid rocket engines, also measurement accuracy requirements are not regulated by this International Standard. Measurement accuracy requirements are established by engine designer. Parameters listed in this International Standard characterize performance attributes of liquid rocket engines and are used for evaluating of technical state of engines (operative, inoperative), if they correspond to the requirements specified and possibilities of putting them into operation. There are parameters specified in this International Standard, obligatory for registration and optional ones. The manufacturer of liquid rocket engines can determine additional list of parameters for specific items taking into account their design and diagrammatical features. The meaning “optional parameter” denotes (in cases when a proper unit or a component can be the part of an engine) that according to the manufacturer’s decision, measurements are allowed not to be made. Measurement of parameters at firing stand and flight tests of liquid rocket engines is be made by means of the same sensors if possible.

Standards Relationship
ISO 16694:2015 Identical

ISO 15865:2005 Space systems — Qualification assessment
ISO 15864:2004 Space systems General test methods for space craft, subsystems and units
ISO 24917:2010 Space systems General test requirements for launch vehicles

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.