Space systems. The measured parameters at firing bench and flight tests of liquid rocket engines Ingestion-build-50790 The environmental conditions specified in

The environmental conditions specified in this document are limited to those which can directly affect the performance of products

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Space systems. The measured parameters at firing bench and flight tests of liquid rocket engines Ingestion-build-50790 The environmental conditions specified in1 Scope This International Standard applies 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). This International Standard establishes a list of parameters to be measured and registered with the firing stand and