ISO 16694:2015
For ISO 16694:2015, item title is Space systems — The measured parameters at firing bench and flight tests of liquid rocket engines; status code is 9599; successor is ISO 16694:2024; withdrawn / published date is 2015-03-03, recorded from its source on 2026-08-05.
- Identifier
- ISO 16694:2015 verified
- Item title
- Space systems — The measured parameters at firing bench and flight tests of liquid rocket engines verified
- Status code
- 9599 verified
- Successor
- ISO 16694:2024
- Withdrawn / published date
- 2015-03-03 verified
Verified
Review by
What the source says
57447,IS,,ISO 16694:2015,Space systems — The measured parameters at firing bench and flight tests of liquid rocket engines,Systèmes spatiaux — Paramètres mesurés au banc d'allumage et essais de vol des moteurs à propergol liquide,2015-03-03,1,['49.140'],ISO/TC 20/SC 14,9599,,[83493],['en'],13,"<p>ISO 16694:2015 applies to all types of liquid rocket engines for expendable launch systems and satellites:</p><p>a) Combustible fuel (including cryogenic);</p><p>b) Large-thrust, multiple component engines, with and without afterburning;</p><p>c) Low-thrust engines, one component (mono-propellant) and two-component (bi-propellant).</p><p>This International Standard establishes a list of par
— isopublicstorageprod.blob.core.windows.net, retrieved 2026-08-05
Source
- isopublicstorageprod.blob.core.windows.nethttps://isopublicstorageprod.blob.core.windows.net/opendata/_latest/iso_deliverables_metadata/csv/iso_deliverables_metadata.csv