BS EN 16603-35-10:2014
Current
The latest, up-to-date edition.
Space engineering. Compatibility testing for liquid propulsion components, subsystems and systems
Hardcopy , PDF
English
30-09-2014
Foreword
1 Scope
2 Normative references
3 Terms, definitions and abbreviated
terms
4 General requirements for compatibility
tests
5 Identification of compatibility problems
for liquid propulsion systems
6 Identification of tests to characterize the
compatibility
7 Deliverables
Annex A (normative) - Compatibility assessment
and applicability report for liquid propulsion
components, subsystems and systems
(CAAR) - DRD
Annex B (normative) - Compatibility Testing
for Liquid Propulsion Report (CTLP) - DRD
Annex C (normative) - Propulsion components
and subsystems compatibility aspects
Annex D (normative) - Known incompatibilities
Annex E (informative) - Example of tailoring
the requirements list for propulsion systems
Bibliography
Describes materials used in propulsion for which incompatibility can create problems.
Committee |
ACE/68
|
DocumentType |
Standard
|
Pages |
70
|
PublisherName |
British Standards Institution
|
Status |
Current
|
ECSS-E-ST-35-10 belongs to the propulsion field of the mechanical discipline, as defined in ECSS-S-ST-00, and concerns itself with compatibility testing of propulsion components, sub-systems and systems.
Compatibility encompasses the interaction of two or more materials, solids (e.g. structural materials), liquids (e.g. propellants, simulation and cleaning liquids) or gases (e.g. air, pressurants). In case the interaction has the effect that the properties of the materials change, there is the possibility of a compatibility issue.
The standard:
identifies materials used in propulsion for which incompatibility can create problems,
identifies the time scale at which problems can occur. It makes a difference whether a system is only stored or operational for a short period and is to function only during launch (time scale measured in months) and systems that have a long life in orbit (time scale measured in years),
identifies the liquid propulsion components, subsystems and systems to be subject to compatibility testing,
identifies, specifies and defines the tests, test conditions and compatibility test procedures to ensure that representative compatibility testing can take place, and
establishes the test requirements.
The standard is applicable to the design and the qualification of liquid propulsion components, sub-systems and systems and can be applied to their development; it also applies to COTS items procured for the propulsion system.
From the tests described in this standard the effects of interactions of space propulsion materials and fluids on the components, subsystems and systems can be established. In this way it can be assured that the component, subsystem or system satisfies the requirements.
This standard is limited to tests on component-, subsystem- and system-level. Only for those cases where new materials, substances or conditions are involved for which there is no experience or data available, the performance of screening tests is specified.
This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Standards | Relationship |
EN 16603-35-10:2014 | Identical |
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ISO 21010:2014 | Cryogenic vessels Gas/materials compatibility |
ASTM G 72 : 2001 | Standard Test Method for Autogenous Ignition Temperature of Liquids and Solids in a High-Pressure Oxygen-Enriched Environment |
ASTM G 71 : 1981 | GUIDE FOR CONDUCTING AND EVALUATING GALVANIC CORROSION TESTS IN ELECTROLYTES |
EN 16602-70-45:2014 | Space product assurance - Mechanical testing of metallic materials |
NACE TM 04 99 : 2009 | IMMERSION CORROSION TESTING OF CERAMIC MATERIALS |
ISO 10297:2014 | Gas cylinders — Cylinder valves — Specification and type testing |
EN 16602-70-37:2014 | Space product assurance - Determination of the susceptibility of metals to stress-corrosion cracking |
ASTM G 111 : 1997 | Standard Guide for Corrosion Tests in High Temperature or High Pressure Environment, or Both |
ISO 15859-1:2004 | Space systems Fluid characteristics, sampling and test methods Part 1: Oxygen |
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ISO 15859-7:2004 | Space systems Fluid characteristics, sampling and test methods Part 7: Hydrazine propellant |
EN 16603-35:2014 | Space engineering - Propulsion general requirements |
ASTM G 86 : 1998 : REV A | Standard Test Method for Determining Ignition Sensitivity of Materials to Mechanical Impact in Ambient Liquid Oxygen and Pressurized Liquid and Gaseous Oxygen Environments |
ASTM G 4 : 2001 | Standard Guide for Conducting Corrosion Tests in Field Applications |
EN 16603-32:2014 | Space engineering - Structural general requirements |
EN 16603-32-10:2014 | Space engineering - Structural factors of safety for spaceflight hardware |
ASTM D 570 : 1998 : R2018 | Standard Test Method for Water Absorption of Plastics |
EN 16603-35-06:2014 | Space engineering - Cleanliness requirements for spacecraft propulsion hardware |
ASTM D 638 : 2014 : REDLINE | Standard Test Method for Tensile Properties of Plastics |
ISO 1817:2015 | Rubber, vulcanized or thermoplastic Determination of the effect of liquids |
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