REG KSC-KTI-5210 REV C-2012 MATERIAL SELECTION LIST FOR OXYGEN SERVICES.pdf
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1、KTI-5210 REVISION: C 1 MATERIAL SELECTION LIST FOR OXYGEN SERVICE APPROVED: _ David Lubas, Chief (Acting) Materials and Processes Engineering Branch (NE-L4) _ Virginia J. Ward, Center Materials Representative (CMR) Materials and Processes Engineering Branch (NE-L4) 1. FOREWORD Materials selection re
2、quirements for oxygen service have changed significantly since the last revision of this document. Historically, flammability and mechanical impact ratings were the main criteria for materials selection for oxygen service. Materials used in liquid oxygen (LO2) or gaseous oxygen (GO2) environments mu
3、st be evaluated as described in NASA-STD-6001B, section 6.3. Materials selection for LO2 and GO2 environments in accordance with NASA-STD-6001B begins with pre-selection of materials based on flammability and combustion test data, followed by flammability assessment of materials in the worst-case co
4、nfiguration and environment. Material flammability ratings based on NASA-STD-6001B test results for many materials, including those identified in this document, are found in the Materials and Processes Technical Information System (MAPTIS) database and ASTM G63 and ASTM G94. If test results are not
5、available through ASTM, NASA, or other sources, materials should be submitted to NASA/NE-L2-T for testing. Requests for flammability testing should be addressed to NASA/MC: NE-L2-T, Kennedy Space Center, FL 32899. The test results will be electronically archived locally at KSC by NASA/NE-L and submi
6、tted for inclusion in MAPTIS II. If the materials are determined to be nonflammable in their use configuration and environment, and no additional material control is required, the materials may be used. If the materials are determined to be flammable, an oxygen compatibility assessment1 (OCA) must b
7、e performed on the components and systems in accordance with NASA/TM-2007-213740, which provides an overview of oxygen fire hazards and procedures which are consistent with the latest versions of ASTM G63, ASTM G94, and ASTM MNL 36. The OCA is used to determine whether the material may be used, or w
8、hether there is a need to perform supplemental material, configuration, or component testing. Requests for oxygen compatibility testing of materials should be addressed to NASA/MC: NE-L2-T, Kennedy Space Center, FL 32899. Oxygen compatibility test results will be transmitted to the customer by NASA/
9、NE-L. The test results will be electronically archived locally at KSC by NASA/NE-L and submitted for inclusion in MAPTIS II. Contact NASA M validate prior to use. Provided by IHS Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-KTI-5210 REVISION: C 2 Materials used
10、in oxygen systems for the Shuttle program were typically been tested for flammability and mechanical impact, which have been the basic criteria for materials selection for oxygen service for more than 20 years. Materials selection for post-Shuttle programs will be in accordance with the materials se
11、lection and OCA requirements called out in NASA-STD-6016 for flight and NASA-STD-5005C for GSE. Materials used in existing oxygen system designs with a history of safe use are considered acceptable for continued use; however, changes to materials used in such systems must be assessed on an individua
12、l basis. Contact NASA M Promoted Ignition (NASA-STD-6001B, Test 17) data are presented for metallic materials. Codes are assigned to each material per KTI-5209, Material Usage Code. The nonmetallic materials listed in Table 1 were also tested per NASA-STD-6001B supplemental tests for mechanical impa
13、ct in ambient pressure LO2 (Test 13A) and variable pressure GO2 and LO2 (Test 13B). The materials listed in Table 1 are rated A2 for mechanical impact up to the operating pressures listed in the table. Mechanical impact is only considered a credible ignition mechanism in certain components; mechanic
14、al impact test results can be utilized as an aid to the OCA process when mechanical impact is identified as a credible ignition mechanism. Batch/lot testing for mechanical impact is no longer required for all soft goods used in oxygen service in the 1,650 - 6,700 psi range. NASA Design Engineering o
15、r NASA M number of tests = 20 and the number of reactions = 0 (zero), or number of tests = 60 and the number of reactions = 1 (one). Standard impact energy is 72 ft-lb, but may vary. Consult MAPTIS for actual test conditions. RELEASED - Printed documents may be obsolete; validate prior to use. Provi
16、ded by IHS Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-KTI-5210 REVISION: C 3 The vendors and applicable specifications for the materials listed in this KTI have been updated from the previous revision. These listings do not take into account the effects of unk
17、nown formulation and/or process changes that could be performed by a manufacturer, which could result in a material performing differently than these test results would indicate. Materials requiring initial testing, revalidation testing, or mechanical impact testing in accordance with NASA-STD-6001B
18、 may be submitted to the KSC Materials Science Laboratory. 3. GUIDELINES FOR MATERIALS SELECTION FOR OXYGEN SYSTEM DESIGN The list is new to this revision and is intended as a starting point for materials selection in the preliminary design phase. This list is to be utilized only as reference prior
19、to evaluation of the system for oxygen service. 3.1 Nonmetallic Materials (Soft Good Materials and Lubricants) Nearly all soft goods and lubricants are flammable in oxygen at ambient pressure. Selection of soft goods is based on their relative performance in various oxygen compatibility studies (aut
20、ogenous ignition, heat of combustion, oxygen index, mechanical impact, and gaseous impact tests) and histories of use within NASA and other institutions. In addition to material compatibility, mechanical properties of soft goods and lubricants must be considered, e.g., cold flow of PTFE. Information
21、 on material trade names within the chemical classes is found in Table 1. Consult ASTM G63 for further information on selection of nonmetallic materials for oxygen service. The following nonmetallic materials are recommended for consideration for oxygen service: Plastics Polytetrafluoroethylene (PTF
22、E) Fluorinated ethylene propylene (FEP) Perfluoroalkoxy (PFA) Polychlorotrifluoroethylene (PCTFE) Polyimide (PI) Amorphous fluoropolymers Elastomers Fluorocarbonelastomer (FKM) Perfluoroelastomer (FFKM) Fluorosilicone elastomer (MVQ) RELEASED - Printed documents may be obsolete; validate prior to us
23、e. Provided by IHS Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-KTI-5210 REVISION: C 4 Lubricants Perfluoropolyether (PFPE) Chlorotrifluoroethylene (CTFE) oligomers Molybdenum disulfide (MoS2) dry lubricants 3.2 Ceramics All ceramics without organic fillers or b
24、inders may be used in oxygen service; however, due to the brittleness of many ceramics, consideration of the effects of failure, including the functionality of components within the system, is recommended. Contact NASA M Replaces Braycote 600 with environment friendly formula. May require re-test. C
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