REG NASA-LLIS-0686--2000 Lessons Learned Selection of Compatible Materials for use with Fluorine.pdf
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1、Best Practices Entry: Best Practice Info:a71 Committee Approval Date: 2000-03-09a71 Center Point of Contact: GRCa71 Submitted by: Wil HarkinsSubject: Selection of Compatible Materials for use with Fluorine Practice: Use established design guidelines for selection of materials that provide safe opera
2、tion when exposed to elemental fluorine and fluorine-oxygen (FLOX) mixtures.Programs that Certify Usage: N/ACenter to Contact for Information: GRCImplementation Method: This Lesson Learned is based on Reliability Guideline Number GD-ED-2206 from NASA Technical Memorandum 4322A, NASA Reliability Pref
3、erred Practices for Design and Test.Benefit:The design data provides a list of materials and conditions which are compatible for use with fluorine. The use of this data by design engineers will result in the selection of materials for use with fluorine that can provide safe and reliable system opera
4、tion.Implementation Method:Generally failures in systems using fluorine are caused by: (1) improper choice of materials and/or Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-system components; (2) improper fabrication and assembly practices, (ref 1)
5、; and (3) improper system preparation and operating procedures, resulting in the presence of contaminants. This guideline applies design considerations to preclude failures caused by improper choice of materials. Design guidelines to address failure causes (2) and (3) are beyond the scope of this do
6、cument (see Reference 1).The design considerations to be used in selection of materials for use in fluorine systems should consist of:a. Selection of materials based on property requirements for the application (e.g., strength, thermal properties, welding or brazing characteristics, etc). Note: This
7、 design consideration represents standard design approach and is presented here for completeness onlyb. Selection of materials that can be fabricated without introducing contaminants and/or entrapped voids.c. Consideration of effects peculiar to a fluorine environment (e.g., ignition temperature of
8、material in fluorine, fluoride films and exposure to friction, moisture presence and compatibility with hydrogen fluoride, etc).The design considerations of (b) and (c) above are based on extensive test experience from liquid fluorine rocket testing conducted at LeRC, and from materials tests conduc
9、ted at LeRC and other laboratories.References 1, 2, and 3 present material compatibility with liquid fluorine for metallic and nonmetallic materials, respectively. Table 1 below, extracted from reference 1 and presented here for purposes of illustration, lists the ignition temperatures and ignition
10、delays for metals in fluorine.Table 1. Ignition Temperatures of Metals in Fluorine (a) Technique A Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Metal Wire diameter, in.Ignition temperature, CAverage ignition temperature, CMax variation from averag
11、e, percentAluminum 0.010 0.016- (a) -Copper 0.0123 645 to 747 692 8.0Iron 0.014 667 to 677 672 0.8Molybdenum 0.0149 188 to 220 205 8.3Monel 0.010 348 to 437 396 12.0Nickel 0.008 0.0155 0.0154 0.01521168 1096 1219 10841162 6.0Stainless Steel 302 0.020 570 to 796 681 13.0Tungsten 0.0153 260 to 332 283
12、 18.0Table 1. Ignition Temperatures of Metals in Fluorine-Concluded (a) Technique B Metal Wire diameter, (in)Max wire temperature CIgnition delay, secIgnition temp range CActivation energy, kcal/moleCopper 0.012 905 852 810 767 701 6890.8 1.0 0.6 0.8 1.2 No ignition689 to 701 39.5Iron 0.014 730 676
13、648 644 6181.0 1.6 2.0 2.2 No ignition618 to 644 16.3Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Nickel 0.015 1357 1306 1266 12530.6 1.2 0.6 No ignition1253 to 1266-The data for Table 1 was obtained from tests using two techniques, techniques A a
14、nd B. In technique A, an evacuated bomb was filled with gaseous fluorine at atmospheric pressure and the fluorine was increased in temperature by a heated wire. The temperature at which the wire burned is listed in the part of Table 1 for technique A. In technique B, the evacuated bomb was brought t
15、o temperature before fluorine introduction. The time required for the reaction to go to completion, the ignition delay, is listed in the part of Table 1 for technique B.In addition, Table 2 was produced from Reference 1 which shows an expanded list of materials and their reactive effects with fluori
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