ASTM D2512-1995(2002)e1 Standard Test Method for Compatibility of Materials with Liquid Oxygen (Impact Sensitivity Threshold and Pass-Fail Techniques)《材料与液氧兼容性标准试验方法(冲击敏感阀与可靠性技术)》.pdf
《ASTM D2512-1995(2002)e1 Standard Test Method for Compatibility of Materials with Liquid Oxygen (Impact Sensitivity Threshold and Pass-Fail Techniques)《材料与液氧兼容性标准试验方法(冲击敏感阀与可靠性技术)》.pdf》由会员分享,可在线阅读,更多相关《ASTM D2512-1995(2002)e1 Standard Test Method for Compatibility of Materials with Liquid Oxygen (Impact Sensitivity Threshold and Pass-Fail Techniques)《材料与液氧兼容性标准试验方法(冲击敏感阀与可靠性技术)》.pdf(13页珍藏版)》请在麦多课文档分享上搜索。
1、Designation: D 2512 95 (Reapproved 2002)e1Standard Test Method forCompatibility of Materials with Liquid Oxygen (ImpactSensitivity Threshold and Pass-Fail Techniques)1This standard is issued under the fixed designation D 2512; the number immediately following the designation indicates the year ofori
2、ginal adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. Asuperscript epsilon (e) indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the Department of
3、Defense.e1NOTEAdjunct references were corrected editorially in June 2006.1. Scope1.1 This method2,3,4covers the determination of compatibil-ity and relative sensitivity of materials with liquid oxygenunder impact energy using the Army Ballistic Missile Agency(ABMA)-type impact tester. Materials that
4、 are impact-sensitivewith liquid oxygen are generally also sensitive to reaction byother forms of energy in the presence of oxygen.1.2 This standard should be used to measure and describethe properties of materials, products, or assemblies in responseto heat and flame under controlled laboratory con
5、ditions andshould not be used to describe or appraise the fire hazard orfire risk of materials, products, or assemblies under actual fireconditions. However, results of this test may be used aselements of a fire risk assessment which takes into account allof the factors which are pertinent to an ass
6、essment of the firehazard of a particular end use.1.3 This standard does not purport to address all of thesafety concerns, if any, associated with its use. It is theresponsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of r
7、egulatory limitations prior to use.2. Referenced Documents2.1 ASTM Standards:C 145 Specification for Solid Load-Bearing Concrete Ma-sonry Units5D 1193 Specification for Reagent Water62.2 Military Standards:MIL-D-16791G Detergent, General Purpose (Liquid, Non-ionic)7MIL-P-27401C Propellant Pressurizi
8、ng Agent, Nitrogen7MIL-PRF-25508F Propellant, Oxygen7MIL-T-27602B Trichloroethylene, Oxygen PropellantCompatible8MIL-C-81302D Cleaning Compound, Solvent, Trichlorotri-fluorocarbon72.3 ASTM Adjuncts:Type Impact Tester and Anvil Region Assembly, 38 Draw-ings93. Summary of Test Method3.1 A sample of th
9、e test material is placed in a specimencup, precooled and covered with liquid oxygen, and placed inthe cup holder located in the anvil region assembly of theimpact tester. A precooled striker pin is then centered in thecup. The plummet is dropped from selected heights onto thepin, which transmits th
10、e energy to the test specimen. Observa-tion for any reaction is made and the liquid oxygen impactsensitivity of the test material is noted. Drop tests are continuedusing a fresh specimen cup and striker pin for each drop, until1This test method is under the jurisdiction of ASTM Committee G04 onCompa
11、tibility and Sensitivity of Materials in Oxygen Enriched Atmospheres and isthe direct responsibility of Subcommittee G04.01 on Test Methods.Current edition approved Feb. 15, 1995. Published April 1995. Originallypublished as D 2512 66. Last previous edition D 2512 82 (1994)e1.2“NASA Handbook 8060. 1
12、B, Ambient LOX Mechanical Impact ScreeningTest,” September 1981, pp. 4-53 through 4-71. “Oxygen Systems.” George C.Marshall Space Flight Center, National Aeronautics and Space Administration.Specification MSFC 106B. September 1981.3“Lubrication and Related Research and Test Method Development for Av
13、iationPropulsion Systems.” Technical Report No. 59-726. Wright Air DevelopmentDivision, January 1960.4“General Safety Precautions for Missile Liquid Propellants.”5Annual Book of ASTM Standards, Vol 04.05.6Annual Book of ASTM Standards, Vol 11.01.7Available from Standardization Documents Order Desk,
14、Bldg. 4 Section D, 700Robbins Ave., Philadelphia, PA 19111-5098, Attn: NPODS.8Cancelled in 1983. Previously available from Standardization DocumentsOrder Desk, Bldg. 4 Section D, 700 Robbins Ave., Philadelphia, PA 19111-5098,Attn: NPODS.9Detailed drawings for the ABMA-Type Impact Tester and Anvil Re
15、gionAssembly are available from ASTM International Headquarters. Order AdjunctADJD2512.1Copyright ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, United States.the threshold valve is achieved. A series of drop tests areconducted at an energy level of 98 J (7
16、2 ftlbf) or as specifiedfor the pass-fail tests.4. Significance and Use4.1 When this test method is used to measure the thresholdimpact sensitivity of a material, a relative sensitivity assess-ment is obtained which permits the ranking of materials.4.2 This test method may also be used for acceptanc
17、e-testing materials for use in liquid oxygen systems. Twentyseparate samples of the material submerged in liquid oxygenare subjected to 98 J (72 ftlbf) or as specified. Impact energydelivered through a 12.7-mm (12-in.) diameter contact. Morethan one indication of sensitivity is cause for immediatere
18、jection. A single explosion, flash, or other indication ofsensitivity during the initial series of 20 tests requires that anadditional 40 samples be tested without incident to ensureacceptability of the material.4.3 The threshold values are determined by this test methodat ambient pressure. The sens
19、itivity of materials to mechanicalimpact is known to increase with increasing pressure. Sincemost liquid oxygen systems operate at pressures above ambientcondition, some consideration should be given to increasedsensitivity and reactivity of materials at higher pressure whenselecting materials for u
20、se in pressurized system.5. Apparatus5.1 ABMA-Type Impact Tester9(Fig. 1 , See ADJD2512),for determining the sensitivity of materials to liquid oxygenwith impact energy. Fig. 2 shows the schematic diagram of thetypical power supply. The tester consists of the following parts:5.1.1 Three Guide Tracks
21、, capable of maintaining accuratevertical alignment under repeated shock conditions.5.1.2 Plummet, with a weight of 9.072 6 0.023 kg (20 60.05 lbs).5.1.3 Safety Catch, operated by a solenoid, and designed tohold the plummet near the base of the magnet. It is used tosupport the plummet in the event o
22、f a power failure.5.1.4 Electromagnet, for supporting or releasing the plum-met. The electromagnet is designed to hold 9.072 kg (20 lbs) ofweight with a minimum amount of electrical energy.5.1.5 BaseThe base of the tester is composed of thefollowing: a rigid 0.61- by 0.61- by 0.61-m (2- by 2- by 2-f
23、t)(min) reinforced concrete block (concrete conforming to Speci-fication C 145), a 3.2-mm (18-in.) stainless steel sheet, and a25-mm (1-in.) thick stainless steel base plate. Four stainlesssteel foundation bolts protruding from the concrete block areused to fasten the plate and sheet to the smooth s
24、urface of theconcrete block with stainless steel nuts.NOTE 1Where not otherwise indicated, stainless steel shall be of theAISI 300 series.5.1.6 Anvil Plate (Fig. 3), made from a 51-mm (2-in.) thickType 440B heat-treated steel plate, (56 to 58 HRC) that iscentered and rests on the base plate. It in t
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