NAVY MIL-T-15089 C-1974 TUBING ALUMINUM ALLOY ROUND SEAMLESS (FOR ROCKET MOTORS)《火箭发动机无缝球状铝合金管道》.pdf
《NAVY MIL-T-15089 C-1974 TUBING ALUMINUM ALLOY ROUND SEAMLESS (FOR ROCKET MOTORS)《火箭发动机无缝球状铝合金管道》.pdf》由会员分享,可在线阅读,更多相关《NAVY MIL-T-15089 C-1974 TUBING ALUMINUM ALLOY ROUND SEAMLESS (FOR ROCKET MOTORS)《火箭发动机无缝球状铝合金管道》.pdf(8页珍藏版)》请在麦多课文档分享上搜索。
1、, PROPOSED MILITARY SPECIFICATION. . MIL-T-15089C (OS) 13 September 1974 SUPERSEDING MIL-T-15089B (Nord) 27 April 1959 TUBING, ALUMINUM ALLOY, ROUND, SEAMLESS (FOR ROCKET MOTORS) This specification is approved for use by all departments and agencies of the Department of Defense. 1. SCOPE AND CLASSIF
2、ICATION - 1.1 Scope. This specification covers aluminum alloy, seamless, round tubing for use in the manufacture of rocket motors. * 1.2 Classification. The tubing shall be of the following alloys, tempers, and classes as specified (see 6.1): Alloy 2014 - T6 or T65 11 Aiioy 2024 - T8 1 or T85 1 1 c
3、Nominal size (inches) (inches) - Class Outside diameter Wall thickness 1 2 3 4 5.25 5 .o0 2.75 2.00 0.292 0.138 0.072 0.060 )FSC- Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-15089C Li7 W 777790b 0272025 T m MIL-T-15089C (OS) 2. APPLICABLE D
4、OCUMENTS 2.1 The following documents of the issues in effect on date of invitation for bid or request for proposals form a part of this specification to the extent specified herein. SPECIFICATIONS Military MIL-H-6088 STANDARDS Federal *FED-STD-15 1 *FED-STD-245 Militarv MIL-STD-649 DRAWINGS Navy Dep
5、artment Heat Treatment of Aluminum Alloys; Process for (for Aircraft Applications) Metal, Test Methods Tolerance for Aluminum Alloy and Magnesium Alloy Wrought Products Aluminum and Magnesium Products, Preparation for Shipment and Storage If required by the contract or order, applicable drawings for
6、 the finished rocket motor form part of this specification (see 6.1 ). (Copies of specifications, standards, drawings, and publications required by suppliers in connection with specific procurement functions should be obtained from the procuring activity or as directed by the contracting officer.) *
7、2.2 Other publications. The following document forms a part of this specification to the extent specified herein. Unless otherwise indicated the issue in effect on date of invitation for bids or request for proposal shall apply. i 2 T I Provided by IHSNot for ResaleNo reproduction or networking perm
8、itted without license from IHS-,-,- MIL-T-L.5087C 47 W 7377906 O272026 L W i MIL-T-15089C (OS) American Society for Testing and Materials ASTM E 8 Standard Method of Tension Testing of Metallic Materials (Application for copies should be addressed to the American Society for Testing and Materials, 1
9、9 16 Race Street, Philadelphia, Pa. 19 103.) 3. REQUIREMENTS 3.1 Chemical composition. The chemical composition shall conform to the requirements given in table 1. *Table I CHEMICAL COMPOSITION I Alloy 20 14 t7GT Element Copper Magnesium Manganese Silicon Iron Chromium zinc Titanium Titanium plus zi
10、rconium Others (each)l Others (total) Aluminum 3.9 0.20 0.40 0.50 - - - _. -. - - Ren (%, max.) 5.0 O. 8 1.2 1.2 0.7 0.10 0.25 0.1 5 0.20 0.05 0.15 nder Alloy 2024 (%, min.) - - Rem (%, max.) 4.9 1.8 0.9 0.50 O. 50 0.10 0.25 0.10 0.25 0.05 0.15 Under lAnalysis shall regularly be made only for the el
11、ements specifically mentioned in the above table. If, however, the presence of other elements is indicated in the course of routine analysis, further analysis shall be made to determine that these other elements are not present in excess of 0.05 percent each, and that the total of these other elemen
12、ts does not exceed 0.15 percent. The material shall not contain these other elements in excess of the above limits. 3.2 Heat treatment. 3.2.1 Process. The process for heat treatment shall be in accordance with the requirements of MIL-H-6088, except as modified herein. 3.2.2 Corrosion. Tubing shall n
13、ot show presence of excessive intergranular attack when tested in accordance with 4.5.2. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-I MIL-T-LSOBSC 47 W 7797706 0272027 3 W Class All 1 2,394 MIL-T-15089C (OS) Tensile strength (psi, min) 60,000
14、66,000 64,000 3.3 Mechanical properties. Tubing shall conform to the minimum requirements shown in table II. *Table II MECHANICAL PROPERTIES Alloy ana temper 2014-T651, T6511 2024-T8 1, T85 1 1 Yield strength at 0.2% offset (psi, min) Elongation in 2 inches (%, min) 53,000 58,000 56,000 7 5 4 *3.4 I
15、nternal hydrostatic pressure. When specified, tubing shall be capable of conforming to the hydrostatic pressure test requirements specified on the applicable drawings for the fuished rocket motor (see 6.1 ). *3.5 Dimensional tolerances. Unless otherwise specified, tolerances shall conform - to FED-S
16、TD-245. 3.6 Marking. Each length-of tubing shall be legibly marked parallel to the axis of the tubing at intervals not to exceed nominal length for the finished rocket motor tube (see 6.1). Marking fluid shall be such that the markings produced shall not be removable by normal handling. Marking shal
17、l include the following: a. Manufacturers name or trademark b. Number of this specification c. Class number, alloy, and temper designation d. Lot number tubing *3.7 Workmanship. The tubing shall be seamless and uniform in quality and temper. The exterior and interior surfaces shall be clean, smooth,
18、 and free from slivers, laminations, folds, grooves, cracks, and other injurious defects within the limits consistent with the best commercial practice. Discoloration due to thermal treatment will not be cause for rejection. *4. QUALITY ASSURANCE PROVISIONS *4.1 Responsibility for inspection. Unless
19、 otherwise specified in the contract or purchase order, the supplier is responsible for the performance of all inspection requirements as specified herein. Except as otherwise specified in the contract or order, the supplier may use 4 Provided by IHSNot for ResaleNo reproduction or networking permit
20、ted without license from IHS-,-,-MIL-T-L5089C LI7 m 9997706 0272028 5 m I MIL-T-15089C (OS) his own or any other facilities suitable for the performance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the insp
21、ection set forth in the specification where such inspections are deemed necessary to assure supplies and services conform to prescribed requirements. , *4.2 Sampling. *4.2.1 Lot. A lot shall consist of an identifiable quantity of tubing of the same alloy, temper, and class, traceable to a heat treat
22、 lot or lots, and subjected to inspection at one time. *4.2.2 Sampling for chemical analysis. *4.2.2.1 ingot analysis. At least one sample shall be taken from each group of ingots of the same alloy poured simultaneously from the same source of molten metal by the producer and analyzed to determine c
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