NAVY MIL-C-85659-1984 CONTAINER SHIPPING AND STORAGE ALL UP ROUND CNU-398 E《CNU-398 E型运输储存集装箱》.pdf

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1、MIL-C-85659(AS) 21 November 1984 MILITARY SPECIFICATION CONTAINER, SHIPPING AND STORAGE, ALL UP ROUND CNU -398/E This specification is approved for use by the Naval Air Systems Command, Department of the Navy, and is available for use by all Departments and Agencies of the Department of Defense. 1.

2、SCOPE - . -. . -. . . 1.1 Scope. This specification establishes the requirements for the manufacture and acceptance of the CNU-398/E al 1 -up-round (AUR) container for the SIDEWINDER AIM-9 series missile, referred to herein as the container. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Sp

3、ecifscations, standards, and handbooks. Unless otherwise speci- fied, the following standards of the issue listed in that issue of the Depart- ment of Defense Index of Specifications and Standards (DoDISS) specified in the solicitation form a part of this specification to the extent specified herei

4、n. Beneficial comments (recommendations, additions, deletions) and any per- tinent data which may be of use in improving this document should be addressed to: Commanding Officer, Naval Air Engineering Center, Engil neering Specifscations and Standards Department (ESSD) Code 93, Lakehurst, New Jersey

5、 08733, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document FSC 8140 THIS DOCUMENT CONTAINS 1-3 PAGES Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-flIL-C-5b57 81 m 777790b

6、- 0270033 5 m - - MIL-C-85659 (AS) STANDARDS FEDERAL FED-STD-101 . Test Procedures for Packaging Materials MIL I TARY MIL-STD-454 M I L -S TD - 6 48 Standard General Requirements for Electronic Equipment Design Cri teri a for Special i zed Shipping Containers 2.1,2 Other Government documents, drawin

7、gs, and publications. The follow- ing Government drawings form a part of this specification to the extent speci fied herein. DRAW I NGS Naval Air Systems Command (Code Ident 30003) 129 73 23 . Sling 639AS2879 159 6AS 10 O 1596AS 104 159 6AS10 1 Dome Protector Assembly Container, Shipping and Storage

8、, CNU-398/E Upper She1 1 Assembly Cradle Assembly (Copies of specifications, standards, drawings, and publications required by manufacturers in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting officer. ) 2.1.3 Order of

9、precedence. In the event of a conflict between the text of this specification and the references cited herein, the text of this specification shall take precedence. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-85657 81 77777Ob 0270034 7 MI

10、L-C-85659 3. REQUIREMENTS 3.1 Container description. The container, which is of rectangular construction, includes an upper shell assembly and cradle assembly. The cradle assembly consista of a lower shell assembly and frame. A suspension system consisting of eight shock mounts is provided between t

11、he lower shell assembly and frame. for rapid securing and opening. shell assembly protected by dunnage. providing proper closure seal. assembly which can quickly be released for access to the missiles. sure relief valve is installed in the lower shell assembly. Skids, forklift pockets and lifting ey

12、es are provided in the frame to facilitate handling. 3.1.1 MaJor. The container shall consist of the following major components in accordance with Drawing 1596AS100: Fasteners are positioned around the periphery to provide The container is airtight with a gasket Wings and fins are carried in the low

13、er Missiles are held in place by a-retainer A pres- a. Cradle assembly (Drawing 1596AS101) o b. Upper shell assembly (Drawing 1596AS104). 3.2 First article. When specified, a sample shall be subjected to first article inspection see 4.4.1 and 6.3). 3.3 General Characteristicso The container shall ex

14、hibit the following genera 11 a. The container shall be reusable and shall furnish transporta- tion and storage protection for one to four SIDEWINDER all-up-round missiles (see 6.4.1) with storage included for one to four sets crf wings atid fins. b. The container shall not be pressurized for shipme

15、nt and storage. 3.4 Design and construction. Design and construction of the container shall be in accordance with Drawing 1596AS100 and as specified herein. 3.5 Performance requirements. The container shall meet all requirements Specified herein when loaded with one to four AIM-9 series missiles, in

16、cluding wings and fins. 3.5.1 Leakage. When tested in accordance with FED-STD-101, method 5009, Pneumatic pressure technique, container leakage as indicated by a drop in pressure shall be not greater than 0.05 pound per square inch gage (psig) per hour (see 4.8.1). 3 Provided by IHSNot for ResaleNo

17、reproduction or networking permitted without license from IHS-,-,-MIL-C-85657 81 a 7779706 0270035 7 H MIL-C-85659( AS) 3.5.2 Shock. When the container is tested in accordance with the fol lowing speci fi ed methods of FED-STD-101, the container shall meet the acceptance criteria of MIL-STD-648, Mec

18、hanical shock. a. Edgewise drop. The fully loaded container shall perform as specified herein when tested in accordance with FED-STD-101, method 5008 at -20 t5 degrees Fahrenheit (OF) and 140 - t5OF (see 4.8.2). specified herein when tested in accordance with FED-STD-101, method 5005 at -20 - t5“F a

19、nd 140 - t5OF (see 4.8.3). c. Repetitive shock. The fully loaded container shall perform as specified herein when tested in accordance with MIL-STD-648, Repetitive shock test; and MIL-STD-648, Repetitive shock test, using a superimposed load equal to four fully loaded containers (see 4.8.4). 3.5.3 V

20、ibration. with FED-STD-101, method 5020, there shall be no evidence of physical or func- tional damage to container or contents, and there shall be no shifting of contents (see 4.8.5). with FED-STD-101, method 5012, or method 5023, at -20 t5OF and 140 t5OF; the container chal 1 meet the acceptance c

21、riteria of MIL-STD-648, MechanTcal shock (see 4.8.6). accordance with FED-STD-101, method 5016, there shall be no evidence of phys- ical or functional damage to stacking features or other container features, or shifting of contents. result in any unsafe configuration or condition shall be cause for

22、rejection of the container (see 4.8.7). 3.5.6. Mechanical hand1 ing. When the fully loaded container is tested in accordance with FED-STD-101, method 5011, Lifting and transporting by forklift truck, Hoisting with slings, Pushing, and Towing; there shall be no evidence of physical or functional dama

23、ge to container handling features or other container features, or damage to or shifting of contents (see 4.8.8). b. Cornerwise drop. The fully loaded container shall perform as When the fully loaded container is tested in accordance 3.5.4. Impact. When the fully loaded container is tested in accorda

24、nce 3.5.5 Superimposed load. When the fully loaded container is tested in . Temporary or permanent deformation sufficient to 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-85659 81 m 9799906 0290036 O m 3.5.7. HQis%ing. When the container is

25、 suspended by? its lifting eyes and - tested in accordance with MIL-STD-648, Hoisting strength test, there -shall be no evidence of structural or functional damage to the lifting eyes (see 4.8.9). 3.5.8 Stackgd. bihen the fully loaded container, in unitized? shipping configuration, is tested in acco

26、rdance with MIL-STD-648, Impact test (stacked), there shall be no evidence of failure of the connecting structures which would permit any of the containers to become unattached (see 4.8.10). 3.5.9 Shipboard shock. When the fully loaded container is tested in accordant-648, Shipboard shock test (elig

27、ibility), using a freefall drop height of 18.0 +1.5 inches; there shall be no evidence of physical or functional damage-to container or contents and there shall be no shifting of contents (see 4.8.11). 3.6. Reliability. Container shall be capable of 20 openings and closings with no evidence of physi

28、cal or functional damage or evidence of wear that would require the replacement of any container component (see 4.11). 3.4. Configuration control. Unless otherwise specified in the contract or purchase-he contractor shall submit a supplemental sample to the procQring activity for appropriate inspect

29、ions whenever a change is authorized by the procuring activity . 3.8 Government-1 oaned property. Unless otherwise speci f ied in the con- tract o-cha-11, the following property will be loaned to ?the contractor by the Government (see 6.5): Four SIDEWINDER dummy rounds with wings and fins. a. b. Fou

30、r dome protectors (see Drawing 639AS2879). c. Two slings (see Drawing 1297323). 3.9 Workmanship. Workmanship shall be in accordance with MIL-STD-454, Requirement 9, and the following. The container shall be constructed and finished in a manner to ensure compliance with all requirements specified her

31、ein. assembly inciucling construction of interface assemblies. areas shall be free of excessive weld, weld splatter, voids, and excessive Particular attention shall be paid to neatness and thoroughness of The gasket cavity 5 Provided by IHSNot for ResaleNo reproduction or networking permitted withou

32、t license from IHS-,-,-11_1 MIL-C-85659Bx-m 9999906 0290037 2 m - - - MI L-C-85659 (AS ) marks due to smoothing of welds. The coating and finish shall be even and neat, and the container shall be free of burrs and sharp edges. The standards of workmanship exhibited in any approved first article samp

33、les, subject to any qualifications stated in the Government notice of approval, shall establish the minimum workmanship standards for production items where such workmanship i s not spec1 f i cal 1 y covered, by appl i cab1 e standards ( see 4.12) . - 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibili

34、ty for inspection. Unless otherwise specified in .the contract or purchase order, the contractor is responsible for the performance of all inspection requirements as specified herein. Except as otherwise specified in the contract or purchase order, the contractor may use his own or any other facilit

35、ies suitable for the performance of the inspection requirements specified herein, un1 esc di sapproved by the Government. Government reserves the right to perform any of the inspections set forth in this specification where such inspections are deemed necessary to assure supplies and services confor

36、m to prescribed requirements. fied herein are classified as follows: The 4.2 Classification of inspections. The inspection requirements speci- a. b. c. First article inspection (see 4.4). Qual i ty conformance inspection (see 4.5). Product verification inspection (see 4.6). 4.3 Inspection conditions

37、. Unless otherwise specified herein, all inspec- tions shall be performed in accordance with the test conditions specified in 4.3.1. 4.3.1 Test conditions. Test conditions for inspections shall be the tem- perature, pressure and humi di ty condi ti ons ambient to the testi ng faci 1 i ty . 4.4 First

38、 article inspection. Unless otherwise specified in the contract or purchase order (see 6.2.1), the container shall be subjected to the first article inspection of Table I. designated testing facility specified in the contract or purchase order The first article shall be inspected at a 6 Provided by

39、IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-85b57 3 H 7777706 0290038 4 MI L-C-85659 (AS) TABLE I. First article, quality conformance, and product verification inspections. Exami nation or test . First Article inspection Design and construction Leak ag

40、e Edgewi se drop Cornerwi se drop Repeti tive shock Vi bration Impact Superimposed load Mechanical handl i ng Hoi s ti ng Stacked impact Shipboard shock Re1 i abi 1 i ty Work ma ns h i p I. Qual i ty conformance inspection Workmanship Le aka ge :. Product verification i nspecti on Design and constru

41、ction Leakage Edgewi se drop Cornerwi se drop Repetitive shock Vi brati on Impact Superimposed load Mechani cal handl i ng Hoisting Stacked impact Shipboard shock Reliability Morkmanship Requirement paragraph 3.4 3.5.1 3.5.2a 3.5.2b 3.5.2 3.5.3 3.5.4 3.5.5 3.5.6 3.5.7 3.5.8 3.5.9 3.6 3.9 3.9 3.5.1 3

42、.4 3.5.1 3.5.2a 3.5.2b 3.5.2 3.5.3 3.5.4 3.5.5 3.5.6 3.5.7 3.5.8 3.5.9 3.6 3.9 Method paragraph 4.9 4.8.1 4.8.2 4.8.3 4.8.4 4.8.5 4.8.6 4.8.7 4.8.8 4.8.9 4.8.10 4.8.11 4.11 4.12 4.12 4.8.1 4.9 4.8.1 4.8.2 4.8.3 4.8.4 4.8.5 4.8.6 4.8.7 4.8.8 4.8.9 4.8.10 4.8.11 4.11 4.12 7 Provided by IHSNot for Resa

43、leNo reproduction or networking permitted without license from IHS-,-,-MIL-C-85657 83 7777706 0270039 6 MIL-C-85659 (AS I (see 6.2.1). inspection shall be cause for rejection of the first article. of containers prior to first article approval shall be at the. contractors risk. Failure of the first a

44、rticle sample to pass the first article Any production 4.4.1 First article sample. The first article sample shall consist of two containers. The first article sample shall be representative of the methods, materials, processes and parts the contractor proposes to use in production of the container.

45、4.4.2 First article data. The contractor shall generate test reports documenting all tests of the first article inspection (see 6.2.2). shall include complete details of the nature of the tests, test methods, test equipment, test results and result analyses. 4.5 Quality conformance inspection. The q

46、uality conformance inspection shall be as specified in Table I and shall be performed on 100 percent of the containers supplied under this specification. Failure of any container to pass the quality conformance inspection shall be cause for rejection of that -contai ner. Reports 46. Product verifica

47、tion inspection. The product verification inspection shall be as specified in Table I. 4.6.1 Acceptance lot size. The lot size for each lot submitted for acceptance shall be as specified in the contract or purchase order (see 6.2.1), but shall be not greater than 100 containers. 4.6.1.1 Sample inspe

48、ction lot size. The sample inspection lot size for each lot submitted for acceptance shall be one container which shall be selected at random. 4.6.2 Acceptance tests. Acceptance tests shall be performed by the Failure of the sample of a sample inspection lot to pass any contractor for each lot submi

49、tted for acceptance, lot shall be subjected to the product verification inspection specified in Table I. test of the product verification inspection shall be cause for rejection of that lot. 4.6.3 Acceptance data. The contractor shall generate test reports docu- menting all tests of the product verification inspection (see 6.2.2). Reports shall include complete details of the nature of the tests, test meth