ARMY MIL-M-64016-1983 MOTOR ROCKET METAL PARTS FOR AND LOADING ASSEMBLY FOR DEMOLITION KIT CRATERING M180《磨顶槽拆卸工具包用金属零件及其加载装置和火箭发动机 M180 t型》.pdf

《ARMY MIL-M-64016-1983 MOTOR ROCKET METAL PARTS FOR AND LOADING ASSEMBLY FOR DEMOLITION KIT CRATERING M180《磨顶槽拆卸工具包用金属零件及其加载装置和火箭发动机 M180 t型》.pdf》由会员分享，可在线阅读，更多相关《ARMY MIL-M-64016-1983 MOTOR ROCKET METAL PARTS FOR AND LOADING ASSEMBLY FOR DEMOLITION KIT CRATERING M180《磨顶槽拆卸工具包用金属零件及其加载装置和火箭发动机 M180 t型》.pdf（24页珍藏版）》请在麦多课文档分享上搜索。

1、MIL-M-640Lb 13 7779706 0352730 I T -. 19 WRCH 1983 MILITARY SPECIFICATION MOTOR, ROCKET, METAL PARTS FOR AND LOADING ASSEMBLY FOR DEMOLITION KIT, CRATERING: M180 This specification is approved for use by U.S. Army Armament Research andbevelopment Command, and is available for use by all Departments

2、and Agencies of the Department of Defense. 1. SCOPE 1.1 - Scope. - This specification covers quality assurance provisions and preparation for delivery for the metal parts and loading assembly of the rocket motor for Demolition Kit, Cratering: M180. 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2

3、.1.1 Specifications and standards. Unless otherwise specified (see 6.1), the following specifications and standards of the issue listed in that issue of the Department of Defense Index of Specifications and Standards (DoDISS) specified in the solicitation, form a part of this specification to the ex

4、tent specified herein. SPECIFICATIONS FEDERAL PPP-B-585 - Box, Wood, Wirebound. PPP-B-601 - Boxes, Wood, Cleated Plywood. PPP-B-621 - Box, Wood, Nailed and Lock Corner. PPP-B-636 - Boxes, Shipping, Fiberboard. PPP-C-843 - Cushioning Material, Cellulosic. QQ-S-781 - Strapping, Steel, and Seals. MILIT

5、ARY MIL-P-116 - Preservation, Methods of. MIL-P- 117 - Bag, Sleeve and Tubing, Interior Packaging. MIL-1-6868 - Inspection Process, Magnetic Particle. MIL-A-48078 - Ammunition, Standard Quality Assurance Provisions, General Specification for. Beneficial comments (recommendations, additions, deletion

6、s) and any pertinent data which may be of use in improvin this document should be addressed to: Commander, US Army Armament fiesearch and Develo ment Command, Attn. DRDAR-QA, Dover, New Jersey 07801 by using t!e self-addressed Standardization Document Improvement Proposal (DD Form 1428) appearing at

7、 the end of this document or by letter. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-60L6 13 W 7977706 0352732 3 MIL-I- 4 8 110 - MIL-P-50202 - STANDARDS MIL I TA RY MIL-STD-105 - MIL-STD- 12 9 - MIL-STD- 410 - MIL-STD-1188 - MIL-M-64016 (AR

8、) Igniter Assembly, Rocket, for Demolition Kit, Cratering, M180. Propellant Charge, Rocket, for Demolition Kit, Cratering, M180. Sampling Procedures and Tables for Inspection by Attributes. Marking for Shipment and Storage. Nondestructive Testing Personnel Qualification and Certification. Commercial

9、 Packaging of Supplies and Equipment. 2.1.2 Other Government documents, drawings, and pubJications. - The following other Government documents, drawings, and publications form a part of this specification to the extent specified herein. DRAWIVGS (See 6.5) US ARMY ARMAMENT RESEARCII AND DEVELOPMENT C

10、OMMAND 9329589 - Rocket Motor Assembly. 9329725 - Packing and Marking For Box, Fiberboard For 9329726 - Packing and Marking For Box, Packing For Box, 9340544 - Packing and Marking For Box, Packing For Box, Rocket Motor Assembly or Rocket Motor and Detonator Assembly. Fiberboard For Rocket Motor and

11、Detonator Assembly or Rocket Motor Assembly. Fiberboard For Rocket Motor and Detonator Assembly or Rocket Motor Assembly. (Copies of specifications, standards, handbooks, drawings, and publications required by manufacturers in connection with specific acquisition functions should be obtained from th

12、e contracting activity or as directed by the contracting officer.) 2.2 Other publications. The following document(s1 form a part - of this specification to the extent specified herein. The issues of the documents which are indicated as DoD adopted shall be the issiie listed in the current DoDISS and

13、 the supplement thereto, if applicable. AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM E 18 (Part 10) - Rockwell Hardness and Rockwell ASTM B 117 (Part 10)- Salt Spray (Fog) Testing. Superficial Hardness of Metallic Materials. 2 Provided by IHSNot for ResaleNo reproduction or networking perm

14、itted without license from IHS-,-,-MIL-M-64016 (AR) Application for copies of ASTM publications should be addressed to the American Society for Testing and Materials, 1916 Race Street, Philadelphia, Pennsylvania 19103.) 2.3 - Order of precedence. - In the event of a conflict between the text of this

15、 specification and the references cited herein, the text of this specification shall take precedence. 3. REQUIREMENTS 3.1 Material. - Materials shall be in accordance with the applicable drawings, specifications and standards. 3.2 Parts. All parts shall comply with applicable drawings, specification

16、s and standards. 3.3 Rocket motor assembly. The rocket motor assembly shall -I- comply with all requirements specified on Drawing (Dwg.) 9329589, - all associated drawings, and with all requirements specified in applicable specifications and standards. 3.4 Magnetic particle inspection (Motor Assembl

17、y Weld) . The - - - -_-_ -_ motor assembly weld shall show no evidence of voids, slag deposits, cracks or crack-like indications when tested as specified in 4.5.3. 3.5 Weldinq. - All welds shall be reasonably smooth and free of craters. They shall exhibit characteristics of good fusion, penetration,

18、 and soundness of deposit representative of good welding practice. The process shall be such as to prevent warpage and distortion. There shall be no crack in or near welded areas. 3.6 - First article inspection. -_ This specification contains technical provisions for first article inspection. Requir

19、ements for the submission of first article samples by- the contractor shall be as specified in the contract. 3.7 Workmanship. I- All parts and assemblies shall be fabricated, loaded and assembled in a thorough, workmanlike manner. They shall be free of burrs, sharp edges, cracks, gouges, dirt, greas

20、e, rust, and other foreign matter. After loading, all external surfaces, including cavities, shall be free from explosive. The cleaning method used shall not be injurious to any parts, nor shall the parts be contaminated by the cleaning agents. Exterior surface coatings shall be continuous, however,

21、 a few light scratches not exposing base metal may be permitted. All required marking and stamping shall be neat and sharply defined. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-M-6901b 13 7797706 0352733 7 H MIL-M-64016 (AR) 4. QUALITY AS

22、SURANCE PROVISIONS 4 1 RecPonsibiiltY-_for-cPi-Y - assurance Erovisions. - Unless otherwise specified herein or in the contract, the provisions of MIL-A-48078 shall apply and are hereby made a part of this detail specification. 4.2 Classification of inspections. - The inspection requirements specifi

23、ed herein are classified as follows: a. First article inspection (see 4.3). b. Quality conformance inspection (see 4.4). 4.3 First article inspection. - 4.3.1 - Submission. The contractor shall submit a first article sample as designated by the Contracting Officer for evaluation in accordance with p

24、rovisions of 4.3.2. The first article sample shall consist of the following items in sample quantities as indicated below and Table I. Head, Rocket 9244407 5 Plate, Retainer, Rocket 9244408 5 Nozzle, Motor Case 9244439 5 Case, Motor 9244440 5 Rocket Motor Case Assembly 9244441 5 Charge Assembly (Pro

25、pellant) 9329587 10 Rocket Motor Assembly 9329589 10 4.3.2 - Inspections - to be performed. - See MIL-A-48078 and Table I specified herein. 4.3.3 - Rejection. - See MIL-A-48078. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-6401b 13 = 77777

26、06 035273LI 7 ci u al W al Fi k rl a IR rn Q, 8 4 ci ci a, A! u O p: uci ci ci au u u Yo) al al UU U U oal alal al an 21 Q n . cv m w cvh) cv cv wu, w w www ww w w rl cvrlh) .;ruiu, . . . .e . . . . NN N cv mm m m CVNCU mmm e 5 Provided by IHSNot for ResaleNo reproduction or networking permitted wit

27、hout license from IHS-,-,-MIL-M-6401b 13 = 7777706 0352735 O k- b . H w cl m cvcvmw cv cv mmmm m m .*.o . b 8 4 U u rn c H a, rl Uu rn .4 aJU BQ m 6 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-64016 (AR) 4.4 Quality conformance inspection.

28、0.4.1 Inspection lot formation. Inspection lots shall comply with the lot formation provisions of MIL-A-48078. In addition, each lot shall contain: a. Igniter assemblies of one lot interfix number from one manufacturer. (See 4.4.5) b. Propellant charge of one lot interfix number from one manufacture

29、r and complying with MIL-P-50202. 4.4.2 Examination. See MIL-A-48078. a. Sampling plans. Unless otherwise specified in the classification of Defects and Tests Tables, sampling plans and procedures for major and minor defects shall be in accordance with MIL-STD-105, Inspection Level. II. 7 Provided b

30、y IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-640Lb 13 m 9777706 0352737 V m ZI o1 u a, A! ffi 5 Id al m 8 b crl E 3( a al c .FI w a, o a, c O z 5 a, n- oi IDID- a -w 5 c mv) m 5 atum rlrla, a, 004 u cc0 m 5 8 Y cw am Li i565 s a aaaJaJv) m afia3 u4J m

31、 o o mmaoa 2 a, al c-ri 3 o a, 4JuoLiuoc 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-b4016 13 = 777770h 0352738 b ts rl CI a, Y u O v . LI a, C .I+ m -lJ 2 b ci m rl pi dPdPdpdPaadPcJP dPdP 00000000 m mdP I *-r*-r w wo 00000000 o orl e. .

32、 n m Y ro a, C 4 rcI a, CI a, c O 2 rl rdl 9 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-640Lb 13 m 7777706 0352737 m (v(vN(v (v N(vP mmmm m mmm .e . dpdpdpdp dP dpdp O000 o Lnrndp * * wwo O000 o 004 .a 0 . a a, E .d UJ a, a a, c O z a, a m

33、i U1 .4 LirlNrn*lVI Lirlcvm u 000000 O000 .d *rrl rl rl d rl chinini .?I u/:I XI 10 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-U-640Lb 13 7777706 0352740 4 M d Id Ld 8 c ci h ai II) u m rl rl cvcvcvcvcvcv cv cv cvl- mmmmmm m m mm . e. , d6dP

34、dPdPdPdP dp 000000 o Ln LndP *e* * w wo 000000 o o orl e. . 0 0. o ai C -4 w ai W ai z 8 ci Class 2, Style 4, PPP-B-621 boxes; or Class 3, Style 2 or 3, PPP-B-585 boxes. Closure and strapping shall be in accordance with applicable container specifications except strapping shall conform to Type I or

35、IV, Finish A, QQ-S-781. 5.6.2 - Level B. Level B packing shall be as specified in 5.6.1. 5.6.3 - Level C. The Rocket Motor Assembly shall be packed in accordance with Dwg. 9329726 or 9340544, as applicable. 5.6.4 Commercial. - Commercial packaging shall be in accordance with MIL-STD-1188, except the

36、 Rocket Motor Assembly shall not be packed commercial. 5.7 Marking. I- 5.7.1 - Level A. Marking shall be in accordance with MIL-STD-129. 5.7.2 - Level B. Marking shall be in accordance with MIL-STD-129. 5.7.3 - Level C. Marking shall be in accordance with MIL-STD-129, Dwg. 9329726 or 9340544, as app

37、licable. 5.7.4 _-_- Commercial. Marking shall be in accordance with MIL-STD-1188. 5.8 Shipping. When assemblies from more than one lot are shipped at one-time, each lot shall be kept separate and the division between lots clearly indicated to prevent mixing of lots in transit. 6. NOTES 6.1 - Orderin

38、g - data. See MIL-A-48078. 6.2 Submission of inspection equipment des9ns for approval. (See MIL-A-48078). Equipment designs shall be submitted as required to: Commander, U .S. Army Armament Research and Development Command, ATTN: DRDAR-QAT-I, Dover, New Jersey 07801. Request letter of submittal shou

39、ld state contractor, contract number, specification number, item nomenclature, and classification of defects and tests paragraph number. - - - - - - 23 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-M-64016 (AR) 6.3 Cost - of check test. The con

40、tracting officer will arrange for the contractor to be reimbursed for the expense incurred in the performance of the check test for deterioration of the igniter assemblies. The tests shall be conducted at Government expense without cost to the contractor who loaded the igniter assemblies or to the c

41、ontractor assembling the igniter assemblies into the rocket motors; and shall not constitute a basis for rejection against either contractor except where deterioration has occurred as a direct result of carelessness in handling, storagec etc., permitted while the igniter assemblies lot was under the

42、 jurisdiction of either contractor. 6.4 - Data cards. (See MIL-A-48078). Distribution of data cards shall include the following: Commander, U.S. Army Armament Research and Development Command, ATTN: DRDAR-QAT-M, Dover, New Jersey 07801. 6.5 - Drawigs. Drawings listed in Section 2 of this specificati

43、on under the heading US Army Armament Research and Development Command (ARRADCOM) may also include drawings prepared by, and identified as, Edgewood Arsenal, Frankford Arsenal, Rock Island Arsenal or Picatinny Arsenal drawings. Technical data originally prepared by these activities are now under the cognizance of ARRADCOM. Custodian: Army-AR Preparing activity: Army-AR (Project 1375-A252) * US. GOVERNMENT PRINTING OFFICE: 1983-605-034/2203 24 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-