ARMY MIL-C-48881 B-1983 CHARGE PROPELLING M205 LOADING ASSEMBLING AND PACKING《M205型装药推进器的装卸 组装和包装》.pdf

1、J - MIL-C-488BLB 33 7999706 0325339 b 5 -57-05 - MIL-C-48881B (AR) 11 March 1983 SUPERSEDING MIL-C-48881A 30 October 1978 MILITARY SPECIFICATION CHARGE, PROPELLING, M205 LOADING, ASSEMBLING AND PACKING This specification is approved for use by the US Army Armament Research and Development Command, a

2、nd is available for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 This specification covers requirements and quality assurance provisions for the loading, assembling and packing for the Charge, Propelling, M205 for use on the Cartridge, 81MM, HE, M374A3 and WP, M375A

3、3. k 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. Unless otherwise specified (seo 6.2), 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 s

4、olicitation, forms a part of this specification to the extent specified herein. SPECIFICATIONS MILITARY MIL-A-48078 - Ammunition, Standard Quality Assur- ance Provisions, General Specification for FSC 1315 I 1 Beneficial comments (recommendations, additions, deletions) and any pertinent data which m

5、ay be of use in improvin this document should be addressed to: Commander, US Army Armament iesearch and Develo ment Command, Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. Attn. DRDAR-QA, Dover, New Jersey 07801 by using t R e self-ad

6、dressed 1 I I P Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-48881B (AR) STANDARDS MILITARY MIL-STD-414 - Sampling Procedures and Tables for Inspection by Variables for Percent Defective 2.1.2 Other Government documents, drawings and publica

7、tions, The following other Government documents, drawings, and publica- tions form a part of this specification to the extent specified herein. - DRAWINGS (See 6.5) US ARMY ARMAMENT RESEARCH AND DEnLOPMENT COMMAND (ARRADCOM) 9278773 - Container Assembly 9280588 - Charge, Propelling, M205 I 9313721 -

8、 Packing and Marking for Box, Fiber- 9313756 - Packing for Pallet for Box, Fiberboard, board, Outer for Charge, Propelling, M205 or Container Assembly Outer for Charge Propelling M205 or Container Assembly (Copies of specifications, standards, handbooks, drawings and publications required by manufac

9、turers 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 precedence. In the event of a conflict between the text of this specification and the reference cited herein, the text of this specific

10、ation shall take precedence. 3. REQUIREMENTS 3.1 Materials. Materials shall be in accordance with the applicable drawings and specifications. 3.2 Assembly. The propelling charge assembly shall comply with all requirements specified on drawing 9280588 and associated drawings and with all requirements

11、 specified in applicable specifications and standards. 3.3 Gross weiqht of propelling charge. The weight of the loaded propelling charge shall not vary more than plus or minus 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C- 4 88 8 1B (AR) el

12、even grains from the assessed propellant weight plus the median drawing weight of the container assembly when tested as specified in 4.5.3. 3.4 Velocity. The propelling charges shall impart a corrected muzzle velocity of not more than 900 feet per second (fps) and not less than 870 fps when tested a

13、s specified in 4.5.4 (see 6.9). 3.5 First article inspection. This specification contains technical provisions for first article inspection. Requirements for the submission of first article samples by the contractor shall be as specified in the contract. 3.6 Workmanship. 3.6.1 Propelling charge. The

14、 propelling charge shall be free of dirt, grease or other foreign material. 3.6.2 Packaging. The packaging shall be free from foreign material. The boxes shall be assembled without undue binding and no flap shall project beyond the edge of the box when closed . 4. QUALITY ASSURANCE PROVISIONS 4.1 Re

15、sponsibility for inspection and standard quality assurance provisions. 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 following types of inspection shall b

16、e conducted on this item: a. First article inspection b. Quality conformance inspection 4.3 submission. The contractor shall submit a first article sample as designated by the contracting officer for evaluation in accordance with provisions of 4.3.2. The first article sample shall consist of the fol

17、lowing item in sample quantities as indicated. Part Description Drawing Quantity Charge, Propelling, M205 9280588 210 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-48881B (AR) 4.3.2 Inspections to be performed. See MIL-A-48078 and Table I s

18、pecified herein. 4.3.3 Rejection. See MIL-A-48078 (AR) . 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Tr m e . . ri ri . nI ntmm -r mmdi di* . . . . O O O0 rl oricv ri riri* u) 0 u a, w a, ru 8 lu c C .rl 0 a C .ri 5 x El 5 . n a, tri Tl .rl Li

19、0 k a u Li a, pi rJY Q) oi Li td c u di Y u) a, 0 u *I4 Li 0 & a u O m lu O a, tri Li m c u X . 2 a, c CI O CI 0 rl a 3 rl 3 0 a! u) rl 3 3 N K G Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-L. - I - - II MIL-C-98881B 13 77797Ob 032514Y T m MIL -C

20、- 4 8 8 8 1B (AR ) 4.4 Quality conformance inspection. 4.4.1 inspection lot formation. Inspection lots shall comply with the lot formation provisions of MIL-A-48078. In addition each inspection lot of propelling charges shall con ta i n: a. Container parts of one lot interfix from one manu- facturer

21、. b. Propellant from not more than one lot. 4.4.2 Examination. See MIL-A-48078. Unless otherwise specified in the Classification of Defects and Test Tables, sampling plans and procedures for major and minor defects shall be in accordance with MIL-STQ-105, Inspection Level II. 6 Provided by IHSNot fo

22、r ResaleNo reproduction or networking permitted without license from IHS-,-,-n u) In cr rl m I II 14 3 . . Y n In Ln cr 4 m I II) .rl 3 e . U rl m 7 II) *rl 3 4 . CJcum =Y ru W *o e 0.0 e o mmm m m m CJm ru mm m . x 2 a c m O a, +J tn a .m c II c Y z Li B u-l O a, u c a, m ?Id cum !=!I 7 Provided by

23、 IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-8 t * (um Um S4 O Li .al wc Li .rl am OU ac Li0 au a rl Li ho *u) xo ON Li- OP iwc oirl crl -4 al .Ya Li0 aLi cpi 5. cal atr Li trm cc -4 u .Y piiw mE: .ri $8 N N v b, . . . - rl m 1 m .I+ 3 rl m 1 m -4 3 rl a 1 m

24、 .FI 3 rl m 1 m -4 3 O0 o o O O W al c lH al W al c O 2 .ri a .ri c u) c a E 2 3 Li O O a lH O al u c al W 3 w 8 ri ? /- i 8 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-z O I? u w pi m H H w u z 2 P. u * I3 4 id: 3 O H h p: 4 Y a rl Co Co Co e I

25、u I 4 H x ci 6, rl rl w pi 8 4-I (r c .FI 2 u w pi M hl -F b! . . . *&a, O00 e* O00 0 rn a X O 11 % c -4 iu Q) a al c O z 9 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-4888lB (AR) 4.4.3 Testing. 4.4.3.1 Ve loc i ty . 4.4.3.1.1 First article

26、. The sampling plan for cartridges required and procedure/acceptance criteria for this test shall be in accordance with MIL-STD-414, Section B, Table B-3, Code Letter M and an AQL of 0.40 percent. The test shall be performed as specified in 4.5.4. 4.4.3.1.2 Production. 4.4.3.1.2.1 Beginning with the

27、 first lot produced and continuing until three consecutive lots of propelling charges have complied with the applicable requirements, the sampling plan and required procedures for cartridges for this test shall be in accordance with MIL-STD-414 Section BI Table B-3, Code Letter M and an AQL of 1.0 p

28、ercent. The test shall be performed as specified in 4.5.4. 4.4.3.1.2.2 After three consecutive lots have met the criteria of 4.4.3.1.2.1 the sampling plan for cartridges for this test shall be in accordance with MIL-STD-414, Section B, Table B-3, Code Letter II and an AQL of 1.0 percent. The test sh

29、all be performed as specified in 4.5.4. In the event of a lot rejection the sampling plan of 4.4.3.1.2.1 shall be required beginning with the next lot and continuing until three consecutive lots of propelling charges have complied with the applicable requirements. 4.4.4 Inspection equipment. The ins

30、pection equipment required to perform the examinations and tests prescribed herein is described in the “Paragraph Reference/Inspection Method“ column in the tables starting with paragraph 4.4.2.1. The contractor shall submit for approval inspection equipment designs in accordance with the terms of t

31、he contract. See Section 6 of MIL-A-48078 and 6.3 herein. 4.5 Test method and procedures. - 4.5.1 Weight of propellant. 4.5.1.1 Manual method. 4.5.1.1.1 Method 1. The propellant shall be weighed. Weight limits for weighing should be established within the applicable weight requirements, depending up

32、on the accuracy and precision of the weighing system to assure compliance with the charge weight requirements. Any charge of bulk propellant failing to meet the applicable requirement shall be classified defective and removed from the lot. 10 Provided by IHSNot for ResaleNo reproduction or networkin

33、g permitted without license from IHS-,-,-MIL-C-48881B (AR) 4.5.1.1.2 Method 2. Samples for this test shall be selected from propelling charges that have met the requirements of 3.3. A sample of 200 propelling charges shall be randomly selected during production for each shift. The propellant shall b

34、e removed from the charge, and weighed. If one or more critical defects or two or more major defects are found, the production represented by the sample shall be rejected. 4.5.1.2 Automated method. The contractor may elect to perform this operation with automated equipment and mandatory process cont

35、rols. The automated equipment shall weigh the container and place this weight in memory and then weigh/check- weigh the propellant before loading. After loading, the total weight of the container/propellant combination shall be weighed to verify complete loading by subtracting the increment weight (

36、from memory) from the total weight to obtain the loaded propel- lant weight. In such cases, process control plans in accordance with Data Item Description DI-P-1604 must be submitted to the Technical Agency (see 6.6) for review of the automated opera- tion. 4.5.2 Weight of propellant in charge, prop

37、elling (first article). 4.5.2.1 Cestructive test. The propellant shall be removed from the charge, propelling and weighed. If any sample fails to meet the requirement it shall be classified defective and the first article sample shall be rejected. 4.5.2.2 Non-destructive (alternate procedure). The c

38、harge, propelling shall be weighed and the net weight of propellant determined by subtracting parts tare weight from the gross weight. If any sample fails to meet the requirement it shall be classified defective and the first article sample shall be rejected. 4.5.3 Gross weight of propelling charge.

39、 The loaded propelling charge shall be weighed individually. If any assembly fails to meet the requirement, it shall be classified defective and removed from the lot. 4.5.4 Velocity test. This test shall be conducted at a Government proving ground. The rounds shall be inert loaded to 9.05 plus or mi

40、nus .O5 pounds including the weight of the dummy fuze. The rounds shall be assembled at maximum charge (i.e. with four charges). The rounds shall be conditioned to 700 + 2.00 Fahrenheit and fired from a hard mount at an elevation of 800 mils, from an (M29) 81MM mortar tube (3.207 inches max.) - 11 a

41、- - . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-LILB 13 M 7779706 0325350 5 M - MIL-C- 48 8 8 1B (AR) for which the round is standard. Reference rounds shall be fired after every third test round. These reference rounds shall consist of r

42、eference standard components and a calibra- tion lot of propellant charges, and ignition cartridges for velocity correction. The individual velocities and pressures shall be obtained and recorded. Velocity standard deviation and mean velocity shall be calculated to determine compliance with applicab

43、le requirements. A formal firing report shall be submitted (see 6.7). 4.5.5 Damaged propelling charge. To ascertain that a damaged propelling charge is to be classed as critical or maior, - the following procedures shall be used: a. Place the damaged charge on a M24 fin, oriented such that b. The fi

44、n-charge assembly shall be hand-shaken vigorously the propellafit would he resting against the damaged surface. three times. c. Examination shall be made for propellant spillage - if any propellant is observed, the damaged propelling charge shall be classed as a critical defect: if no propellant is

45、observed, the damaged propelling charge shall be classed as a major defect. 5. PREPARATION FOR DELIVERY 5.1 Unit packing. Packing shall be as specified on dwg. 9313721. 5.2 Exterior packing. Packing shall be as specified on dwg. 9313756. 5.3 Marking. Marking shall be as specified on dwg. 9313721 and

46、 dwg, 9313756. 6. NOTES 6.1 Intended use. The components covered by this specifica- tion are intended for use on the 81MM Mortar for use on the Cartridge, 81MM, HE, M374A3 and WP, M375A3. 6.2 Ordering data. See MIL-A-48078. 6.3 Submission of inspection equipment for design approvals. See MIL-A-48078

47、. Submit designs as required to Commander, Us Army Armament Research and Development Command, ATTN: DRDAR-QAT-I, Dover, NJ 07801. 12 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-C-48881B (AR) 6.4 Data requirements. Deliverable data required by

48、 this Paragraph Cata Requirement Applicable DIE specification is cited in the following paragraph: 4.5.1.2 Manufacturing Methods DI -P-1604 Reports (Copies of data item descriptions required by the contractor in connection with specific procurement functions should be obtained from the procuring act

49、ivity or as directed by the contracting officer). 6.5 Erawings. Crawings listed in Section 2 of this specifi- cation under the heading US Army Armament Research and Develop- ment Command (ARRACCOM) may also include drawings prepared by, and identified as Edgewood Arsenal, Frankfrd Arsenal, Rock Island Arsenal, or Picat