1、MIL-T-63262 (AR) 27 February i978 MILITARY SPECIFICATION TEST MODE ASSEMBLY, ROCKET: M180 CRATERING DEVICE PROPELLANT TESTING This specification is approved for use by all departments and agencies of the Department of Defense. 1. SCOPE 1.1 This specification covers the parts and assembly for one typ
2、e of test mode assembly designated as Test Mode Assembly, Rocket: 180 Cratering Device Propellant Testing. 2. APPLICABLE DOCUMENTS 2.1 The following documents of the issue in effect on date of invitation for bids or request for proposals form a part of this specification to the extent specified here
3、in. SPECIFICATIONS MILITARY MIL-A-48078 - Ammunition, Standard Quality Assurance Provisions, General Spec if icat ion for STANDARDS MILITARY MIL-STD-1169 - Packaging, packing and marking for shipment OT Inert Ammunition com- ponent s DRAWINGS (See 6.3) U.S. ARMY ARMAMENT RESEARCH AND DEVELOPMENT COM
4、MAND 9325862 - Test Mode Assembly, Rocket FSC: i140 Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of UM in improving this document should be addressed to: commander, US Army Armament Research and Development Command, Ath. DRDARQA, Dover, New Jersey 0
5、7801 by using the self-addreseed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. 1 I r- THIS DOCUMENT CONTAINS ” PAGES Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-63262 13 m 7
6、777906 03Li6808 7 MIL-T-63262 (AR) (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). 3. REQUIREMENTS 3.1 Material - Materia
7、ls shall be in accordance with applicable drawings and specifications. 3.2 Assembly- The assembly shall comply with all re- quirements specified on drawing (dwg.) 9325862 and with all c requirements specified in applicable specifications. 3.3 First Article Inspection- This specification contains tec
8、hnica1 provisions for first article inspection. Requirements for the submission of first article samples by the contractor shall be as specified in the contract. 3.4 Hydrostatic Inspection- Test mode assembly shall be fitted with a suitable seal and mounted on a suitable hydrostatic test fixture. H
9、ydrostatic pressure shall be applied in accordance with the requirements of dwg. 9325862. The Test Mode Rocket Assembly shall then be disassembled and all parts inspected for cracks, distortion or any other evidence of failure or damage. 3.5 Workmanship- All parts and assemblies shall be fabricated
10、and finished in a thorough workmanlike manner, and all manufacturing, processing, and assembly operations shall be correctly performed. They shall be clean and free of burrs, sharp edges, unblended radii, surface defects, chips, dirt, grease and oil (except where specifically required) , corrosion p
11、roducts and other foreign matter. The cleaning method used shall not be injurious to any part or assembly nor shall they be contaminated by the cleaning agent. Exterior surface coatings shall be continuous except for a few light scratches not exposing base material. markings and stampings shall be n
12、eat and sharply defined. (Required packing shall be dry). All required 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for Inspections- The responsibility for inspections shall comply with MIL-A-48078. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS
13、MIL-T-b3262 13 9999906 03L(b079 MIL-T-6 3 2 6 2 (.AR) 4.2 Classification of Inspections- The following types of inspection shall be conducted on this item: a. First Article Inspection b. Quality Conformance Inspection .4.3 First Article Inspection 4.3.1 Submission- The contractor shall submit a
14、 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 following items in sample quantities as indicated. Part Description Drawing No. Quantity Retainer, forward 9325866 Head 9325867 Nozzle 9
15、325863 Retainer, nozzle 9325864 Screw 9326728 Case 9325865 Plate, retainer, rocket 9244408 Gasket 9326071 4.3.2 Inspections to be performed - See MIL-A-48078 and Table I specified herein. 4.3.3 Rejection- See MIL-A-48078. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without
16、 license from IHS-,-,-n P; 4 (u u) (u M u) I B I GI H x v 2 O H B V w Pl ro 2 w GI V H B P; H u) +I c, V U a, a, k k a, a, n n al - k rll- k MO NkO Qk NDk Co o Ico i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-63262 13 I 7777906 0346811 7 I
17、 Cu I I NNNNNNNNNNNNNN NlnN mmmmmmmmmmmmmm mmm . -?:-?-?:-?-?:-?-?-? 00000000000000 . 040 a al c .d w al a al t: O z X B n Fi al h rn Fi .,-I cAOE z 3s: uw alw 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-z O H m u w PI zo H E! u 2 4 X P; O k z
18、O u * H H rll 4 5 d B rl w i5 a ld al X Cu (u f f (ucucu(u(ucu MITMMM (u (u Lncu rr)rr)mrr) LnLno Ln A-* O Fr 2 O u * E-i Crl 4 3 cp H aJ rl N N O 2 n(u (u(u(ucu(u(u(u MMMMMrr)M MM . . . . . . . kl (dl 0000000 dI O0 u1 El rlrlddrlrlrl El (UN 9 3 L = i Provided by IHSNot for ResaleNo reproduction or
19、networking permitted without license from IHS-,-,-2 O H E-i V w pi B 2 H w u 2 4 x Fr z O u tt P H Cll 4 3 a a, rl N N O 2 k a, F: *rl id c, ;P; -. Ia, - MIL-T-63262 13 I- 7779706 0346816 b d ld Cu(uCuCuCuCuCuCuCu InCu Cu mmmmmmmmm mmm . . . . . . . . . . a, E: O z E O k k Cdt VI LI IO Provided by I
20、HSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-63262 23 M 9797906 0346827 B =t=t O Q o* .d a .rl s u) E: id E X k O 3 k O O a %I O al o r: al e .?I * w 11 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL
21、T-63262 13 U 9777706 0346818 T U 2 O H I u w pi B 2 H w u 2 4 E ffi O h z O u H I H cl 4 3 a w v) 4 u rid dd (u(uN(uNN(u(u(u(uN (u n(u mmmmmmmmmmm mmm . . f*f-f-ffA-ff*-f 00000000000 . no Ln wow 040 . kl ni di *e d(umAnDt-cOchod di dNb kl (dl 000000000drl *dl O00 u1 CI drlrldrldrldrlrlrl CI (ucum 1
22、2 i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-T-632b2 33 9797706 0346839 3 I - I rl Ii.i Visual and Mechanical Inspections - The visual, manual and mechanical inspections and tests shall verify compliance with the requirements of sections 3
23、 and 5 of this specification in accordance with 4.4.2 herein and Table I. 4.5.2 Hydrostatic Pressure Test - The Test Mode Rocket Assembly, dwg 9325862, shall be assembled and mounted on a suitable hydrostatic test fixture. 5. PREPARATION FOR DELIVERY 5.1 Packaging Inspection - The sampling and inspe
24、ction of the preservation-packaging, packing and container marking shall be in accordance with the requirements of MIL-STD-1169. 6. NOTES 6.1 Ordering Data - See MIL-A-48078. I 16 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-T-63262 13 m 39397
25、06 0346823 3 W MIL-T-63262(AR) 6.2 Submission of Designs for Approval- See MIL-A-48078. Submit equipment designs, as required, to Commander, ARRADCOM ATTN: DRDAR-&AA-I, Dover, New Jersey 07801. 6.3 Drawings. - Drawings listed in Section 2 of this specification under the heading US Army Armament Rese
26、arch and Development Command (ARRADCOM) may also include drawings pre- pared by, and identified as, Edgewood Arsenal, Frankford Arsenal, Rock Island Arsenal or Picatinny Arsenal drawings. Technical data originally prepared by these activities is now under the cognizance of ARRADCOM. Custodian: Army-AR Preparing Activity: Army-AR Project Number: 134O-A543 MJ.9. GOVERNHJ3NT PRINTING OFFICE :19 78-703-122/2883 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
