ARMY MIL-S-70791-1990 SIMULATOR MISSILE SAGGER XM27 PARTS FOR AND LOADING ASSEMBLING AND PACKING《XM27型SAGGER导弹模拟器零件的装载 组装和包装》.pdf

《ARMY MIL-S-70791-1990 SIMULATOR MISSILE SAGGER XM27 PARTS FOR AND LOADING ASSEMBLING AND PACKING《XM27型SAGGER导弹模拟器零件的装载 组装和包装》.pdf》由会员分享，可在线阅读，更多相关《ARMY MIL-S-70791-1990 SIMULATOR MISSILE SAGGER XM27 PARTS FOR AND LOADING ASSEMBLING AND PACKING《XM27型SAGGER导弹模拟器零件的装载 组装和包装》.pdf（24页珍藏版）》请在麦多课文档分享上搜索。

1、MIL-S-70771 13 W 777770b 043Llb7b 2 MIL-S-70791 (AR) 9 April 1990 MI LI TARY SPEC I FI CATION SIMULATOR, MISSILE: SAGGER XM27, PARTS FOR AND LOADING, ASSEMBLING AND PACKING This specification is approved for use within the U.S. Army Armament, Munitions and Chemical Command, and is available for use

2、by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification contains requirements not covered by the drawings and provides quality assurance provisions for the fabrication of parts for and loading, assembling and packing for one type of simulator designated a

3、s simulator, Missile: sagger XM27. 9 %=% 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications, standards and handbooks. The following specifications, standards and handbooks form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of

4、these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2). O Benefida comments (-datim, additioas, deletions) and any pertineot data which may be of use in improving this docun

5、ient shauld be adckssed to: Canmaoder, U.S. Army ARDEC, ATlN SMCAR-BAGS, Picathy bd, New Jersey W8Cl6-5000 by Upng the kif-addressed Stadah% tim Document improvement n)clposai (DD Form 1426) appearing at the end of this document or by Ittter. AMSC NIA NT A, Approved for public release; distribution

6、is unlimited. FSC 1370 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SPECIFICATIONS MILITARY MIL-P-116 - Preservation Methods of MIL-A-48078 - Ammunition, Standard Quality Assurance Provisions, General Specification For, MI L-P-7 O 7 6 2 - Propella

7、nt, Composite, Cast, For use in Simulator, Missile: sagger XM27 STANDARDS MILITARY MIL-S-70771 13 M 777770b O434b77 4 1 MIL-S-70791 (AR) MI L- S T D- 3 3 1 - Fuze and Fuze Components, Environmental % and Performance Tests For (Unless otherwise indicated, copies of federal and available from the Mili

8、tary Specifications and Standards, Bldg. 4D, 700 Robbins Ave, Philadelphia, PA 19111-5094. military specifications, standards, and handbooks are d I- 2.1.2 Other Government documents, drawings, and publications. The following other Government documents, drawinss. and publications-form a part of this

9、 specification to the extent specified herein. unless otherwise specified, the issues shall be those in effect on the date of the solicitation, O DRAWINGS U.S. ARMY ARMAMENT, RESEARCH, DEVELOPMENT AND ENGINEERING CENTER (ARDEC) PRODUCT AND PACKAGING DRAWINGS 12576572 - Sirnulator, Missile: sagger XM

10、27 12598324 - Packing and Marking For Support, 12598333 - Packing and Marking for Box, Pallet Shipping, Polystyrene Foam For Simulator, Missile: sagger XM27 Type, Wirebound for Simulator, Missile sagger XM27 a Provided by IHSNot for ResaleNo reproduction or networking permitted without license from

11、IHS-,-,-MIL-S-70791 13 = 99999Oh 043qh98 h W MIL-S-70791 (AR) (Copies of drawings, publications, and other Government documents required by contractors in connection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting activity.) 2.2

12、Order of 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. Nothing in this specification, however, shall supersede applicable laws and regulations unless specific exemption has been obt

13、ained, 3. REQUIREMENTS 3.1 Materials. Materiais and parts shall be in accordance with 3.2 Assembly. The Simulator Assembly shall comply with all 9. applicable drawings, specifications and standards. requirements specified on Drawing 12576572 and all associated drawings, and with all requirements spe

14、cified in applicable specifications and standards. *% 3.3 Propellant. The propellant shall comply with all 3.3.1 Loaded rocket. Total area of cracks and voids on the requirements of MIL-P-70762 and all applicable drawings. o propellant surface shall not exceed 2 square inches. 3.3.1.1 Rocket propell

15、ant adhesion. Propellant shall exhibit no visual signs of separation from the tube wall. 3.4 Function. The simulator shall comply with the following requirements when fired using igniter assembly (dwg. 9390399), an electric match and twelve (12) volt power source, from an approved fixture capable of

16、 firing up to an angle of 30 degrees maximum (max) from the horizontal. a. The rocket shall expel a visible flame and minimal light b, The rockSb shall not impact the ground for the first 1000 grey plume, both visible during powered flight. feet of flight. 3 Provided by IHSNot for ResaleNo reproduct

17、ion or networking permitted without license from IHS-,-,-c. The rocket range shall be a minimum of 1000 ft. 3.5 Environmental Conditions. -. - MIL-S-70792 13 = 9999906 0434699 8 MIL-S-70791 (AR) 3.5.1 Rocket assembly integrity test (Dwg. 12576571). The nose and tailcone shall not separate from the r

18、ocket tube and shall not exhibit any signs of bulging or displacement when tested as specified in 4.5.5. 3.5.1.1 Dimensional stability test. The rocket assembly shall exhibit dimensional stability (less than 2 percent variation) when tested as specified in 4.5.5.1. 3.5.2 Transportation vibration - t

19、emperature. The rocket 8 simulator (Dwg. 12576572) shall comply with the following requirements when tested as specified in 4.5.3. rl a. There shall be no loose propellant on the simulator or in the test box after testing. b. The rocket components shall not separate during test. c. The rocket shall

20、not function during test. 3.5.3 Five foot drop test. The loaded rocket (Dwg. 12576572) shall not function and shall remain fully operable when tested as specified in 4.5.4 and 4.5.2. 0 3.6 First article inspection. This specification contains technical provisions for first article inspection. Requir

21、ements for the submission of first article samples by the contractor shall be as specified in the contract. 3.7 Workmanship. All parts and assemblies shall be fabricated and finished in a thorough, workmanlike manner. They shall be free of burrs, chips, sharp edges, cracks, crazes, porosity, warpage

22、, burn marks, blisters, excess flash, scratches, dirt, grease and other defects and foreign matter which would affect appearance or serviceability, The cleaning method used shall not be injurious to any part nor shall the parts be contaminated by the cleaning agent. All required markings shall be ne

23、at, legible and sharply defined. All packing components shall be dry. , 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-70791 13 W 9777906 0434700 O W MIL-S-70791 (AR) 4. QUALITY ASSURANCE PROVISIONS 4.1 Responsibility for inspection. Unless

24、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 utilize his own or any other facilities suitable for the pe

25、rformance of the inspection requirements specified herein, unless disapproved by the Government. The Government reserves the right to perform any of the inspections set forth in the specification where such inspections are deemed necessary to assure supplies and services conform to prescribed requir

26、ements. 4.1.1 Responsibility for compliance. All items must meet all a requirements of sections 3 and 5. The inspection set forth in this specification shall become a part of the contractors overall .- inspection system or quality program. % requirements in the specification shall not relieve the co

27、ntractor of the responsibility of assuring that all products or supplies submitted to the Government for acceptance comply with all requirements of the contract. Sampling in quality conformance does not authorize submission of known defective material, either indicated or actual nor does it commit t

28、he Government to acceptance of any defective material. inspection shall be conducted on this item: The absence of any inspection 4.2 Classification of inspections. The following types of a. First Article Inspection b. Quality Conformance Inspection 4.3 First article inspection 4.3.1 Submission. The

29、contractor shall submit a first article sample as designated by the Contracting Officer for evaluation in accordance with provisions of 4.3.2 and 4.3.3. The first article sample shall consist of the following items and sample quantities as indicated in Table I: Part Description Drawings Nose 1257651

30、6 Tube, Rocket 12576517 Taiicone 12576518 Simulator, Missile: sagger XM27 12576572 Box, Pallet Type, Wirebound 12597833 Support 12598581 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-70792 13 = 9999906 0434703 2 MIL-S-70791 (AR) 4.3.2 Inspe

31、ctions to be performed. First article assemblies, components and test specimens shall be subjected by the Government to any or all of the examinations and tests specified in Table I and MIL-A-48078. 4.3.3 Rejection. See MIL-A-48078. 6 Provided by IHSNot for ResaleNo reproduction or networking permit

32、ted without license from IHS-,-,-MIL-S-70771 13 M 7777906 0434702 4 * c O .rl 5 c, u a, a (II c .rl al d u -Fi 4J LI ld 4J (II LI “a 02 . H w cl m 2 ffi 4 U rl QI P O b I v) I I2 H E tn I- s2 m Ei I- # o L O z 0 I- U s2 4 2 o (u LLi O I+ ti I fn I- (u c x LI a, F F (d (II * a, rl -ri (II (II .rl c L

33、I O u d a, 1-0 MIL-S-70791 13 7999906 OLI39707 7 W ri ri m m 5 5 u) w 4 -4 3 3 cv r- m m . Li O 4J u a a, .ri Li c Li u) a oal 14 n Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-z % O H U w pi CA z H H C rl r3 ti I v) h rl O 4J Li O .rl Li ch h rl

34、a E a, cn ._ II) 4 4J a, 24- u gffi O MIL-S-70773 33 779770b 0434730 3 rl m 07 DII) %! cub mm 44 44 HH HI-I HH a, rlrl Q- Q 4J a, HH a, rld QQ am BH rl rdl Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-70772 23 W 7777706 0434721 5 = rlrl -4 .

35、rl 33 rl rlrl e NuNcv M Mme NI- MMMM M MMM MM . . HHH H H H HH HHH H HHrl rl . Irlrlrl rl rlrlm Oa,a, a, a,* 333 3 33e -a,a,a, a, CUO. Locl cl GI i-4 i-4i-4* 5 444 4 4- a, HHH a,a,Q, a, 5 c -4 w u U a, 16 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,

36、-,-MIL-S-70771 13 = 7777706 Oq34712 7 M w 4 rl a, a JJ O rlrl NFniN NNN mmm mmmm . . .a rl 3 rlrld H III vi O00 4 H I I I I i I I ! I I 1 I LLL 4 . -a, c O u rl -4 m JJ Li O 4-1 n u) a, rl O c Y a, c O u a, I) O c Li O 4-1 n u) a, rl O c U a, u m 4-1 Li 5 I) rl a, 3 a, II F c -4 * E t e C m u .rl pi

37、 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-70791 13 9999906 0434713 7 z O H H u W pi cn 2 H W u z p: O tri z O u * H H GI a 3 5 J ! u o al H a, m rd 2 m cvcv cvcv mm mm NI- mm H HH HH HH HH HH HH HH H P m IQ 5 EU -4 a, o -4 M luici o -m Q

38、 Li oc QO E a =I* a, co c a, -4 c,u w ur0 a, 5 MOP u.c, m a, o a24 c Ud m O .c a, !Z GI 05 ow Orl OQ dE U -4 Li JJOdNmTYodCV -rl *no o o o c o o M d rl TI cv cv, G c Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-70791 13 W 9977706 OL1347111 O

39、 M I I I I I I I l I I l. ! !. z ,u O H H w pi VI z H w u z p: O 0g u * !3 H !J 5 O 5 F: 7 O Q a, Li -li z 4 a, Q.l 31 H .4J a, rl rl a pi x wo 4 grn rlrlrl rlrl aaa am 757 75 WWW Wv1 .Fi -d-d 333 .-g -$ NP hl“ mmm mm . HHH HHH 3 HHH H3 444 444 44 HHH HH HHH HH a,a,a, Wa, rlrlrl rlrl QQQ QQ aaa aa H

40、HH HH a a, c -?I u a, 5 a, c O z A U a pi 7 W5 a, wrl E ha, cum QW I-iOha, OQ OW u u0 c CO H Hd Li O 19 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-70771 13 m 7777706 0434735 2 MIL-S-70791 (AR) 4.4.3 Testing. 4.4.3.1 Function test (hot, col

41、d, ambient). Beginning with e the first lot produced and continuing until three (3) consecutive lots have complied with the acceptance criteria a total of eighty (80) simulator assemblies shall be selected from each lot for test in accordance with 4.5.2 (40 ambient, 20 hot, 20 cold). The lot shall b

42、e rejected if two (2) or more major functioning defects occur. After three (3) consecutive lots have met the acceptance criteria above, fifty (50) simulators shall be selected from each lot for test (30 ambient, 10 hot, 10 cold). The lot shall be rejected if one (1) or more major functioning defects

43、 occur, and lotsampling shall revert to eighty (80) samples per lot. 4.4.4 Inspection equipment. The inspection 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. T

44、he contractor shall submit for approval inspection equipment designs in accordance with the terms of the contract. See Section 6 of MIL-A-48078 and 6.3 herein. 4.5 Methods of inspection. 4.5.1 Propellant. The propellant shall be tested in accordance with MIL-P-70762. Any lot failing any requirement

45、outlined in the specification and drawings shall be disqualified for use in production. 51.5+3OC (125+50F), cold, -32+3oC (-25+5OF). The simuTators shall be conditioned for 12-hours minimum at the specified temperature and fired within 10 minutes after removal from the conditioning chamber. The simu

46、lators shall be mounted in an approved firing fixture on a rigid support and fired by means of the specified power source and firing device at an angle of 27.50 + 2.50 quadrant elevation. Observation shall be made for compliance with the applicable requirements. Any rocket that fails to comply with

47、requirements shall be classified as a defect. NOTE: Rocket shall not be tested in wind conditions of 15 knots head wind or 15 knots crosswinds. 4.5.3 Transportation vibration - temperature. Simulator samples shall be tested according to Test 119 MIL-STD-331, Procedure I. Five (5) rockets shall be pr

48、e-conditioned at OF for two (2) hours max. prior to vibration and the other five (5) rockets at 1450F for two (2) hours max. prior to vibration. The vibration test duration at each temperature shall be six (6) hours (2 hours per axis). Simulators shall be functioned at ambient temperature in accordance with 4.5.2. (First Article Only) 4.5.2 Function test. (Ambient, 21+3oC (70+5OF), - Hot, 20 “ *, O c Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-S-70791 33 999990b O434736 4 MIL-S-70791 (AR) 4.5.4 Five foot drop. The rocket shall be te