NAVY MIL-P-85121-1980 PROJECTILES 20 MM MARK 100 SERIES《20 MM标号100系列射弹》.pdf
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1、MIL-P-85121(AS) 8 January 1980 SUPERSEDING (See Section 6) MILITARY SPECIFIC ATION PROJECTILES, 20 MM MARK 100 SERIES This specification is approved for use by the Naval Air Systems Command, Depart- ment of the Navy, and is available for use by ali Departments and Agencies of the Department of Defen
2、se. i. SCOPE. 1.1 Scope, This specification defines the characteristics of inert metal parts and their performance and test requirements for the projectiles used in the MARK 100 Series aircraft gun ammunition. 1.2 Classification. Projectiles covered by this specification shall be of the following ty
3、pes: (a) Pressure test (b) MARK 11 MOD 1 (e) MARK 12 MOD O (d) MARK 13 MOD O (e) MARK 14 MOD O -_I_.- Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commanding Officer, Naval Air Engineering Ce
4、nter, Engineering Specifications and Ste.ndard3 Department (ESSD), Code 93, Lakehurst, NJ 08733, by using the self-addressed Staiidmdization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, or by letter. - -_I_-_-. I - _-._._._ _. _._- - - I_-c THIS DOCUMENT CONTAI
5、NS Il0 PAGES* 1-1 - - I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-P-85L2L 13 W 7797906 0363860 6 EI M IGP-8 5 1 2 1 (AS) 2. APPLICABLE DOCUMENTS. 2.1 Issues of documents. The following documents of the issue in effect on date of invitation
6、 for bids or request for proposal, form a part of this specification to the extent specified herein. SPECIFICATIONS M ILITA R Y M IL-S-138 1 2 M IL-1-45607 MIL-C-85122 STANDARDS FEDERAL FED-STD-14 1 MILITARY MIL-STD-105 M IL-STD-1 O9 MIL-STD-PZ9 M IL-STD-I 167 MIL-STD-1168 M IL-STD-1695 Steel Plate,
7、 Wrought, Homogeneous for Ammunition Testing (1/4 to 12 inches). Inspection Equipment, Supply and Main- tenance, for Ordnance. Cartridges, 20 MM MARK 100 Series. Paint, Varnish, Lacquer and Related Materials, Methods of Inspection, Sampling and Testing. Sampling Procedures and Tables for Inspections
8、 by Attributes. Quality Assurance Terms and Definitions. Marking for Shipment and Storage. Ammunition Data Card. Ammunition Lot Numbering. Environments, Working, Minimum Standards for. t 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-f Provided by
9、 IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-P-85LZL 13 M 777770b 0363862 T Hi I MIL-P-85121(AS) PUBLIC ATIONS MILITARY Naval Sea Systems Command (Code Ident 10001) NAPEC-01-2 Operation Instruction for Eddy Current Flaw Detector. Naval Air Systems Comman
10、d (Code Ident 30003) AD-1324 Range Firing Procedures for MARK 100 Series 20 Millimeter Naval Aircraft Gun Ammunition. (Copies of specifications, standards, drawings, and publications required by contractors in connection with specific procurement functions should be obtained from the procuring activ
11、ity or as directed by the contracting officer.) 3. REQUIREMENTS. 3.1 General. The requirement for the projectile shall be as specified herein for the type projectile ordered. The projectile shall pass all applicable ballistic tests of MIL-C-85122, as specified by the procuring activity. See 6.2.1 fo
12、r type of projectile ordered, appiicable tests of ML-C-5i%2, ana testing activity. 3.2 First article. Unless otherwise specified in the contract or purchase order, the contractor shall furnish 500 sample projectiles for first article inspection and approval (see 4.4 and 6.2.1). The first article sam
13、ple shall be manufactured using the same methods, materials, processes, and procedures proposed for produc- tion. The samples shall be delivered to the testing activity designated in the con- tract or purchase order (see 6.2.1). Any production prior to acceptance of the first article sample shall be
14、 at the risk of the contractor. 3.3 Conformance to documents. The projectiles shall be manufactured in accordance with the requirements specified herein and the requirements of the documents listed on the following drawing lists (DLs): (a) Pressure Test . . . . . . . . . . . DL 2605727 (b) MARK 11 M
15、OD 1 . . . -. . . . . DL 2176062 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-(c) MARK 12 MOD O . (d) MARK 13 MOD O . DL 1350781 (e) MARK 14 MOD O . DL 1381197 DL982432 3.4 Materials. 3.4.1 Chemical compositions. The projectile assembly and comp
16、onents shall meet the requirements of the material specification listed on the applicable drawing. 3.5 Mechanical properties. 3.5.1 Residual stress. Components produced by cold forming operations shall be adequately stress relieved to assure freedom from susceptibility to cracking or subsequent dist
17、ortion or malfunction due to unrelieved stress. 3.5.1.1 Hardness. The projectile assembly and components shall meet the hard- ness requirements specified on the applicable drawings. MARK 13 MOD O and MARK 14 MOD O projectile assemblies shall also meet the penetration require- ments of 3.6.1, when lo
18、aded and fired as specified in AD-1324. 3.5.2 Freedom from defects. 3.5.2.1 Soundness. Metal discontinuity in the MARK 11 MOD 1 and MARK 12 MOD O projectile bodies, and the MARK 13 MOD O adapter, and the MARK 14 MOD O windshield as determined by eddy current inspection, shall be less than that repre
19、sented by production check standards of NAPEC-0050 drawings. 3.5.2.2 Fractures or inclusions. Metal discontinuity in the MARK 13 MOD O and MARK 14 MOD O projectile bodies, as determined by ultrasonic inspection, shall be less than that represented by production check and calibration standards of NAP
20、EC-0182 drawings. 3.5.3 Static forces. Projectile body component assemblies shall withstand the following static forces: (a) Pressure test and MARK 11 MOD 1 projectiles shall withstand 40 inch-pounds torque with no angular displacement (see 6.3.1) of the nose plug relative to the body, (b) MARK 13 M
21、OD O projectile body assemblies shall withstand a com- pressive axial load of 8,000 pounds without a permanent increase greater than 0.0015-inch diameter in the cylindrical portion of the 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-M IL-P-85 12
22、 1 (AS) adapter. After having successfully passed the axial load test, the test samples shall withstand 2,500 inch-pounds torque with no angular displacement of the adapter relative to the body. MARK 14 MOD O projectiles shall withstand a compressive axial load of 6,000 pounds without a permanent in
23、crease greater than 0.001 5-inch diameter in the cylindrical portion of the windshield. After having successfully passed the axial load test, the test samples shall withstand 1,000 inch-pounds torque with no angular displacement of the windshield relative to the body. (c) 3.5.4 Band tightness. The r
24、otating band blank and the rotating band seat shall be clean at the time of banding. Shot or sandblasting shall not be used to clean the serrated band seat after knurling. The rotating band blank shall fill the band seat with a maximum allowable void of 0.004 inch between the band seat and .band sea
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