NAVY MIL-I-82877-1992 IGNITION ELEMENT PVU-15 B《 PVU-15 B点火器元件》.pdf
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1、. 5 MIL-I-8277 13 9979906 0511573 T MIL-1-82877 24 hhgh 199 2 SUPERSEDING WS 33113 22 January 1992 MILITARY SPECIFICATION IGNITION ELEMENT, PVU-lS/B Ihis specijkation is approved for use by all Departments and Agencies of the Department of Defewe. 1. SCOPE 1.1 Scope. This specification establishes t
2、he requirements for the PVU-1YB ignition element (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications and standards. The following specifications and standards form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of the
3、se 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). SPECIFICATIONS FEDERAL PPP-T-60 Tape: Packaging, Waterproof PPP-B-566 Boxes, Folding, Paperboard Beneficial comments (re
4、commendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commander, Indian Head Division, Naval Surface Warfare Center, Standardization Branch (Code 3730), 101 Strauss Avenue, Indian Head, MD 20640-5035 by using the Standardiz
5、ation Document Improvement Proposal D Form 1426) appearing at the end of this document or sending a letter. AMSC N/A ESC 1377 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. 0 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from
6、IHS-,-,- _ _- MIL-1-82877 33 m 9999906 0533574 3 m PPP-B-62 1 PPP-C- 1797 MILITARY MIL-P-116 MIL-B-117 MIL-L-3055 MIL-S-8660 MIL-D- 1679 1 MIL-1-23659 STANDARDS MILITARY MIL-STD- 129 MIL-STD-453 MILI-82877 Boxes, Wood, Nailed and Lock-Corner Cushioning Material, Resilient, Low Density, Unicellular,
7、Polypropylene Foam Preservation, Methods of Bags, Sleeves and Tubing Lead Azide Silicone Compound, NATO Code Number S-736 Detergent, General Purpose (Liquid, Nonionic) Initiators, Electric, General Design Specification for Marking for Shipment and Storage Inspection, Radiographic (Unless otherwise i
8、ndicated, copies of federal and military specifications and standards are available from the Standardization Documents Order Desk, Building 4D, 700 Robbins Avenue, Philadelphia, PA 191 11-5094.) 2.1.2 Other Government documents, drawings and publications. The following other Government documents, dr
9、awings and publications form a part of this specification to the extent specified herein. Unless otherwise specified, the issues are those cited in the solicitation. DRAWINGS NAVAL SEA SYSTEMS COMMAND (CAGE Code 53711) DL 6261381 Ignition Element, PVU-lS/B DL 6610182 Test Fixture For PVU-lWB (Applic
10、ation for copies should be addressed to: Commanding Officer, Naval Ordnance Station, Crane Division, Naval Surface Warfare Center, Attention Code 802, Louisville, KY 40214-5001.) 4 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-_ MIL-I-B2877 33 E
11、9999906 0533575 3 PUBLICATIONS CODE OF FEDERAL REGULATIONS (CFBs) 49 CFR 100-199 Transportation (Copies of CFRs are available from the Superintendent of Documents, U.S. Government Printing Office, Washington, BC 20432-8801 .) 2.2 Order of precedence. IR the event of a conflict between the text of th
12、is document and the references cited herein, the text of this document shall take precedence. Nothing in this document, however, shall supersede applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 First article. Unless otherwise specified in the contrac
13、t or order (see 6.2), a first article sample (see 6.3) shall be submitted for testing (see 4.4). 3.2 Conformance to documents. The PVU-lS/B ignition element covered by this specification shall be manufactured in accordance with BL 6261381 and all documents listed thereon. 3.3 Product characteristics
14、. 3.3.1 Materials. All materials used in the manufacture of the ignition elements shall conform strictly to the specifications referred to on the respective drawings unless specific approval in writing covering a departure therefrom has been obtained from the cognizant Navy design activity prior to
15、manufacture. When alternate materials or methods of manufacture are specified on the drawings, the bidders selections shall be clearly stated in the proposal. 3.3.2 Primary components. For the purpose of this specification, the propellant, RDX, Drawing 6261706, Powder, Lead Azide, Type I, MIL-L-3055
16、, Powder, ZKV Ignition, Drawing 6261707, are defined as primary components. There shall be only one production lot of each primary component used in the same lot of ignition elements. 3.3.3 Bridge circuit resistance. The bridge circuit resistance of each ignition element when measured in accordance
17、with 4.6.2 shall not be less than 0.1 1 ohm nor more than 0.15 ohm. 3.3.4 Radiographic. Ignition elements shall be free of imperfections in components oc assembly when inspected as specified in 4.6.3. 3.3.4.1 Serial number identification. Ignition elements shall be permanently and legibly identified
18、 by serial numbers (see 4.6.3). 3.3.5 Leakage. Ignition elements shall not exhibit a leak rate in excess of 1 X i cubic centimeters per second of air at a pressure differential of 1 f 0.1 atmosphere when tested according to 4.6.4. e 3 Provided by IHSNot for ResaleNo reproduction or networking permit
19、ted without license from IHS-,-,- _ MIL-I-2877 13 9999906 051157b 5 MILI42877 3.3.6 No-fire. The ignition element shall not fire during the no-fire test (see 4.6.5) and shall then meet the requirements of 3.5 when functionally tested. 3.3.7 Electrostatic discharge. The ignition element shall not fir
20、e when subjected to a simulated human electrostatic discharge (see 4.6.6) and meet the requirements of 3.5 after the electrostatic discharge test when functionally tested (see 4.6.10). 3.3.8 Non-shorting. The ignition element shall not short when subjected to the non-shorting test of 4.6.11. 3.4 Env
21、ironmental requirements. 3.4.1 Impact shock operation. The ignition element shall meet the functional requirements of 3.5 after the impact shock operation test (see 4.6.7). 3.4.2 Temperature, humidity and altitude cycling. The ignition element shall meet the leak rate requirement of 3.3.4 and the fu
22、nctional requirements of 3.5 at 70 degrees Fahrenheit (OF) only after temperature, humidity and altitude cycling (see 4.6.8). 3.4.3 Vibration. The ignition element shall not initiate, suffer damage, or subsequently fail to meet the functional requirements of 3.5 after vibration (see 4.6.9). 3.5 Func
23、tional requirements. 3.5.1 Ignition delay time. The elapsed time from first indication of 5 f 0.1 amperes current in the ignition elenient bridgewire to the first indication of slug movement must fall in the range of 0.005 to 0.040 second. 3.5.2 Maximum travel time. The ignition element shall provid
24、e sufficient energy to enable the slug (see 4.6.10) to travel 36 f 0.5 inches in 10.71 milliseconds (maximum) when functionally tested at cold (- 89 f: 5“F), ambient (+70 f 5F) and hot (+250 0 5F) temperatures. 3.4 Workmanship. Ignition elements shall be free of defects such as burrs, contaminations
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