1、 MIL-V-85830 Li2 777770b 023b557 b I INCH-POUND 1 MIL-V-85830(AS) 6 November 1989 MILITARY SPECIFICATION VENTILATOR, TACTICAL, HELICOPTER AIRCREWMAN, CHEMICAL, BLOLOGICAL, RADIOLOGICAL PROTECTIVE This specification is approved for use wfthin the Naval Air Systems Command, Department of the Navy, and
2、 is available for use by all Departments and Agencies of the Deparment of Defense. 1. SCOPE 1.1 Scope. This specification establishes the requirements for the manufacture and acceptance of a ventilator to be used with and form part of the Protective Assembly, Helicopter Aircrewman, Chemical, Biologi
3、cal, Radiological (PASS). 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 these document
4、s shall be those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement thereto, cited in the solici tation. SPECIFICATIONS FED ERAL PPP-B-636 - Box, Shipping, Fiberboard Beneficial comments (recommendations, additions, deletions) and any perti
5、nent data which may be of use in improving this document should be addressed to: Commanding Officer, Naval Air Engineering Center, Systems Engineering and Standardization Department (Code 531, Lakehurst, NJ 08733-5100, by using the self-addressed Standardization Document Improvement Proposal (DD For
6、m 1426) appearing at the end of this document or by letter. AMSC NIA FSC 4240 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. / -% THIS DOCUMENT CONTAINS 90 PAGES. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-
7、V-85830 Y2 m 7777706 023b558 m / SPEC1 FICATIONS FEDERAL (con t d) MIL-V-85830(AS) PP P-c-7 9 5 - PPP-C-1842 - _ MI LITARY MI L-B- 1 8 - MI Lip- 1 1 6 MIL-B-117 - - - MIL-E-5400 - MI L-A-8625_ - MI L-W-16878 - MIL-N-18307 - MI L-P-28809 - MI L-8-49430 - MIL-P-55110 - MI L-C-85829 - MI L-P-85833 - ST
8、ANDARDS FEDERAL FED-STD-595 - Cushioning Material, Flexible, Cellular, Plastic Film for Packaging Appl i cations Cushioning Material, Plastic, Open Cell (.For Packaging Appl ications) Batteries, Non-Rechargeable, Dry. Preservation, Methods of. , . -. Bags, Sleeves and Tubing - Interior Packaging. Ge
9、neral Specification for Aerospace Electronic Equipment. Anodi c Coati ngs for Al umi num and Aluminum Al loys. Wire, Electrical, Insulated, General Specification for. Nomenclature and Identification for Aero- nautical Systems Including Joint Electronics Type Designated Systems and Associated Support
10、 Systems Printed Wiring Assemblies. Battery, Non Rechargeable, Lithium Sulfur Dioxide. Pr i nted Wi ri ng Boards. Coup1 ing Assembly, Hose, Chemica Biological, Radiological Protect Protective Assembly, Helicopter Aircrewman, Chemical, Biological Radiological . Colors. 9 ve. 2 Provided by IHSNot for
11、ResaleNo reproduction or networking permitted without license from IHS-,-,-.- - _. MIL-V-85830 42 9979906 0236559 T W STANDARDS MI LI TARY MI L-STD-21 O MI L-STD-282 DOD-STD-1 O0 MI L-STD-105 MIL-STD-129 MI L-STD-130 MI L-STD-143 MI L-STD-454 MI L-STD-461 MI L-STD-462 DOD-STD-480 MI L-STD-483 MI L-S
12、TD-490 MIL-STD-781 MI L-STD-794 MI L-STD-8 1 O MIL-STD-889 MIL-V-85830(AS) . Engineeering Drawing Practices. Sampl i ng Procedures and Tab1 es for Inspection by Attributes. Marking for Shipment and Storage. Property. Order of Precedence for the Setection of Standards and Speci f icaions. Climatic Ex
13、fremes for Military Equipment. Filter Units, Protective Gas Mask Components and Related Products, Performance Test Methods. Standard General Requirements for El ec tron i c Equi pment . Electromagnet i c Emmi ssion and Suscepti bi 1 i ty Requirements for the Measurement of Electromagnetic Interferen
14、ce Characteristics. Conf i go rat i on C0.n trol - Eng i neer i ng Changes, Devi ations and Waivers. Configuration Management Practices for Systems, Equipment, Munitions and Computer Programs. Specification Practices. Re1 iabi 1 i ty Design and Production Acceptance Tests: Exponential Distribution.
15、.Parts and Equipment, Procedures for Packaging and Packing of. Environmental Test Methods and Engineering Guidelines. Di s s i mi 1 ar Me tal s 1 - Identification Marking of U.S. Military . Control of Electromagnetic Interference. 3 Provided by IHSNot for ResaleNo reproduction or networking permitte
16、d without license from IHS-,-,-i MIL-V-85830 42 77777Ob 023b560 b MI L-V-85830(AS) STANDARDS MILITARY (con t d) MIL-STD-1189 - MIL-STD-1472 - MS-3116 - HANDBOOKS MIL-HDBK-69 5 - Standard Department of Defense Bar Code Human Engineering Design Criteria for Military Systems, Equipment and Faci 1 i ti
17、es Symbol ogy . Connector, Plug, Electric, Series 1, Slder Type, Straight, Bayonet Coupling. Rubber Products: Recommended Shelf Life. 2.1.2 Other Government documents and drawings. The fol lowing other Government documents and drawings form a part of this specification to the extent specified herein
18、. those in effect on the date of the solicitation. Unless otherwise specified, lhe issues shall be Naval Air Systems Command SD-24 - General Specification for Design and Construction of Aircraft Weapon Systems. NAVAIR-1605AS410 - . Tactical Venti lator Mount Assembly. Naval Sea Systems Commarid NAVS
19、EA NOTICE 9310 - Responsibilities and Procedures for the Naval Lithium Battery Safety Program. Headquarters, Department of the Army Army Field - NBC Decontamination Manual FM 3-5 (Copies of specifications, standards, handbooks, drawings, and other Government documents required by contractors in conn
20、ection with specific acquisition functions should be obtained from the contracting activity or as directed by the contracting activity.) specification to the extent specified herein. Unless otherwise specified, the issues of the documents which are DOD adopted shall be those listed in the issue of t
21、he DODISS specified in the solicitation. specified, the issues of documents not listed in the DODISS shall be the issue of the nongovernment documents which is current on the date of the sol ici tation. 2.2 Other publications. The foilowing documents form a part of this 7 Unless otherwised 4 Provide
22、d by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-V-85830EAS 1 AEROSPACE MAT ER I ALS SP ECI FI CAT I ORS AMs-3238. - Butyl Rubber, Phosphate Ester Resistant. specification shall take precedence. No shall supersede appl icable laws and regu has been obtai
23、 ned. 3. REQUIREMENTS . (Application for copies should be addressed to the S8ciety of Automotive Engi neers, 400 Commonweal th Dr.i ve, Warrendal e, PA 15096. ) AMERICAN SOCIETY FOR TESTING AND MATERIALS AST#i 3951 - .Commercial Packaging. (Application for copies should be addressed to the American
24、Society for Testing and Materials, 1916 Race Street, Philadelphia, PA 19103.) 2.3 Order of precedence. in the event of a conflict between the text of this mecification and the references cited herein, the text of this hing in this specification, however, ations unless a specific exemption 3.1 Qualif
25、ication. Ventilators furn shed under this specification shall be products which are authorized by the qualifying activity for listing on the applicable qualified products list at the time set for the opening of bids (see 4.3 and 6.3). 3.2 First article. When specified in the contract or purchase ord
26、er, a . sample shall be subjected to first article inspection (see 4.4 and. 6.4). 3.3 Selection of specifications and standards. Specifications and . standards for necessary commodities and services not specified. herein shall be selected as specified in MIL-STD-143. 3.4 Material s. Materials refere
27、nced herein shall conform to applicable specifications and standards. specifications and that are not specifically described -herein shall be the best quality and the lightest practical weight. Materials shall be corrosion resistant, or suitably treated to resist corrosion due to fuels, salt spray,
28、. environmental, chemical or biological warfare conditions. Aluminum alloy parts shall be anodical-ly treated as specified in MIL-A-8625. To provide adequate bonding, the aluminum oxide film formed by this treatment shall be removed from the actual contact area of all surfaces that act as a path for
29、 electrical current and from the areas under fasteners used for assembly or mounting purposes. Materials that are not covered by- 3.4.1 Aluminum alloy. 3.4.2 Dissimilar metals. Dissimilar metals shall not be used in intimate contact with each other. Dissimilar metals are defined in MIL-STD-889. 3.4.
30、3 Nonmetallic materials Rubber seals and O-rings shall meet the requirements as specified in AMs-3238 and the requirements .specified herein. 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-V-85830 Y2 7779406 0236562 T W i - I. MI L-V-858 30 (
31、ASj 3.4.4 Fungus-proof materials. All materials shall be incapable of supporting fungoid growth. 3.4.5 Age. Elastomeric components shall be comprised of materials with expected shelf life of greater than 5 years in accordance with MIL-HDBK-695 when consistent with the properties required for functib
32、nal suitabi 1 i ty. . These components alone or as part of an assembly shall be delivered to the Government with less than 18 months elapsed from date of cure/manufacture to the date of delivery to the Government. 3.4.6 Toxic materials. The use of materials which produce toxic effects under -any con
33、ditions shall be avoided. 3.4.7 Flammable materials: The use of materials which will support combustion shall be avoided. 3.5 Design. The ventilator shall be used with and form part of the protective assembly (PASS), as shown on Figure 1. the requirements as specified in MIL-P-85833 and this specifi
34、cation. The ventilator shall be designed as shown on Figure 2. It shall be a compact and portable unit suitable for carriage on the aircrewman during ground operations and mounting in the aircraft during flight. The ventilator shall function without interruption upon being connected to or disconnect
35、ed from an external power source. When connected to an external power source the battery power shall not be utilized and inadvertent charging of the battery shall not be possible. The ventilator shall be designed to utilize the mounting bracket as specified in NAVAIR 1605AS410. The design of the ven
36、tilator shall be such as to minimize the retention of moisture and dust and to facilitate inspection, servicing, maintenance and cleaning. The design shall permit decontamination, using procedures of Army FM 3-5, without damage to or deterioration of the venti lator or its protective capabi 1 i ty.
37、The ventilator shall meet 3.5.1 Storage life. The ventilator, less battery, shall be designed to meet the performance requirements of this specification after five years storage under worldwide climatic conditions specified in MIL-STD-210, when packaged as specified in MIL-STD-794. 3.5.2 Interchange
38、ability. All parts, subassemblies and assemblies having the same part number shall be identical as specified in DOD-STD-480 and DOD-STD-100. al 1 performance 1 imi ts without adjustment of any controls or modification of any part or subassembly. When any unit or part is interchanged, the ventilator
39、shall meet 3.5.3 Printed wiring boards. Printed wiring boards shall be designed as specified in MIL-P-55110. 3.5.4 Reverse polarity. The ventilator shall not be damaged by the inadvertent reversal of the battery polarity. 3.6 Construct i on. 3.6.1 Standard parts. Military standard parts shall be use
40、d whenever they Standard parts shall be as specified in are suitable for the purpose. MIL-E-5400. 3.6.1.1 Non standard parts approval. Request for approval for the use of non standard parts shall be as specified in MIL-STD-965, Procedure I. 6 Provided by IHSNot for ResaleNo reproduction or networkin
41、g permitted without license from IHS-,-,-MI L-W-E830 t AS )- 3.6.2 Selection of printed wiring boards. The selection of parts and materials shall be as specified in MIL-STD-454, Requirement 17 or with the approval of thesacquiring activity. Microelectric technology should be utilized to the fullest
42、extent possible. Components shall be rated so that the ventilator shall function within the limits of this *specification after extended inoaerative aeriods while carried in militarv aircraft and subiected to the varied range of environmental conditions defined herein. subassemblies, as outlined in
43、MIL-E-5400, shall be used when practical. modifications shall be performed as specified in MIL-P-28809. spec if i ed i n MI L-STD-454. Nonrepa T 3.6.2.1 . Printed wiring board modifications. 3.6.3 Electronic components. All electronic components shall be as Printed wiring board rabie 3.6.4 Insulatin
44、g materials. Electrical insulating materials shall be as specified in MIL-STD-454, Requirement 11. Insulation for power circuits shall be arc-resistant as specified in MIL-STD-454, Requirement 26. 3.6.5 Encapsulation and embedment. Materials for encapsulation and embedment s ha1 1 be as spec if i ed
45、 i n MIL-STD-454, Requi rement 47. 3.6.6 Semiconductor devices. Semiconductor devices -shall be selected and applied as specified in MIL-STD-454, Requirement 30. Microelectronic devices shall be selected and applied as specified in MIL-STD-454, Requirement 64. Use of nonstandard Darts shall be subst
46、antiated bv re1 iabi 1 i tv data or testing to assure adequate device re1 iabi 1 i ty for the appj ication. - be as specified in MIL-STD-454, 3.6.7 Resistors. Resistors shalT Requirement 33. 1 be chosen and applied as spec fied in 3.6.8 Capacitors. Capacitors sha MI L-STD-454, Requirement 2. be as s
47、pecified in MIL-STD-454, 3.6.9 Soldering. Soldering shall Requirement 5. 3.6.10 Relays. Relays shall be as specified in MIL-STD-454, Requirement 57. fied in MIL-W-16878, 3.6.11 Wiring. Wiring shall be as spec 3.7 Hardware. 3.7.1 Fasteners. All fasteners, includ washers and hinges shall be as specifi
48、ed in ng bolts, screws., nuts, rivets, SD-24. 3.8 Quantitative reliability requirements. When tested in accordance with MIL-STD-781 as specified in 4.8.3.3, the mean time between failure (MTBF) for the ventilator, based on an exponential distribution of failure times, the lower single sided 90 perce
49、nt confidence limit, shall be 500 hours (excluding batteries). The performance requirements specified in 3.9.1, 3.9.2, 3.9.3, 3.9.4 and 3.9.5 shall be the reliability requirements for determining mean time between failures. 3.9 Performance. 7 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-V-85830 42 999970b 0236564 3 / 3.9 1 Leakage. 3.9.1.1 Suctio
