NAVY MIL-D-23615 C-1993 DESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICES《为炮筒驱动装置设计和估价》.pdf

1、,.,INCH-POUNDMIL-D-23615C(AS)30 NovemlSUPERSEDMIL-D-235 MarchMILITARY SPECIFICATIONDESIGN AND EVALUATION OF CARTRIDGE ACTUATED DEVICESer 1993NG15B(AS)974This specification is approved by the Naval Air Systems Command,Department of the Navy, and is available for use by all Departmentsand Agencies of

2、the Department of Defense.1. SCOPE1.1 *. This specification covers the general requirements for design andestablishes uniform methods for testing cartridge actuated devices, (CADS). Guns,rockets, rocket catapults, ballistic hose/tubing, and stores separation equipmentare not covered by this specific

3、ation. For purposes of this specification, theterm cartridge actuated device includes any device which provides the means ofreleasing potential cartridge energy or harnessing this energy to accomplishwork. Linear shaped charge, explosive energy transfer lines, and “sealed-in”cartridge actuated devic

4、es (see 6.4.1) fall within the scope of MIL-O-21625.However, devices of the “sealed-in” type are also required to meet the safety andstructural design requirements of this specification as specified In 3.6.3. Thepurpose of the testing program is to determine performance, safety, soundness ofmechanic

5、al design, and resistance to environments encountered during storage,handling, and service use. Cartridge actuated devices are safe for handling anddo not deteriorate to a degree which wouid render their performance or safetydoubtful after being subjected to the testing programs of this specificatio

6、n.1.2 Classification of the types of cartridqe actuated device release.Type ISafety of handling and installation. This type of release is requiredprior to handling and installation of CADS in naval equipment. For requirements,see 3.17.1.Beneficial comments (recommendations, additions, deletions) and

7、 any pertinentdata which may be of use in improving this document should be addressed to:Commanding Officer, Naval Air Warfare Center Aircraft Division Lakehurst, SystemsRequirements Department, Code SR3, Lakehurst, NJ 08733-5100, by using theself-addressed Standardization Document Improvement Propo

8、sal (00 Form 1426)apLsearlngat the end of this document or by letter.AMSC N/A FSC 1377DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-O-23615C(AS)Type IIInterim serv

9、ice release. This release is required prior to anyflights or use of CADS involving naval personnel and will be granted inaccordance with the provisions of 3,17.2. The Naval Air Systems Command hasthe prerogative to authorize procurement of CADS for fleet use, subsequent toa Type II release.Type 111

10、AFinal release to service (fully documented). This type of release1s required for admission of CADs into the Naval supply system as a fullydocumented device (see 3.9). For requirements, see 3.17.2Type III BSpecial release to service (documented by a source controldrawing). If the data required for a

11、 Type III A release are not available,such as proprietary rights and patents, then a Type 111 B release to serviceis required for admission of CADS into the Naval supply system. Forrequirements,for a Type 111 B release, see 3.17.2. For documentation anddata requirements for a Type III B release, see

12、 3.9.Type IVUse of approved cartridge actuated device (using same ballisticenergy source and associated equipment) in a new application. If a CAD haspreviously been granted a Type 111 A or Type III B release and is to be usedin a new application, a Type IV release to service for the new applicationw

13、ill be granted in accordance with the requirements of 3.17.3.2. APPLICABLE DIXUMENTS2.1 Government documents.2.1.1 Specifications, standards and handbcoks. The followingspecifications, standards, and handbooks form a part of this document to theextent specified herein. Unless otherwise specified, th

14、e issues of thesedocuments are those listed in the ssue of the Department of Defense Index ofSpecifications and Standards (OODISS) and supplement thereto, cited in thesolicitation (see 6.2).SPECIFICATIONSMILITARYMIL-P-514 Plate, Identification, Instruction and Marking, BlankMIL-S-5002 Surface Treatm

15、ents and Inorganic Coatings for MetalSurfaces of Weapons SystemsMIL-C-5501 Caps and Plugs, Protective, Dust and Moisture SealMIL-C-5541 Chemical Conversion Coatings of Aluminum and Aluminum Alloys2Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-D

16、-23615C(AS)MIL-A-8625MIL-N-18307MIL-P-19834MIL-D-21625MIL-P-23460MIL-I-23659MIL-O-81980MIL-C-83124STANOAROSFEOERALFEO-STO-H28MILITARYMIL-STO-1OOMIL-STO-129MIL-STO-l30MIL-STO-331MIL-STO-453MIL-STD-810MIL-STD-875MIL-STO-889MIL-STO-970MIL-STD-1168MIL-STO-1521DOO-STO-2101Anodic Coatings, for Aluminum an

17、d Aluminum AlloysNomenclature and Identification for Electronic, Aeronautical,and Aeronautical SupportPlates, Identification or Instruction, Metal Foil, AdhesiveBacked, General Specification forDesign and Evaluation of Cartridges for Cartridge ActuatedOevicesPin, Quick-Release, Self-Retaining, Posit

18、ive LockingInitiators, Electric, General Design Specification forDesign and Evaluation of Signal Transmission Subsystems:General Specification forCartrtdge Actuated/Propellant Actuated Oevices, General OeslgnSpecification forScrew-Thread Standards for Federal ServicesEngineering Drawing PracticesMar

19、king for Shipment and StorageIdentification Marking of U.S. Military PropertyFuze and Fuze Components, Environmental and Performance TestsforInspection, RadiographicEnvironmental Test MethodsType Designation System for Aeronautical and AeronauticalSupport EquipmentDissimilar MetalsStandards and Spec

20、ifications, Order of Precedence for theSelection ofAmmunition Lot NumberingTechnical Reviews and Audits for Systems, Equipments, andComputer SoftwareClassification of Characteristics3Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-D-23615C(AS)(Un

21、less otherwise indicated, copies of federal and military specifications,standards, and handbooks are available from DODSSP - Customer Service,Standardization Documents Order Oesk, 700 Robbins Avenue, Building 4D,Philadelphia, PA 19111-5094.)2.1.2 Other Government documents, drawings and publications

22、. The followingother Government documents, drawings, and publications form a part of thisdocument to the extent specified herein. Unless otherwise specified, the issuesare those cited in the solicitation.CODE OF FEOERAL REGULATIONS49CFR Parts 100-199 Transportation(Copies are available from the Supe

23、rintendent of Documents, U.S. GovernmentPrinting Office, Washington, DC 20402-0001.)2.2 Non-Government publications. The following document(s) form a part ofthis document to the extent specified herein. Unless otherwise specified, theIssues of the documents which are 00D adopted are those listed in

24、the issue ofthe DODISScited in the solicitation. Unless otherwise specified, the issues ofdocuments not listed in the 0001SS are the issues of the documents cited in thesolicitation (see 6.2).AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA (AIA)NAS 618 Fastener-Recommended Shank, Hole andRadius Limits f

25、orNAS 1091 Streamer Assembly, WarningHead-to-Shank Fillet(Application for copies should be addressed to the Aerospace IndustriesAssociation of America, Inc., 1250 Eye Street NW, Washington, OC 20005.)Ai4ERICANSOCIETY FOR TESTING ANO MATERIALS (ASTM)ASTM D 4919 Specification for Testing of Hazardous

26、Materials, Packaging(Application for copies should be addresed to the American Society forTesting and Materials, 1916 Race Street, Philadelphia, PA 19103-1187.)(Non-Government standards and other publications are normally availablefrom the organizations that prepare or distribute the documents, Thes

27、edocuments also may be available in or through libraries or otherinformational services.)2.3 Order of precedence. In the event of a conflict between the text ofthis document and the references cited herein, the text of this documenttakes precedence. Nothing in this document, however, supersedes appl

28、icablelaws and regulations unless a specific exemption has been obtained.”2.4 Streamlining. This document has been streamlined. Appendix A toNIL-D-23615 lists those documents required for MIL-D-23615 acquisition and4isProvided by IHSNot for ResaleNo reproduction or networking permitted without licen

29、se from IHS-,-,-MIL-D-23615C(AS)a mandatory part of MIL-D-23615. Those documents listed in Appendix A havethe same status as those referenced directly in NIL-D-23615 (first tierdocuments). All other documents, referenced through tiering, may be used asguidance and information to supplement 141L-D-23

30、615. MIL-D-23615 is astreamlined document.3. REQUIRE14ENTS3.1 Selection of speclflcatlons and standards. Specifications andstandards for necessary commodities and services not specified herein shallbe selected in accordance with MIL-STD-970.3.2 Special requirements. Special requirements for specific

31、amlications shall take Precedence over those listed herein, provided suchspkclal requirements are”more stringent. Other conflicting-requirements aresubject to the approval of the cognizant design agency (see 6.4.3) for thespecific application invoived.3.3 Materials. Materials for the CAD shall be co

32、mpatible with theexplosive, propellant, delay composition, pyrotechnic, combustion products,and buffering fluid (if used); and shall withstand environmental, functional,service, and storage conditions to which the CAD will be exposed. Acceptanceor approval of materials for design or use during the c

33、ourse of manufactureshall in no case be construed as a guarantee of acceptance of the finisheddevice. Pyrocellulose materials shall not be included as wads, spacers, orclosure discs. Materials which are nutrients for fungi shall not be used.3.3.1 m. Exposed metals shall be of the corrosion-resisting

34、 typeor suttably treated to resist the corrosive effects of fuels, salt spray oratnsosphertcconditions to which the CAD may be subjected in storage or normalservice use.3.3.1.1” Dissimilar metals. Dissimilar metals shall not be used inIntimate contact with each other unless protected against electro

35、lyticcorrosion. Dissimilar metals are defined in MIL-STD-889.3.3.2 Plastic parts. The use of plastic parts shall be subject to theapproval of the cognizant design agency for the specific application involved.3.4 Finishes. Protective coatfngs and finishes shall be used which willnot crack, chip, or s

36、cale during normal service life or when subjected toenvironmental conditions specified herein. Surface treatments, coatings, andfinishes shall conform to MIL-S-5002 except that aluminum and aluminum alloyparts shall be anodized In accordance with 3.4.1.3.4.1 Anodizinq. Aluminum and aluminum alloy pa

37、rts subject to wear,abrasion, and erosion or exposed to corrosive environmental elements shall beanodized in accordance with MIL-A-8625, Types II or III. Chemical conversioncoatings conforming to MIL-C-5541 may be used to repair mechanically damagedareas from which the anodic coating has been remove

38、d.3.5 Color coding. Color coding of CADS as a primary means ofidentification is strictly forbidden.5Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-D-23615C(AS)3.6 Design and construction. The CAO shall be of the simplest and mosteffictent desiqn

39、 consistent with the m_oDosed use. SDecific considerationshall be given-to the factors of minlrnum”size and weight, resistance todeleterious environments, reliability of performance, maintainability (see3.6.2), and safety of operation. All CADS, including the ballistic energysource, such as cartridg

40、es and explosive energy transfer lines, submitted foror subjected to the requirements of 3.16 shall be of final designconfiguration, identical in design, manufactured by the same process andshall be from the same lot. Prior to manufacturing CADS for service releasetesting, a critical design review s

41、hall be conducted per MIL-STD-1521 (see6.3).3.6.1 Ballistic energy. Prior to service release, the cartridge(s) forthe CAO shall have met the release requirements of MIL-O-21625.3.6.2 Disassembly and reassembly. Unless otherwise approved by thecognizant design agency, the CAD shall be designed so tha

42、t it can bedisassembled for inspection or installation of the cartridge(s), O rings, andassociated subassemblies and reassembled. Disassembly and reassembly of thedevice shall be accomplished by the use of standard tools.3.6.3 “Sealed-in” type of cartridqe actuated device. “Sealed-in” typeof cartrid

43、ge actuated devices (see 6.4.1) shall meet the design,environmental and functional requirements of MIL-D-21625 and the firingmechanism, shear pin, dust, submersion, iced condition and structuralintegrity requirements of this specification.3.6.4 Service life. C4DS, when packaged in hermetically seale

44、dcontainers, shall have a service life of not less than 5 years from the dateof manufacture, and shall be capable of being rendered serviceable after thisperiod by replacement of cartridges, O rings, shear pins, and similar items.Service life assignments must be approved by the Naval Air Systems Com

45、mandprior to application in service.3.6.5 Structural inteqrity. CADS shall be designed ulth a minimumsafety factor of 1.5 at the most critical temperature extreme based on themaximum calculated operating pressure limit in the most severe operatingcondition.3.6.5.1 Locked shut firing. Each CAO shall

46、be designed to withstand theinternal ballistic gas pressure developed during a locked shut condition (see6.4.4) over the temperature range -650F to 2000F. There shall be nomechanical failure or rupture.3.6.5.2 No load firing. For a stroking CAO which is designed to remainintact at the end of a power

47、 stroke, parts shall not separate when it isfired at any temperature between -650F and 2000F with no restraining loadapplied to the CAO; e.g., the piston shall not separate from the CAD at theend of stroke nor shall fragmentation of components occur.3.6.6 Locking of parts. All parts not required to

48、have relative motionprior to or during cartridge/ballistic energy source initiation shall besecurely locked by a method that will not damage components or interfere withease of disassembly. Safety wiring is the preferred method. Lock nuts shallnot be used except where it is impossible to use the pre

49、ferred method.Floating or press fit washers shall not be used in the CAO.6Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-D-23615C(AS)3.6.7 Mechanical firinq mechanism. The force required to actuatemechanical firing mechanisms shall be 15 pounds minimum and 35 poundsmaximum. Precocked firing mechanisms shall not be used (see 6.4.2).3.6.7.1 Safety pins. Mechanical firing mechanisms shall be restrainedby single ac