NAVY MIL-STD-2131 A-1991 LAUNCHER EJECTION GUIDED MISSILE AIRCRAFT GENERAL DESIGN CRITERIA FOR《弹射导弹飞行器的发射器的一般设计准则》.pdf

《NAVY MIL-STD-2131 A-1991 LAUNCHER EJECTION GUIDED MISSILE AIRCRAFT GENERAL DESIGN CRITERIA FOR《弹射导弹飞行器的发射器的一般设计准则》.pdf》由会员分享，可在线阅读，更多相关《NAVY MIL-STD-2131 A-1991 LAUNCHER EJECTION GUIDED MISSILE AIRCRAFT GENERAL DESIGN CRITERIA FOR《弹射导弹飞行器的发射器的一般设计准则》.pdf（40页珍藏版）》请在麦多课文档分享上搜索。

1、MIL-STD-2232A 24 m 9999922 020657q 3 = 0- s INCH-POUND 1 MIL-STD-2131A(AS) 16 December 1991 SUPERSEDING 4 April 1983 MIL-STD-2131 (AS) MILITARY STANDARD LAUNCHER, EJECTION, GUIDED MISSILE AIRCRAFT, GENERAL DESIGN CRITERIA FOR FSC 1440 AMSC N/A DISTRIBUTION STATEMENT A. Approved for public release; d

2、istribution is unlimited. 0 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-2333A 34 9999933 0306575 5 MIL-STD-Z131A(AS) FOREWORD 1. This military standard is approved for use by the Naval Air Systems Command, Department of the Navy, and is a

3、vailable for use by all Departments and Agencies of the Department of Defense. 2, Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: 08733-5100, by using the Standardization Document Improvement Pr

4、oposal (DD Commanding Off i Cer, Naval Air Engineering Center, Systems Engineering and Standardization Department (SESD), Code 53, Lakehurst, NJ Form 1426) appearing at the end of this document or by letter. 4 c. I. ii Provided by IHSNot for ResaleNo reproduction or networking permitted without lice

5、nse from IHS-,-,-. . 8 f PARAGRAPH 1 . 1.1 2 . 2.1 2.1.1 2.1.2 2.2 2.3 3 . 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 3.10 3.11 3.12 3.13 3.14 3.15 3.16 3.17 3.18 4 . 4.1 4.2 4,Z.l 4.2.1.1 4.2.1.1.1 4.2.1.1.2 4.2.1.1.3 4.2.1.2 4.2.1.2.1 4.2.1.3 4.2.1.4 4.2.1.5 4.2.1.6 4.2.1.7 MIL-STD-2331A 3Y 9999913 03065

6、76 7 MIL-STD-2131A(AS) CONTENTS PAGE SCOPE 1 Scope . 1 APPLICABLE DOCUMENTS . 2 Government documents 2 Specifications. standards. and handbooks 2 Other Government documents. drawings. and publications . 5 Non-Government publications . 6 Order of precedence . 6 DEFINITIONS 7 Missile launcher 7 Air-la

7、unched missile 7 Ejection launcher . 7 Rail launcher . 7 Launch 7 Jettison 7 Arming 7 Safe separation . 7 Acceptable separation . 7 Cartridge hang fire . 7 Hung missile 7 Loading . 7 Sway braces . 7 Release system 7 Umbilical . 8 Pylon . 8 GENERAL REQUIREMENTS . 9 Launcher types 9 Selection of mater

8、ials. specifications. standards and drawings 9 Materials . 9 Heat treatment 9 Castings 9 Forgings 9 Non-metallic components . 9 Reinforced plastic construction . 10 Lubrication . 10 Hydraulic fluids 10 Fungus-proof materials 10 Potting compounds . 10 Corrosion protection 10 Suspension system . 7 . L

9、ocking system 8 Metal parts . 9 iii Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-2131A 14 H 9999911 010b577 9 H PARAGRAPH 4.2.1.8 4.2.1.8.1 4.2.1.8.2 4.2.1.8.3 4.2.1.9 4.2.1.10 4.2.1.11 4.2.2 4.2.3 4.3 4.3.1 4.3.2 4.3.2.1 4.3.3 4.3.3.1 4.3

10、.3.2 4.3.3.3 4.3.3.4 4.3.3.5 4.3.4 4.3.5 4.3.6 4.3.7 4.3.7.1 4.3.7.2 4.3.7.3 4.3.7.4 4.3.7.4.1 4.3.7.4.2 4.3.8 4.3.8.1 4.3.8.2 4.3.8.3 4.3.8.4 4.3.8.5 4.3.8.6 4.3.8.7 4.3.8.8 4.3.8.9 4.3.8.10 4.3.9 4.3.10 CO NT E NTS Finishes 10 Anodi zi ng . 10 Chemical surface treatment 10 Plating . 10 Electrical

11、connectors . 11 Wiring 11 Soldered or brazed connections 11 Specifications and standards 11 Drawings 11 General design requirements . 11 Performance . 11 Design factors of safety 11 Pressure systems 12 Structural loads requirements . 12 Take-off and landing loads 12 Captive flight loads 12 Launch lo

12、ads 12 Jettison loads 12 Cyclic loads 12 Stress analysis . 12 Service life 13 Re1 iabi 1 i ty . 13 Interfaces 13 Launcher to aircraft interface 13 Launcher to missile interface . 13 Launcher to support equipment interface . 14 Electrical grounding interface 14 Launcher to aircraft structure groundin

13、g 14 Launcher to internal ground interface . 14 Physical characteristics 14 Launcher weight . 14 Launcher drag . 14 Launcher radar cross section 14 Dimensions and tolerances . 14 Clearances 14 Launcher installation alignment . 15 Umbilical alignment . 15 Service access 15 Test access . 15 Drain prov

14、isions 15 Human engineering . 15 Environmental and service conditions 16 iv Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-2131A 1Y W 9999931 0106578 O CONT E NTS PARAGRAPH PAGE 4.3.11 4.3.11.1 . 4.3.11.2 4.3.11.3 4.3.11.4 4.3.11.4.1 4.3.11.

15、4.1.1 4.3.11.4.2 4.3.11.4.2.1 4.3.11.4.3 4.3.11.4.3.1 4.4 4.5 Maintainability Maximum maintenance time . Ejector system maintainability . Ejector system maximum maintenance time Maintenance plan . Organizational maintenance . Organizational maintenance tasks Intermediate maintenance . Intermediate m

16、aintenance tasks . Depot maintenance Depot maintenance tasks Interchangeability . Identification and markina . 4.6 Recycled. virgin and reclimed materials . 5 . DETAILED REQUIREMENTS . 5.1 Loading of missiles 5.1.1 Support equipment 5.2 Launcher structure 5.2.1 Launcher interface alignment . 5.3 Sus

17、pension and release system 5.3.1 Latch mechanism design . 5.3.1.1 Independent self-latching 5.3.1.2 Manual latching 5.3.1.3 Dependent unlatching . 5.3.2 Release mechanism 5.3,Z.l Manual release . 5.3.3 Electromechanical safety interlock . 5.4 Missile sensing 5.5 Umbilical system . 5.6 Sway braces 5.

18、7 Signal management system . 5.8 Fuzing and arming control 5.8.1 Motor ignition provisions . 5.8.2 Warhead arming provisions . 5.9 Launcher ejection system . 5.9.1 Cartridge initiation 5.9.2 Cartridges 5.9.3 Cartridge electrode contact pin 5.9.4 Cartridge breech 5.9.5 Launcher to aircraft reaction .

19、 5.9.6 Separation performance requirements . 5.9.7 Ejection pistons 16 17 17 17 17 17 17 18 18 18 18 18 18 18 19 19 20 20 20 20 20 20 21 21 21 21 21 = 22 22 22 22 23 23 23 23 23 23 24 24 27 27 27 V I Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MI

20、L-STD-ZL3LA 14 97999Ll OLOb579 2 PA RAG RAP H 5.10 5.10.1 5.10.1.1 5.10.1.2 5.10.1.3 5.10.1.3.1 5.10.1.3.2 5.10.1.3.3 5.10.1.3.4 5.10.1.3.5 5.11 5.11.1 5.11.2 5.11.3 5.11.4 5.11.5 5.11.6 5.11.7 5.11.8 5.11.9 6. 6.1 6.2 6.3 6.4 6.5 6.6 CONTENTS Safety in design . Launcher safety program Safety progra

21、m functions . Failure mode effects analysis ,. Specific design safety . Safety interlock . Inadvertent release Locked shut functioning Driven items . 3“ Impulse cartridges . Electromagnetic environmental effects (E 1 . Electromagnetic compatibility program (EMCP) . . . Electromagnetic compatibility

22、(EMC) Electromagnetic vulnerability (EMVI Lightning protection . Bonding and grounding Wiring and cabling . Static electricity . Hazards of electromagnetic radiation to ordnance (HERO) +. Coupling factor (CF) . NOTES . Intended use . Issue of DODISS Consideration of data requirements . International

23、 standardization agreements . Subject term (key word) listing Changes from previous issue PAGE 27 27 27 28 28 28 28 28 28 28 29 29 29 29 29 29 29 28 29 29 32 32 32 32 32 32 32 vi Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-FIGURE MIL-STD-ZIIA 34

24、W 9999913 0306580 9 _ MIL-STD-2131A(AS) CON T E N TS 1. Wiring schematic to achieve primary and secondary release 2. CCU-43/B, CCU-44/B, CCU-45/B cartridge funct time vs applied current TABLE PAGE . 25 oni ng 26 I. External electromagnetic environment . . 30 a standardization agreements . 32 II. Par

25、agraphs containing internationa vi i Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-2131A 14 9999911 0106581 O MIL-STD-2131A(AS) 1. SCOPE 1.1 establishing general criteria for the design, development, construction, maintenance and testing of

26、 an ejection launcher. to all missile suspension systems. However, it is assumed that all new missile developments will employ a 14-inch or 30-inch missile suspension system as defined in MIL-A-8591. The launcher shall provide for the carriage, service and power ejection release of an airborne guide

27、d missile with either a nuclear or conventional warhead from tactical aircraft in flight. Scope. The purpose of this document is to provide guidelines for This standard is applicable 1 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-213LA 14

28、m 9999933 OLOb52 2 m MI L-STD-2131 A(AS) 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 document to the extent specified herein. Unless otherwise specified, the issues of the

29、se documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DODISS) and supplement therto, cited in the solicitation (see 6.2). SPECIFICATIONS FEDERAL L-P-383 Plastic Material, Polyester Resin, Glass Fiber Base, Low Pressure Laminated. QQ-A-367 Al u

30、mi num Al loy Forgi ngs . QQ-P-416 Plating, Cadmium (Electrodeposited). MILITARY MIL-S-5002 Surface Treatments and Inorganic Coatings for Metal Surfaces of Weapons Systems. MI L-B-5087 Bonding, Electrical, and Lightning Protection, For Aerospace Systems. MIL-W-5088 Wi ri ng , Aerospace Vehi cl e, MI

31、 L-C-5541 Chemical Conversion Coatings on Aluminum and Aluminum Al loys. MIL-H-5606 Hydraulic Fluid, Petroleum Base, Aircraft, Missile and Ordnance. MIL-S-6051 Electromagnetic Compatibility Requirements, Systems4 MIL-H-6088 MIL-H-6875 Heat Treatment of Steels, Process for. Heat Treatment of Aluminum

32、 Alloys. MIL-F-7179 Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems. 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NIL-STD-ZIJLA 34 9999933 0306583 4 m, _ SPECIFICATIONS MI LITaARY MI L-F-7 1 90 MIL-T-7743 MIL-B-7

33、883 MI L-1-8500 MIL-A-8591 MIL-A-8625 MI L-C-8837 MI L-P-15024 MIL-F-18264 MIL-N-18307 MI L-A-2 1 1 80 MIL-A-22771 MIL-T-31000 MI L-C-38999 MI L-L-4601 O MIL-H-46855 MI L-H-81200 MI L-D-81303 MI L-STD-2 1 31 A( AS 1 Forging, Steel, for Aircraft/Aerospace Equipment Appl i cations. Testing, Store Susp

34、ension and Release Equipment, General Specification for. Brazing of Steels, Copper, Copper Alloys, Nickel Alloys, Aluminum and Aluminum Alloys. Interchangeabi 1 i ty and Replaceabi 1 i ty of Component Parts for Aerospace Vehicles. Airborne Stores, Suspension Equipment and Aircraft-Store Interface (C

35、arriage Phase); General Design Criteria for. Anodic Coatings, for Aluminum and Aluminum Alloys. Coating, Cadmium (Vacuum Deposited). Plates, Tags and Bands for Identification of Equipment. Finishes, Organic, Weapons System, Application and Control of. Nomenclature and Identification for Aeronautical

36、 Systems Including Joint Electronics Type Designated Systems and Associated Support Systems. Aluminum Alloy Castings, High Strength. Al umi num Al loy Forgl ngs , Heat Treated. Technical Data Packages, General Specification for Connector, Electrical, Circular, Miniature High Density, Quick Disconnec

37、t (Bayonet Threaded and Breech Coupling), Environment Resistant, Removable Crimp and Hermetic Solder Contacts, General Specification for. Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting. Human Engineering Requirements for Mi 1 i tary Systems, Equipment and Facilities. Heat Treatment of Titan

38、ium and Titanium Alloys. Design and Evaluation of Cartridges for Stores Suspension Equipment. 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,- MIL-STD-2333A 14 m 999993L 0306584 b m MIL-STD-Z131A(AS) SPECIFICATIONS MI LI TARY MIL-F-83142 MIL-C-8548

39、5 STANDARDS MILITARY MI L-STD- 1 30 MI L-STD-454 MI L-STD-461 MIL-STD-462 MI L-STD-704 MIL-STD-81 O MI L-STD-838 MI L-STD-882 MIL-STD-889 MIL-STD-970 MIL-STD-1385 MIL-STD-1472 MI L-STD-1568 MIL-STD-1587 MIL-STD-1760 MIL-STD-2088 MIL-STD-2175 Forging, Titanium Alloys, Premium Quality. Cable, Electric

40、, Filter Line, Radio Frequency Absorptive. Identification Marking of U.S. Military Property. Standard General Requirements for Electronic Equipment. Electromagnetic Emission and Susceptibility Requirements for the Control of Electromagnetic Interference. Electromagnetic Interference Characteristics,

41、 Measurement of. Aircraft Electric Power Characteri sti cs. Environmental Test Methods and Engineering Guidelines. Lubrication of Military Equipment. System Safety Program Requirements. Dissimilar Metal s. Standards and Specifications, Order of Precedence for the Selection of. Preclusion of Ordnance

42、 Hazards in Electromagnetic Fi el ds, General Requirements for. Human Engineering Des,ign Criteria for Military Systems, Equipment and Facilities. Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems. Materials and Process Requirements for Air Force Weapon System

43、s. Ai rcraft/Store Electrical Interconnection System. Bomb Rack Unit (BRU), Aircraft, General Design Criteria for. Castings, Classification and Inspection of. 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-233LA 34 9999911 0306585 8 - MI L

44、-STD-2 1 31 A(AS) HANDBOOKS , MILITARY MIL-HDBK-5 Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-235-1 Electromagnetic (Radiated) Environment Considerations for Design and Procurement of Electrical and Electronic Equipment, Subsystems and Systems. BULLETINS MI LI TARY MIL

45、-BUL-147 Specifications and Standards of Non-Government Organizations Released for Flight Vehicle Design and Construction. (Unless otherwise indicated, copies of federal and military specifications, standards, handbooks, and bulletins are available from the Standardization Documents Order Desk, Buil

46、ding 4D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.) 2.1.2 Other Government documents. drawi nas, and pub1 i cations. other Government documents, drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified, the The fol lowing issues are th

47、ose cited in the solicitation. PUBLICATIONS NAVAL AIR SYSTEMS COMMAND (NAVAIR) AR-43 Electromagnetic Compat SD-24 General SDecification Requirement for. bi 1 i ty Advisory Board; or Design and Construction of Ai rcraf t Weapons Sys tems . 11-120A-1.2 Airborne Weapons Packaging/Handling/Stowage (Ship

48、board). 11 -1 40-24 Airborne Weapons Support Equipment, Description and Characteristics. 11 -1 40-25 1 9-1 -1 27 Armament Weapons Support Equioment Configuration. Non Avionics Preferred Common Support Equipment. 19-1 5BD-6 Technical Manual, “Description, Operation, and Maintenance Instruction with I

49、llustrated Parts Breakdown for Single Hoist Ordnance Loading System (SHOLS) . “ 1 9- 100-2 Airborne Weapons Handling Equipment (Shipboard). 5 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-CHIEF OF NAVAL OPERATIONS OPNAVINST 4790.2 Naval Aviation Maintenance Program. AI