1、5n . 12 APRIL 1988 MILITARY SPECIFICATION IGNITER, JET ASSISTED TAKE-OFF JATO) PROPULSION SYSTEM GENERAL DEVELOPMENT SPECIFICATION FOR This specification is approved for use within the Naval Air Systems Command, Department of the Naw, and is available for use by all departments and agencies of the D
2、epartment of Defense. 1. SCOPE 1.1 Purpose. This specification establishes the minimum requirements for the design, verification, and qualification of JATO rocket motor ignition systems, hereinafter referred to as “igniters.” The igniters are components of solid propellant rocket motors for JATO app
3、lications (see 6.1). Implicit within this specification are requirements for the shipping container design. 1.2 Igniter types. Igniters covered by this specification are of two types (see 6.2.1): Type I: Integral igniter Type II: Non-integral igniter Type I ,gniters are designed to be installed in t
4、he rocket motor at the time of manufacture and are designed to remain there for their entire life cycle. Type II igniters, on the other hand, are designed to be installed in the rocket motor by the user only at the time of use. Type II igniters are normally handled, shipped, and stored separately fr
5、om the rocket motor. 1.3 Integrated programs. If the igniter is being developed in conjunction wth a rocket motor, considerable savings in effort and resources may be achieved by integrating the requirements of MIL-R-85880 and this specification. 2. APPLICABLE DOCUMENTS e 2.1 Government documents. 2
6、.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 documents shall be those listed in the issue of the Department of Defense Index of S
7、pecifications and Standards (DoDISS) and supplement thereto, cited in the solicitation. SPECIFICATIONS FEDERAL TT-C-490 TT-P-1757 Cleaning Methods for Ferrous Surfaces and Pretreatments for Organic Coatings Primer Coating, Zinc Chromate, Low-Moisture-Sensitivity Beneficial comments (recommendations,
8、 additions, deletions) and any pertinent 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 (SESD) Code 53, Lakehurst, NJ 08733-5100, by using the self-addressed Standardizat
9、ion Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter. AMSC NIA FSC 1340 Distribution Statement A: Approved for public release: distribution is unlimited. THIS DOCUMENT CONTAINS 3 I PAGES. Licensed by Information Handling ServicesMILITARY MIL-P-116 DOD-D
10、-1000 M IL-S-5002 MIL-C-5541 MIL-H-6088 MIL-H-6875 M I L-F-7179 MIL-F-7190 MIL-S-7742 M 11-8-7883 MIL-1-8500 MIL-W-8611 M I L-A-8625 MIL-F-18264 M I L-A-21180 MIL-P-23377 MIL-1-23659 M IL-S-45743 MIL-W-46132 MIL-H-46855 MIL-R-81128 M IL-H-81200 M IL-C-83286 MIL-A-83377 MIL-R-85880 STANDARDS FEDERAL
11、MILITARY DOD-UD-100 MIL-STD-129 MIL-6TD-130 MIL-STD-331 MIL-STD-453 DOD-STD-480 MIL-STD-490 MIL-STD-648 MIL-STD-785 MIL-919-810 Preservation, Methods of Drawings, Engineering and Associated Lists Surface Treatments and Inorganic Coatings for Metal Surfaces of Weapons Systems Chemical Conversion Coat
12、ings on Aluminum and Aluminum Alloys Heat Treatment of Aluminum Alloys Heat Treatment of Steels, Process for Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems Forgings, Steel, for Aircraft/Aerospace Equipment and Special Ordnance Applications Screw Threads, Standard, O
13、ptimum Selected Series: General Specification for Brazing of Steels, Copper, Copper Alloys, Nickel Alloys, Aluminum and Aluminum Alloys Interchangeability and Replaceability of Component Parts for Aerospace Vehicles Welding, Metal Arc and Gas, Steels, and Corrosion and Heat Resistant Alloys; Process
14、 for Anodic Coatings, for Aluminum and Aluminum Alloys Finishes: Organic, Weapons System, Application and Control of Aluminum-alloy Castings, High Strength Primer Coatings: Epoxy-Polyamide, Chemical and Solvent Resistant Initiators, Electric, General Design Specification for Soldering, Manual Type,
15、High Reliability, Electrical and Electronic Equipment Welding, Fusion, Electron Beam, Process for Human Engineering Requirements for Military Systems, Equipment and Facilities Rocket Motors, Identification of Parts and Assemblies, Requirements for Heat Treatment of Titanium and Titanium Alloys Coati
16、ng, Urethane, Aliphatic Isocyanate, for Aerospace Applications Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for Rocket Motor, Jet Assisted Take-off (JATO) Propulsion System, General Development Specification for Ccrew-Thread Standards for Federal Services Engineering D
17、rawing Practices Marking for Shipment and Storage Identification Marking of US. Military Property Fuze and Fuze Components, Environmental and Performance Tests for Inspection, Radiographic Configuration Control - Engineering Changes, Deviations and Waivers Specification Practices Design Criteria for
18、 Specialized Shipping Containers Reliability Program for Systems and Equipment Development and Production Environmental Test Methods and Engineering Guidelines 2 Licensed by Information Handling ServicesMIL-1-85889 13 7797906 0366347 5 MlL-C85889(AS) t MIL-STD-838 MI L-STD-882 M IL-STD-889 MIL-STD-9
19、61 MI L-STD-970 MIL-STD-980 MI L-STD-1251 MIL-STD-1252 M IL-STD-1472 M IL-STD-1515 MI L-STD-1521 MI L-STD-1598 MIL-STD-1648 MI L-STD-1661 MIL-STD-1670 MIL-STD-1754 M I L-STD-1755 MIL-STD-1756 MIL-STD-1758 MIL-STD-2100 DOD-STD-21 O1 DOD-STD-2105 HANDBOOKS MILITARY MIL-HDBK-5 M IL-H D BK-I 7 M I L-H D
20、 BK-23 M IL-H D BK-I32 M I L-H DBK-157 MI L-H DBK-691 MIL-HDBK-694 MIL-HDBK-695 Lubrication of Military Equipment System Safety Program Requirements Dissimilar Metals Military Specifications and Associated Documents, Preparation of Standards and Specifications, Order of Preference for the Selection
21、of Foreign Object Damage (FOD) Prevention in Aerospace Products Screws and Bolts Preferred for Design, Listing of Inertia Friction Welding Process, Procedure and Performance Qualification Human Engineering Design Criteria for Military Systems, Equipment and Facilities Fastener Systems for Aerospace
22、Application Technical Reviews and Audits for Systems, Equipment, and Computer Software Studs Preferred for Design, Listing of Criteria and Test Procedures for Ordnance Exposed to an Aircraft Fuel Fire MARK and MOD Nomenclature System Environmental Criteria and Guidelines for Air-Launched Weapons Fas
23、tening Devices Preferred for Design, Listing of Keys and Pins Preferred for Design, Listing of Rings, Retaining, Preferred for Design, Listing of Insert, Screw Thread, Preferred for Design, Listing of Propellant, Solid, Characterization of (Except Gun Propellant) Classification of Characteristics Ha
24、zard Assessment Tests for Navy Non-Nuclear Ordnance Metallic Materials and Elements for Aerospace Vehicle Structures Plastics for Aerospace Vehicles Structural Sandwich Composites Protective Finishes for Metal and Wood Surfaces Transportability Criteria Adhesive Bonding Aluminum and Aluminum Alloys
25、Rubber Products: Recommended Shelf Life 2.1.2 Other Gove rnment docu ments and pub lications. The following other Government documents and publications form a part of this specification to the extent specified herein. Unless otherwise specified, the issues shall be those in effect on the date of the
26、 solicitation. CODE OF FEDERAL REGULATIONS 14 CFR 49 46 CFR 146 Shipping 49 CFR 100-199 Aeronautics and Space Hazardous Materials, Regulations, Department of Transportation PUBLICATIONS INSTRUCTIONS NAVAIRINST 5100.7 Technical Guidance for Naval Air Systems Command Safety Programs for Explosive Ordn
27、ance, Laser Systems and Lithium Batteries 3 Licensed by Information Handling Services. MIL-1-85889 13 m 7777706 03bbL50 L Pi MI L-I-85889(AS) 4 NAVSEAINST 8010.5 N 4VSEAI N ST 802W Technical Requirements for Insensitive Munitions Department of Defense Explosives Hazard Classification Procedures .- O
28、THER DOCUMENTS NAVAIR 11-1-117 Identification of Ammunition NAVSEA OD 30393 NAVSEA OD 44811 NAVSUP PUB 505 Design Principles and Practices for Controlling Hazards of Electromagnetic Radiation to Ordnance (HERO Design Guide) Safety and Performance Tests for Qualifications of Explosives Packaging and
29、Handling of Dangerous Material for Transportation by Military Aircraft (NOTAL) S 1 specifications, standards, handbooks, publications, and other Government documents required by contractors in connection with specific acquisition functions should be obtained from the contracting activity or as direc
30、ted by the contracting activity.) 2,2 Other publications. The following document forms a part of this specification to the extent specified herein. Unless otherwise indicated, the issue in effect on date of invifation for bids or request for proposal shall apply. AMERICAN NATIONAL STANDARDS INSTITUT
31、E (ANSI) ANSI Y145 Dimensioning intermittency of phase g. Probability of occurrence of environmental conditions h. Geographical location i. Any other information which will help identify environmental conditions which may act upon the igniter. The contractor shall include recommendations for the fol
32、lowing: a. Storage temperature lower limit (STLL) b. Storage temperature upper limit (STUL) c. Operating temperature lower limit (OTLL) d. Operating temperature upper limit (OTUL) The contractor shall determine whether helicopter transport is a part of the life cycle. Results of the life cycle envir
33、onmental analysis shall be made available to the contracting activity for acceptance. 4.2.2.2 Environmental design criteria and test plan. When specified in the contract or order, the contractor shall devise a plan which defines the specific environmental design and test requirements and includes an
34、 environmental test plan for Phases II and III. The contractor shall utilize the data obtained under provisions of 4.2.2.1. Consideration shall be given to the following: a. Probability of environmental occurrence, alone or in combination b. Expected effects and failure modes e. Effect on hardware p
35、erformance and mission success d. Likelihood of problems disclosure by the test methods e. Occurrence of similar environmental stress in more than one life profile phase f, Experience gained from other equipment similarly deployed The plan shall be made available to the contracting activity for acce
36、ptance. 4.2.2.3 Structural analysis. The contractor shall conduct a structural analysis of the igniter design considering the effects of pressure loads, acceleration loads, and any other significant sources of stress. The contractor shall include in the analysis all components which contribute to th
37、e structural integrity of the igniter. Results of the structural analysis shall be documented in the Design Development Report (see 4.2.3.5). 4.2.2.4 Thermal analysis. The contractor shall conduct a thermal analysis of the igniter design. The contractor shall consider the combined effects of self-ge
38、nerated heat as well as any significant external heat sources. The contractor shall consider all camponents which may serve as heat paths or which may be severely degraded by excessive heat. Results of the thermal analysis shall be documented in the Design Development Report (see 4.2.3.5). 4.2.25 Ba
39、llistic analysis. The contractor shall conduct a ballistics analysis of the igniter design to define expected performance. The contractor shall consider the effects of the operating temperature limits. Maximum expected operating pressure (MEOP) shall be calculated as part of the ballistics analysis.
40、 Results of the ballistics analysis shall be documented in the Design Development Report (see 4.2.3.5). 4.2.2.6 Interface analysis The contractor shall conduct an interface analysis of the igniter design to demonstrate that it satisfies all mechanical and electrical interface requirements. Results o
41、f the interface analysis shall be documented in the Design Development Report (see 42-35), 12 Licensed by Information Handling ServicesMIL-I-587 13 7997706 O366159 W - MlL-I-85889(AS) 4.2.2.7 Preliminary hazard analysis. When specified in the contract or order, the contractor shall prepare a prelimi
42、nary hazard analysis in accordance with Task 202 of MIL-STD-882 with emphasis on ordnance hazards. The hazard listings In NAVAIRINST 5100.7 should be used for guidance. The preliminary hazard analysis shall be made available to the contracting activity for acceptance. O 4.2.3 Documentation and revie
43、ws. 4.2.3.1 Program plan. When specified in the contract or order, the contractor shall prepare a program plan which identifies tasks, responsibilities, and schedule in accordance with the program structure specified in 3.1. The program plan shall be made available to the contracting activity for ac
44、ceptance no later than 60 days following initiation of Phase I. 4.2.3.2 System safety program plan. When specified in the contract or order, the contractor shall prepare a system safety program plan in accordance with Task 101 of MIL-STD-882. The system safety program plan shall be made available to
45、 the contracting activiy for acceptance no later than 90 days following initiation of Phase I. 4.2.3.3 Quality assurance plan. When specified in the contract or order, the contractor shall prepare a quality assurance plan for the entire program. The quality assurance plan shall be made available to
46、the contracting activity for acceptance no later than 30 days prior to the Preliminary Design Review. The contractor shall include provisions for the following: a. Serialization of all hardware and energetic components down to the piece part levels b. 100% inspection of all hardware and energetic co
47、mponents c. Traceability to constituent lot numbers d. Traceability of non-piece part constituents (liner materials, inhibitor materials, lubricants) e. Traceability of the fabrication tooling employed during manufacture f. Maintenance of “as-built” configuration lists g. X-ray inspection of environ
48、mental and static firing test units with sufficient detail to verify the presence and condition of all key components. 4.2.3.4 Marginality of success evaluation plan. When specified in the contract or order, the contractor shall prepare a marginality of success evaluation plan. The plan shall be des
49、igned to aid in the assessment of margins inherent in the design and to verify that tested units demonstrate no signs of incipient failure. The plan shall include provisions for the following: a. Prestatic firing X-ray and visual inspection b. Past-firing hardware examination for such things as dimensional changes, distortion, seal integrity, ejecta, etc. e. Comparison of actual versus predicted ballistic performance The plan shall be made available to the contracting activity for acceptance in Phase I 30 days prior to static firing the first igniter. 4.2.3.5 Design Development Repo
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