NAVY MIL-R-85880-1988 ROCKET MOTOR JET ASSISTED TAKE-OFF (JATO) PROPULSION SYSTEM GENERAL DEVELOPMENT SPECIFICATION FOR《起飞助推器系统的火箭发动机的一般发展规定》.pdf

1、- c_ MIL-R-BSO 13 M 9777906 03bbL11 2 - 12 APRIL 1988 MILITARY SPECIFICATION ROCKET MOTOR, 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 us

2、e by all departments and agencies of the Department of Defense. 1. SCOPE 1.1 Purpose. This specification establishes the minimum requirements for the design, verification and qualification of auxiliary booster propulsion systems, hereinafter referred to as “booster.” Although this specification appl

3、ies to the complete auxiliary booster propulsion system, specific components and parts are addressed to a limited extent. Implicit within this specification are requirements for the shipping container design (see 6.1). 2. APPLICABLE DOCUMENTS 2.1 Government documents. 2.1.1 Specifications, standards

4、, 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 Specifications and Standards (D

5、ODISS) and supplement thereto, cited in the solicitation. SPECIFICATIONS O FEDERAL TT-(2-490 TT-P-1757 MILITARY M IL-P-116 DOD-D-1000 MIL-S-5002 MIL-(3-5541 MIL-H-6088 MIL-H-6875 MI L-F-7179 MIL-F-7190 M 114-7742 Cleaning Methods and Pretreatment of Ferrous Surfaces for Organic Coatings Primer Coati

6、ng, Zinc Chromate, Low-Moisture-Sensitivity Preservation, Methods of Drawings, Engineering and Associated Lists Surface Treatments and Inorganic Coatings for Metal Surfaces of Weapons Systems Chemical Conversion Coatings on Aluminum and Aluminum Alloys Heat Treatment of Aluminum Alloys Heat Treatmen

7、t of Steels, Process for Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Systems Forgings, Steel, for AircraWAerospace Equipment and Special Ordnance Applications Screw Threads, Standard, Optimum Selected Series: General Specification for 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 Standardiza

9、tion 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 ?)b PAGES. - -=_ - - -A - Provided by IHSNot for ResaleNo reproduction or n

10、etworking permitted without license from IHS-,-,-MIL-R-85880 13 9 777770b 03bblL2 LI m M I L-6-7883 M IL-1-8500 MIL-W-8611 M I L-A-8625 M I L-F-18264 MIL-A-21180 MI L-P-23377 M I L-W-461.32 MIL-H-46855 M IL-M-63018 M IL-R-81128 M I L-H-81200 M IL-C-83286 MIL-A-83377 MIL-1-85889 STAN DARDS FEDERAL FE

11、D-STD-H28 MILITARY DOD-STD-100 M I L-STD-129 MIL-STD-130 MIL-STD-143 M IL-STD-331 M IL-STD-453 DOD-STD-480 MIL-STD-490 M IL-STD-648 M I L-STD-785 MIL-STR-810 MIL-STD-838 M I L-STD-882 M IL-STD-889 M IL-STD-961 M IL-STD-980 MIL-STD-1251 M I L-STD-1252 MIL-STD-1385 M I L-STD-1472 MI L-STD-1515 MIL-STD

12、-1521 MIL-STD-1598 MIL-STD-1648 MIL-STD-1661 MIL-STD-1670 MIL-R-85880(AS) A -/ Brazing of Steels, Copper, Copper Alloys, Nickel Alloys, Aluminum and Aluminum 1 e Alloys Interchangeability and Replaceability of Component Parts for Aerospace Vehicles Welding, Metal Arc and Gas, Steels, and Corrosion a

13、nd Heat Resistant Alloys; ProceCs 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 Welding, Fusion, Electron Beam, Process for Hu

14、man Engineering Requirements for Military Systems, Equipment and Facilities Manual, Technical: Nonnuclear Explosive Ordnance Disposal Rocket Motors, Identification of Patts and Assemblies, Requirements for Heat Treatment of Titanium and Titanium Alloys Coating, Urethane, Aliphatic Isocyanate, for Ae

15、rospace Applications Adhesive Bonding (Structural) for Aerospace and Other Systems, Requirements for Igniter, Jet Assisted Take-off (JATO) Propulsion System, General Development Specification for Screw-Thread Standards for Federal Services Engineering Drawing Practices Marking for Shipment and Stora

16、ge Identification Marking of US Military Property Standards and Specifications, Order of Preference for the Selection of Fuze and Fuze Components, Environmental and Performance Tests for Inspection, Radiographic Configuration Control - Engineering Changes, Deviations and Waivers Specification Practi

17、ces Design Criteria for Specialized Shipping Containers Reliability Program for Systems and Equipment Development and Production Environmental Test Methods and Engineering Guidelines Lubrication of Military Equipment System Safety Program Requirements Dissimilar Metals Military Specifications and As

18、sociated Documents, Preparation 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 Preclusions of Ordnance Hazards in Electromagnetic Fields; General Require- ment

19、s for Human Engineering Design Criteria for Military Systems, Equipment and Facilities Fastener Systems for Aerospace Application Technical Reviews and Audits for Systems, Equipments, and Computer Software Studs Preferred for Design, Listing of Criteria and Test Procedures for Ordnance Exposed to an

20、 Aircraft Fuel Fire MARK and MOD Nomenclature System Environmental Criteria and Guidelines for Air-Launched Weapons 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-HDBK-5 MIL-HDBK-17 M IL-H DBK-23 M IL-H DBK-132 MIL-HDBK-157 M IL-HDBK-691 MIL-H

21、DBK-694 MIL-HDBK-695 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 Rubber Products: Recommended Sh

22、elf Life I MIL-R-5O 13 9797906 03bbLL3 b W - - MI L-R-85880(AS) MI L-STD-1756 M I L-STD-1758 M IL-STD-2100 DO D-STD-21 O1 DOD-STD-2105 Rings, Retaining, Preferred for Design, Listing of Insert, Screw Thread, Preferred for Design, Listing of Propellant, Solid, Characterization of (Except Gun Propella

23、nt) Classification of Characteristics Hazard Assessment Tests for Navy Non-Nuclear Ordnance HANDBOOKS MILITARY 2.1.2 Other Goernment documents and publications. The following other Government documents, and pub- lications form a part of this specification to the extent specified herein. Unless other

24、wise specified, the issues shall be those in effect on the date of the-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 OPNAVINST 3401.3 NAVAIRINST 510

25、0.7 NAVSEAINST 8010.5 Nuclear Survivability of Navy and Marine Corps Systems Technical Guidelines for Naval Air Systems Command Safety Programs for Explosive Ordnance,! Laser Systems and Lithium Batteries Technical Requirements for Insensitive Munitions NAVSEAINST 8020.8 Department of Defense Explos

26、ives Hazard Classification Procedures OTHER DOCUMENTS NAVAIR 11-1-117 Identification of Ammunition NAVSEA OD44811 Safety and Performance Tests for Qualifications of Explosives NAVSUP PUB 505 Packaging and Handling of Dangerous Material for Transportation by Military Aircraft (NOTAL) (Copies of speci

27、fications, 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 directed by the contracting activity.) a 3 Provided by IHSNot for ResaleNo reproduction or ne

28、tworking permitted without license from IHS-,-,-flIL-R-85BBO lI3 W 979770b 03bbL14 B MIL-R-85880(AS) L- P k (Copies of specifications, standards, handbooks, publications, and other Government documents required by contractors in connection with specific acquisition functions should be obtained from

29、the contracting activity or as directed by the contracting activity.) 2.2 Other publications. The following document forms a part of this specification to the extent specified here in. Unless otherwise indicated, the issue in effect on date of invitation for bids or request for proposal shall apply.

30、 AMERICAN NATIONAL STANDARDS INSTITUTE (ANSI) ANSI Y145 Dimensioning intermittency of phase g. Probability of occurrence of environmental conditions h. Geographical location i. Any other information whichwill help identify environmental conditions which may act upon the booster. The contractor shall

31、 include recommendations for the following: a. Storage temperature lower limit (STLL) b. Storage temperature upper limit (STUL) c. Operating temperature lower limit (OTLL) d. Operating temperature upper limit (OWL) The contractor shall determine whether helicopter transport is a part of the life cyc

32、le. Results of the life cycle environmental profile 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

33、 test requirements and includes an environmental test plan for Phases II and 111. The contractor shall utilize the data obtained under provisions of 4.2.2,i. Consideration shall be given to the following: a. Probability of environmental occurrence, alone or in combination b. Expected effects and fai

34、lure modes c. ffect on hardware performance 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

35、the contracting activity for acceptance. 4.2.2.3 Structural analysis. The contractor shall conduct a structural analysis of the booster design considering the effects of pressure loads, acceleration loads and any other significant sources of stress. The contractor shall include in the analysis all c

36、omponents which contribute to the structural integrity of the booster and shall include a thorough stress analysis of the propellant grain. The stress analysis shall consider the stress and strain requirements of the propellant grain during post-cure cool down, temperature cycling, and ignition. Res

37、ults of the structural analysis shall be documented in the Design Development Report (see 4.2.3.5). shall consider the combined effects of self-generated heat as well as any significant external heat sources. The contractor shall consider all components which may serve as heat paths or which may be

38、severely degraded by excessive heat. Results of the thermal analysis shall be documented in the Desigri Development Report (see 4.2,3.5). 4.2.2.5 Ballistic analysis. The contractor shall conduct a ballistics analysis of the booster-design to define expected performance. The kontractor shall consider

39、 the effects of the operating temperaturepiimits. Maximum expected operating pressure (MEOP) shall be calculated as part of the ballistics analysis. Results of the ballistics analysis shall be documented in the Design Development Report (see 4.2.3.5). 4.2.2.4 Thermal analysis. The contractor shall c

40、onduct a thermal analysis of the booster desi 14 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-4.2.2.6 Thrust alignment analysis. The contractor shall conduct a thrust alignment analysis to demonstrate that the booster design satisfies the thrust a

41、lignment requirements specified in the acquisition documents (see 6.2.1). Results of the thrust alignment analpis shall be documented in the Design Development Report (see 4.2.3.5). 4.2.2.7 Interface analysis. The contractor shall conduct an interface analysis of the booster design to demon- strate

42、that it satisfis all mechanical and electrical interface requirements. Results of the interface analysis shall be documented in the Design Development Report (see 4.2.35). 4.2.2.8 Preliminary hazard analysis. When specified in the contract or order, the contractor shall prepare a preliminary hazard

43、analysis in accordance with Task 202 of MIL-STD-882 with emphasis on ordnance hazards. The preliminary hazard analysis shall be made available to the contracting activity for acceptance. 4.2.3 Documentation and reviews. 4.2.3.1 Program plan. When specified in the contract or order, the contractor sh

44、all 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 acceptance no later than 60 days following initiation of Phase i. 4.2.3.2 System safety

45、 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 the contracting activity for acceptance no later than 90 days following initiation o

46、f 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 the contracting activity for acceptance no later than 30 days prior to the Prelimina

47、ry Design Review. He shall include provisions for the following: a. Serialization of all hardware and energetic components down to the piece part levels. b. 100 percent inspection of all hardware and energetic components c. Traceability to constituent lot numbers d. Traceability of non-piece part co

48、nstituents (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 environmental and static firing test units with sufficient detail to verify the presence and

49、condition of all key components h. Hydrostatic proof pressure testing of each pressure vessel. 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 designed 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 in- clude provisions for the following: a. Prestatic fi