AIR FORCE JSSG-2009 A-2013 AIR VEHICLE SUBSYSTEMS.pdf

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1、 JSSG-2009A 20 November 2013 SUPERSEDING JSSG-2009 30 October 1998 DEPARTMENT OF DEFENSE JOINT SERVICE SPECIFICATION GUIDE AIR VEHICLE SUBSYSTEMS This specification guide is for guidance only. Do not cite this document as a requirement. AMSC N/A FSC 15GP DISTRIBUTION STATEMENT A. Approved for public

2、 release; distribution is unlimited. NOT MEASUREMENT SENSITIVE Comments, suggestions, or questions on this document should be addressed to AFLCMC/ENRS, 2145 MONAHAN WAY, WRIGHT-PATTERSON AFB OH 45433-7017 USA or e-mailed to AFLCMC.ENEZ.ENGINEERING.STANDARDSWPAFB.AF.MIL. Since contact information can

3、 change, you may want to verify the currency of this address information using the ASSIST Online database at https:/assist.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2009A ii FOREWORD JOINT SERVICE SPECIFICATION GUIDE (JSSG) RELEAS

4、E NOTE This specification guide is predicated on a performance-based business environment approach to product development. It is intended to be used in the preparation of performance specifications. The JSSG Suite includes this document; JSSG-2000, Air System; JSSG-2001, Air Vehicle; JSSG-2005, Avio

5、nics; JSSG-2006, Structures; JSSG-2007, Engines; JSSG-2008, Vehicle Control and Management; JSSG-2010, Crew Systems; and JSSG-2011, Air Vehicle / Ship Integration. The JSSG Suite Compact Disc is available from AFLCMC/ENRS, 2145 MONAHAN WAY, WPAFB OH 45433-7017 USA; DSN 674-5476; COMMERCIAL (937) 904

6、-5476; AFLCMC.ENEZ.ENGINEERING.STANDARDSWPAFB.AF.MIL. The following direction and guidance is applicable to this document: 1. This specification guide, in conjunction with its companion JSSGs, is intended for use by Government and Industry program teams as guidance in developing program-unique speci

7、fications. This document may not be placed on contract. 2. The complete set of JSSGs establish a common framework to be used by Government-Industry Program Teams in the Aviation Sector to develop program-unique requirements documents for Air Systems, Air Vehicles, and major Subsystems. Each JSSG con

8、tains a compilation of candidate references; generically-stated requirements; verification criteria; and associated rationale, guidance, and lessons learned for the program teams consideration. The JSSGs identify typical requirements for a variety of aviation roles and missions. By design, the JSSG

9、sample language for “requirements” and “verification criteria“ are written as generic templates, with blanks that need to be completed to make the requirements meaningful. Program teams need to review the JSSG rationale, guidance, and lessons learned to: (1) determine which requirements are relevant

10、 to their application; and (2) fill in the blanks with appropriate, program-specific requirements. 3. This document consists of two parts. Part 1 of this document is a template to develop the program-unique performance specification. As a generic document, it contains requirement statements for the

11、full range of aviation sector applications. It must be tailored to delete non-applicable requirements to form the program-unique specification. In addition, where blanks exist, these blanks must be filled-in for the program-unique specification to form a complete and consistent set of requirements t

12、o meet program objectives. Part 2 of this document is a handbook which provides the rationale, guidance, and lessons learned relative to each statement in Part 1. The section 4 verification requirements must be tailored to reflect an understanding of: (1) the design solution, (2) the identified prog

13、ram milestones, (3) the associated level of maturity which is expected to be achieved at those milestones, and (4) the specific approach to be used in the design and verification of the required products and processes. It must be recognized that the rationale, guidance, and lessons learned are not o

14、nly generic in nature but also document what has been successful in past programs and practices. This must not be interpreted to limit new practices, processes, methodologies, or tools. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2009A iii P

15、ART 1 CONTENTS 1. SCOPE . 1 1.1 SCOPE . 1 1.2 STRUCTURE . 1 1.3 HANDBOOK . 1 1.4 DEVIATIONS 1 1.5 ENVIRONMENTAL IMPACT 1 1.6 RESPONSIBLE ENGINEERING OFFICE 2 2. APPLICABLE DOCUMENTS . 2 2.1 GENERAL 2 2.2 GOVERNMENT DOCUMENTS 2 2.2.1 SPECIFICATIONS, STANDARDS, AND HANDBOOKS 2 2.3 ORDER OF PRECEDENCE

16、. 3 2.4 STREAMLINING . 3 3. REQUIREMENTS . 4 3.1 DEFINITION . 4 3.1.1 FUNCTIONAL DIAGRAM . 4 3.1.2 INTERFACE DRAWING . 4 3.2 CHARACTERISTICS 4 3.2.1 SECURITY . 4 3.2.2 COMPUTER RESOURCES . 4 3.2.3 OBSERVABLES . 5 3.2.3.1 ELECTROMAGNETIC EMISSIONS . 5 3.2.4 SURVIVABILITY . 5 3.2.5 RELIABILITY 5 3.2.6

17、 MAINTAINABILITY . 5 3.2.7 INTEGRITY AND ENVIRONMENT 5 3.2.7.1 SERVICE LIFE AND USAGE . 5 3.2.7.1.1 DESIGN SERVICE LIFE 5 3.2.7.2 ENVIRONMENT . 5 3.2.7.3 CRASH WORTHINESS 6 3.2.7.4 MATERIALS AND PROCESSES . 6 3.2.7.4.1 COATINGS AND FINISHES . 6 3.2.7.4.2 PROHIBITED MATERIALS AND PROCESSES 6 3.2.7.4.

18、3 PRODUCIBILITY 6 3.2.7.4.4 DAMAGE TOLERANCE . 6 3.2.7.4.4.1 SAFETY AND MISSION CRITICAL FUNCTIONS . 6 3.2.7.4.4.2 DAMAGE TOLERANT - FAIL SAFE EVIDENT SUBSYSTEMS AND COMPONENTS . 6 3.2.7.4.4.3 MECHANICAL COMPONENT DAMAGE TOLERANCE 6 3.2.7.5 STRENGTH 7 3.2.7.6 DURABILITY AND ECONOMIC LIFE 7 3.2.7.6.1

19、 CORROSION . 7 3.2.7.6.2 HIGH CYCLE FATIGUE (HCF) 7 3.2.7.6.3 LOW CYCLE FATIGUE (LCF) 7 3.2.7.6.4 DIELECTRIC MATERIALS . 7 3.2.7.6.5 CREEP . 7 3.2.8 TRANSPORTABILITY 7 3.2.9 INTEGRATED DIAGNOSTICS . 7 3.2.9.1 FAULT DETECTION AND ISOLATION 8 3.2.10 NAMEPLATE AND PRODUCT MARKING . 8 Provided by IHSNot

20、 for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2009A iv 3.3 DESIGN AND CONSTRUCTION . 8 3.3.1 INTERCHANGEABILITY 8 3.3.2 NON-INTERCHANGEABILITY . 8 3.3.3 SAFETY 8 3.3.3.1 SAFETY CRITERIA 8 3.3.3.2 FOREIGN OBJECT DAMAGE (FOD) 9 3.3.3.3 SOFTWARE SAFETY 9 3.3.3.4 A

21、COUSTIC NOISE . 9 3.3.4 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3) . 9 3.3.5 STANDARDIZATION 9 3.3.6 ENVIRONMENTAL . 9 3.3.7 HEALTH . 9 3.3.8 INSTALLATION HAZARDS REDUCTION . 9 3.4 SUBSYSTEM CHARACTERISTICS 10 3.4.1 LANDING SUBSYSTEM 10 3.4.2 HYDRAULIC POWER SUBSYSTEM . 10 3.4.3 AUXILIARY POWER SUBS

22、YSTEM . 10 3.4.4 ENVIRONMENTAL CONTROL SUBSYSTEMS 10 3.4.5 FUEL SUBSYSTEM . 10 3.4.6 AERIAL REFUELING SUBSYSTEM 10 3.4.7 FIRE AND EXPLOSION HAZARD PROTECTION SUBSYSTEM . 10 3.4.8 ELECTRICAL POWER SUBSYSTEM 10 3.4.9 MECHANICAL SUBSYSTEMS 10 3.4.10 CARGO, AERIAL DELIVERY, AND SPECIAL OPERATIONS SUBSYS

23、TEM . 10 3.4.11 VERTICAL TAKEOFF AND LANDING SHORT TAKEOFF AND LANDING POWER DRIVE SUBSYSTEMS . 10 3.4.12 PROPELLER SUBSYSTEM . 11 3.4.13 PNEUMATIC SUBSYSTEM . 11 3.4.14 ADDITIONAL SUBSYSTEMS AND FUNCTIONS 11 4. VERIFICATION 12 4.1 DEFINITION . 12 4.1.1 FUNCTIONAL DIAGRAM . 12 4.1.2 INTERFACE DRAWIN

24、G . 12 4.2 CHARACTERISTICS 12 4.2.1 SECURITY . 12 4.2.2 COMPUTER RESOURCES . 12 4.2.3 OBSERVABLES . 12 4.2.3.1 ELECTROMAGNETIC EMISSIONS . 12 4.2.4 SURVIVABILITY . 12 4.2.5 RELIABILITY 12 4.2.6 MAINTAINABILITY . 12 4.2.7 INTEGRITY AND ENVIRONMENT 13 4.2.7.1 SERVICE LIFE AND USAGE . 13 4.2.7.1.1 DESI

25、GN SERVICE LIFE 13 4.2.7.2 ENVIRONMENT . 13 4.2.7.3 CRASH WORTHINESS 13 4.2.7.4 MATERIALS AND PROCESSES . 13 4.2.7.4.1 COATINGS AND FINISHES . 13 4.2.7.4.2 PROHIBITED MATERIALS AND PROCESSES 13 4.2.7.4.3 PRODUCIBILITY 13 Provided by IHSNot for ResaleNo reproduction or networking permitted without li

26、cense from IHS-,-,-JSSG-2009A v 4.2.7.4.4 DAMAGE TOLERANCE . 13 4.2.7.4.4.1 SAFETY AND MISSION CRITICAL FUNCTIONS . 13 4.2.7.4.4.2 DAMAGE TOLERANT - FAIL SAFE EVIDENT SUBSYSTEMS AND COMPONENTS 13 4.2.7.4.4.3 MECHANICAL COMPONENT DAMAGE TOLERANCE 14 4.2.7.5 STRENGTH 14 4.2.7.6 DURABILITY AND ECONOMIC

27、 LIFE 14 4.2.7.6.1 CORROSION . 14 4.2.7.6.2 HIGH CYCLE FATIGUE (HCF) 14 4.2.7.6.3 LOW CYCLE FATIGUE (LCF) 14 4.2.7.6.4 DIELECTRIC MATERIALS . 14 4.2.7.6.5 CREEP . 14 4.2.8 TRANSPORTABILITY 14 4.2.9 INTEGRATED DIAGNOSTICS . 14 4.2.9.1 FAULT DETECTION AND ISOLATION 14 4.2.10 NAMEPLATE AND PRODUCT MARK

28、ING . 14 4.3 DESIGN AND CONSTRUCTION . 15 4.3.1 INTERCHANGEABILITY 15 4.3.2 NON-INTERCHANGEABILITY . 15 4.3.3 SAFETY 15 4.3.3.1 SAFETY CRITERIA 15 4.3.3.2 FOREIGN OBJECT DAMAGE (FOD) 15 4.3.3.3 SOFTWARE SAFETY 15 4.3.3.4 ACOUSTIC NOISE . 15 4.3.4 ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3) . 15 4.3.5

29、 STANDARDIZATION 15 4.3.6 ENVIRONMENTAL . 15 4.3.7 HEALTH . 16 4.3.8 INSTALLATION HAZARDS REDUCTION . 16 4.4 SUBSYSTEM CHARACTERISTICS 16 4.4.1 LANDING SUBSYSTEM 16 4.4.2 HYDRAULIC POWER SUBSYSTEM . 16 4.4.3 AUXILIARY POWER SUBSYSTEM . 16 4.4.4 ENVIRONMENTAL CONTROL SUBSYSTEMS 16 4.4.5 FUEL SUBSYSTE

30、M . 16 4.4.6 AERIAL REFUELING SUBSYSTEM 16 4.4.7 FIRE AND EXPLOSION HAZARD PROTECTION SUBSYSTEM . 16 4.4.8 ELECTRICAL POWER SUBSYSTEM 16 4.4.9 MECHANICAL SUBSYSTEMS 16 4.4.10 CARGO, AERIAL DELIVERY, AND SPECIAL OPERATIONS SUBSYSTEM . 16 4.4.11 VERTICAL TAKEOFF AND LANDING SHORT TAKEOFF AND LANDING P

31、OWER DRIVE SUBSYSTEMS . 17 4.4.12 PROPELLER SUBSYSTEM . 17 4.4.13 PNEUMATIC SUBSYSTEM . 17 4.4.14 ADDITIONAL SUBSYSTEMS AND FUNCTIONS 17 5. PACKAGING 18 6. NOTES . 18 6.1 INTENDED USE . 18 6.2 ACQUISITION REQUIREMENTS 18 6.3 DEFINITIONS . 18 Provided by IHSNot for ResaleNo reproduction or networking

32、 permitted without license from IHS-,-,-JSSG-2009A vi 6.4 ACRONYMS . 23 6.5 SUBJECT TERM (KEY WORD) LISTING 24 6.6 CHANGES FROM PREVIOUS ISSUE . 25 6.7 RESPONSIBLE ENGINEERING OFFICE 25 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2009A 1 JOI

33、NT SERVICE SPECIFICATION GUIDE AIR VEHICLE SUBSYSTEMS This specification guide is approved for use by all Departments and Agencies of the Department of Defense. 1. SCOPE 1.1 Scope. This specification establishes the item definition, performance, operating characteristics, reliability, maintainabilit

34、y, physical characteristics, general design, installation, and interface requirements for Air Vehicle Subsystems. This specification also establishes the analysis, inspection, demonstrations, and test procedures required by the Using Service for satisfactory completion and acceptance of subsystem co

35、mponent qualifications at the SFR, PDR, CDR, FF, and SVR Milestones. This specification also establishes the content and format to be used by the Using Service or contractor for preparation of the acquisition or model specification. The (TBS) Air Vehicle is composed of airframe, propulsion, avionics

36、, crew station, flight controls, vehicle management system, and subsystems. This specification addresses only the subsystems. The purpose of (TBS) air vehicle subsystems is to provide mechanization, hydraulic, electrical, auxiliary, and pneumatic power, landing provisions, electronics and airframe c

37、ooling, fuel, and fire protection. 1.2 Structure. This specification complies with Guidance for Preparation and Use of Joint Services Guide Specifications, AEB 96-1. 1.3 Handbook. This specification has an accompanying tailoring handbook to be used for contractual purposes in the development of air

38、vehicle subsystems requirements. 1.4 Deviations. Deviations from this specification which will result in improvement of the system performance, reduced life cycle cost, reduced developmental cost, or where the requirements of this specification result in compromise in operational capability, should

39、be brought to the attention of the Using Service. 1.5 Environmental impact. Air Vehicle Subsystems will be designed such that their operation, maintenance, and repair may be accomplished without violating the most stringent environmental regulations applicable to locations where subsystems are used

40、or supported. Compliance with environmental regulations will not prevent subsystems from achieving and sustaining mission performance capability. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2009A 2 Materials, processes, and environmental con

41、trol equipment necessary to meet these environmental requirements must currently be available in the Using Services maintenance and supply system. The design will not use environmentally unsuitable materials such as ozone depleting fluorocarbons, chlorofluorocarbons, and halons, or highly volatile o

42、rganic compounds in solvents and coatings during development, production, operation, maintenance, or repair. The Environmental Protection Agency maintains an online list of toxic chemicals and hazardous substances on its Ozone Layer Depletion Website at http:/www.epa.gov/ozone/snap/ that should be c

43、onsulted. The Significant New Alternatives Policy (SNAP) Program available thereon identifies substitutes for ozone depleting chemicals. The contractor will conduct an environmental analysis of air vehicle subsystems. 1.6 Responsible engineering office. The responsible engineering office (REO) for t

44、his specification is AFLCMC/EZFA, WRIGHT-PATTERSON AFB, OH 45433-7017; DSN 785-2023, COMMERCIAL (937) 255-2023; AFLCMC.EZF.MAILBOXUS.AF.MIL. 2. APPLICABLE DOCUMENTS 2.1 General. The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not inc

45、lude documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements of documents cited in sections

46、3, 4, or 5 of this specification, whether or not they are listed. 2.2 Government documents 2.2.1 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

47、se documents are those cited in the solicitation or contract. DEPARTMENT OF DEFENSE SPECIFICATIONS JSSG-2000 Air System Joint Service Specification Guide JSSG-2001 Air Vehicle Joint Service Specification Guide DEPARTMENT OF DEFENSE STANDARD MIL-STD-130 Identification Marking of U.S. Military Propert

48、y Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2009A 3 (Copies of these documents are available online at http:/quicksearch.dla.mil or from the Standardization Document Order Desk, 700 Robbins Avenue, Bldg 4D, Philadelphia PA 19111-5094.) 2.3 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document t