AIR FORCE JSSG-2010-12-1998 CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK [Superseded AIR FORCE AFGS-87141 B CANC NOTICE 1 CONT DIST. AIR FORCE AFGS-87141 .pdf

《AIR FORCE JSSG-2010-12-1998 CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK [Superseded AIR FORCE AFGS-87141 B CANC NOTICE 1 CONT DIST. AIR FORCE AFGS-87141 .pdf》由会员分享，可在线阅读，更多相关《AIR FORCE JSSG-2010-12-1998 CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK [Superseded AIR FORCE AFGS-87141 B CANC NOTICE 1 CONT DIST. AIR FORCE AFGS-87141 .pdf（129页珍藏版）》请在麦多课文档分享上搜索。

1、NOT MEASUREMENT r SENSITIVE JSSG-2010-12 30 October 1998 SUPERSEDING 14 April 1994 5 March 1986 25 February 1994 AFGS-87141 B MIL-P-8571 O(AS) MlL-STD-l776A(USAF) DEPARTMENT OF DEFENSE JOINT SERVICE SPECIFICATION GUIDE CREW SYSTEMS DEPLOYABLE AERODYNAMIC DECELERATOR (DAD) SYSTEMS HANDBOOK This speci

2、fication guide handbook is for guidance only. Do not cite this document as a requirement. AMSC 15GP DISTRIBUTION STATEMENT A. Approved for public release: distribution is unlimited. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2OLO-L2 II 9024

3、470 00OLL4 T97 811 JSSG-2010-12 FOREWORD JSSG RELEASE NOTE The specification guides support the acquisition reform initiative, and is predicated on a performance based business environment approach to product development. As such it is intended to be used in the preparation of performance specificat

4、ions. It is one of a set of specification guides. It is the initial release of this guide. In this sense this document will continue to be improved as the development program is accomplished. 1. 2. 3. 4. 5. This specification guide handbook is approved for use by all Departments and Agencies of the

5、Department of Defense (DoD). This Joint Service Specification Guide (JSSG) handbook, in conjunction with its companion JSSGs handbooks, is intended for use by Government and Industry program teams as guidance in developing program unique specifications. This handbook is for guidance only. This handb

6、ook cannot be cited as a requirement. If it is, the contractor does not have to comply. This document may not be placed on contract. The complete set of JSSGs, and their respective handbooks, establish a common framework to be used by Government-Industry Program Teams in the Aviation Sector for deve

7、loping program unique requirements documents for Air Systems, Air Vehicles, and major Subsystems. Each JSSG contains a compilation of candidate references, generically stated requirements, verification criteria, and associated rationale, guidance, and lessons learned for program team consideration.

8、The JSSGs identify typical requirements for a variety of aviation roles and missions. By design, the JSSG sample language for “requirements” and “verification criteria” are written as generic templates, with blanks that need to be completed in order to make the requirements meaningful. Program teams

9、 need to review the JSSG rationale, guidance, and lessons learned to: (1) determine which requirements are relevant to their application; and (2) fill in the blanks with appropriate, program-specific requirements. This document is Part 2 of two parts. Part 1 of the JSSG-2010 is a template for develo

10、ping the program unique performance specification. As a generic document, it contains requirement statements for the 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

11、blanks must be filled in for the program unique specification to form a complete and consistent set of requirements to meet program objectives. Part 2 of the JSSG-201 O is a handbook which provides the rationale, guidance, and lessons learned relative to each statement in Part 1. The section 4, veri

12、fication requirements, must be tailored to reflect an understanding of: (1) the design solution; (2) the identified program 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 o

13、f the required products and processes. It must be recognized that the rationale, guidance, and lessons learned are not only 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

14、tools. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: ASUENSID, Bldg. 560, 2530 Loop Road West, Wright-Patterson AFB OH 45433-7101, by using the Standardization Document Improvement Proposal (D

15、D Form 1426) appearing at the end of this document or by letter. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-PARAGRAPH 1. 1.1 2. 2.1 2.2 2.2.1 2.2.2 2.3 2.4 3. 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 3.9 3.1 O 3.1 1 3.12 3.12.1 3.12.1 -1 3.12.1.2 3.1 2.1

16、.3 3.1 2.2 3.1 2.2.1 3.12.2.2 3.12.2.3 3.1 3 3.1 4 4. 5. 5.1 5.1.1 5.1.2 5.1.3 5.1.4 5.1.5 JSSG-ZOLO-LZ H 9024490 RROOLL5 923 1811 JSSG-2010-12 CONTENTS PAGE SCOPE Scope. APPLICABLE DOCUMENTS General. Government documents. Specifications, standards, and handbooks. Other Government documents, drawing

17、s, and publications. Non-Government publications. Order of precedence. REQUIREMENTS Crew Systems Engineering (see JSSG-2010-1). Crew Systems Automation, Information, and ControllDisplay Management (see JSSG-2010-2). CockpitlCrew StationlCabin (see JSSG-2010-3). Aircrew Alerting (see JSSG-2010-4). Ai

18、rcraft Lighting (see JSSG-2010-5). Sustenance and Waste Management (S s/s by MIL-STD-464) Heat Treatment of Aluminum Alloys (Canceled, Heat Treatment of Steel, Process For Ink, Marking (for Parachutes and Other Textile Items) (Canceled, sls by A-A-59291) Finishes, Coatings, and Sealants for the Prot

19、ection of Aerospace Weapons Systems (Canceled, s/s by MIL-STD-7179) Forging, Steel, for AircrafVAerospace Equipment and Special Ordnance Applications Parachutes, Personnel, Detail Manufacturing Instructions For Brazing of Steels, Copper Alloys, Nickel Alloys, Aluminum and Aluminum Allows (Canceled;

20、future acquisitions should specify one: Interchangeability and Replaceability of Component Parts for Aerospace Vehicles (Canceled) Welding, Metal Arc and Gas, Steels and Corrosion and Heat Resistant Alloys (Canceled; s/s by MIL-STD-2219) Anodic Coatings for Aluminum and Aluminum Alloys Drawings, Eng

21、ineering and Associated Lists (Inactive for New Design; use MIL-DTL- 31 000) Finishes: Organic, Weapons Systems, Application and Control Of Aluminum Alloy Castings, High Strength Cartridges for Cartridge Actuated Devices, Design and Evaluation Of Aluminum Alloy Forgings, Heat Treated Design and Eval

22、uation of Cartridge Actuated Devices Initiators, Electrical, General Design Specification For Technical Data Packages S/S by SAE AMs-H-6088) AWSC3.4, AWSmC3.5, AWSC3.6, AWSC3.7) 2 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-2010-12 81 702447

23、0 0000121 127 m JSSG-2010-12 MIL-PRF-5511 O MIL-H-81200 MIL-C-83488 MIL-S-85076 MIL-P-8571 O MIL-C-87115 STAN DARDS FEDERAL FED-STD-H28 FED-STD-191 FED-STD-595 FED-STD-751 DEPARTMENT OF DEFENSE MIL-STD-130 MI L-STD-461 MI L-STD-462 MI L-STD-464 MIL-STD-470 MIL-STD-756 MIL-STD-785 MIL-STD-81 O MIL-ST

24、D-858 MI L-STD-882 MIL-STD-889 Printed Wiring Board, Rigid, General Specification For Heat Treatment of Titanium and Titanium Alloys Coating, Aluminum, Ion Vapor Deposited System, Automatic, Water Activated Parachute Release, Detail Specification For (Canceled) Parachutes, Personnel Emergency Escape

25、 General Design Specification For Coating, Immersion Zinc Flake/Chromate Dispersion (Inactive for New Design) Screw Thread Standards for Federal Services Textile Test Methods Colors Used in Government Procurement Stitches, Seams, and Stitching Identification Marking of US. Military Property Requirem

26、ents for the Control of Electromagnetic Interference Emissions and S usce pt i bi I it y Measurement of Electromagnetic Interference Characteristics, Test Method Standard For Electromagnetic Environmental Effects Requirements for Systems Maintainability Program for Systems and Equipment (Canceled, C

27、IS by MIL-HDBK-470) Reliability Modeling and Prediction Canceled) Reliability Program for Systems and Equipment Development and Production (Canceled) Test Method Standard for Environmental Engineering Considerations and Laboratory Tests Testing Standard for Personnel Parachutes (Canceled) System Saf

28、ety Program Requirements Dissimilar Metals 3 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-JSSG-20LO-LZ 7024490 0000122 063 6 MIL-STD-1252 MIL-STD-1385 MIL-STD-1472 DOD-STD-1866 MIL-STD-2067 MIL-STD-2175 MIL-STD-2219 MIL-STD-7179 DEPARTMENT OF DEFE

29、NSE MIL- H D BK-5 MIL-HDBK-132 MI L-HDBK-470 JSSG-2010-12 Inertia Friction Welding Process, Procedure and Performance Qualification Inactive for New Design) Preclusion of Ordnance Hazards in Electromagnetic Fields, General Requirements For (Canceled, sls by MIL-STD-464) Human Engineering Soldering P

30、rocess General (Non-Electrical) (Canceled) Aircrew Automated Escape Systems Reliability and Maintainability (R/M) Program Requirements For Castings, Classification and Inspection Of Fusion Welding for Aerospace Applications Finishes, Coatings, and Sealants for the Protection of Aerospace Weapons Sys

31、tems Metallic Materials and Elements for Aerospace Structures Protective Finishes for Metal and Wood Surfaces of Weapons Systems (Canceled) Maintainability Program for Systems and Equipment (Unless otherwise indicated, copies of the above specifications, standards, and handbooks are available from t

32、he Standardization Document Order Desk, 700 Robbins Ave., Bldg 4D, Philadelphia PA 191 1 1-5094.) 2.2.2 Other Government documents, drawings, and publications. The following other Government documents, drawings, and publications form a part of this document to the extent specified herein. 49 CFR 171

33、 -1 78 DEPARTMENT OF TRANSPORTATION Transportation FAA TSO-C23 (Copies of 49 CFR are available from the Government Printing Office (GPO), P.O. Box 371954, Pittsburgh PA 15250-7954 and copies of FAA TSO-C23 are available from the Department of Transportation, FAA Aeronautical Center, AML-611, P.O. Bo

34、x 25082, Oklahoma City OK 731 25-5082.) NAVAL WEAPONS CENTER (NWC) SK 13-01 8-001 -85 Parachute Volume Measurement Fixture NWC TP 6575 Parachute Recovery Systems Design Manual 4 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NAVAL AIR SYSTEMS COMMAN

35、D (NAVAIR) NAVAIR 13-1 -6.2 Aviation-Crew Systems Manual-Organization, Intermediate and Depot Level Maintenance with Illustrated Parts Breakdown for Emergency Personnel and Drogue Parachute Systems AS-46 1 3 W S-6536 Application and Derating Requirements for Electronic Components, General Specificat

36、ion For Procedures and Requirements for Preparation and Soldering of Electrical Connections (Copies are available from the Naval Weapons Center (NWC), ATTN: Technical Library, Code 3432, China Lake CA 93555-6001. Copies of the Aeronautical Specifications (AS) are available from the Naval Inventory C

37、ontrol Point (NAVICP), Code 33343.1 O, 700 robbins Ave., Phiadelphia PA 191 11-5098 and copies of the Weapons Specifications (WS) are available from the Defense Automated Printing Service (DAPS), ATTN: DoDSSP, Code NPP-9, Bldg 4/D, 700 Robbins Ave., Philadelphia PA 191 11-5094. AIR FORCE AFFDL-TR-78

38、-151 Recovery Systems Design Guide T.O. 14D3-11-1 Operation, Inspection, Maintenance, and Packing Instructions for Emergency Personnel Recovery Parachute (Chest, Back, Seat Style, and Torso Harness) Inspection, Repair, and Packing Instructions, Drogue Parachute Assembly, Part Numbers: J114712-501, J

39、114712-503, and J114712-505 T.O. 14D1-3-316 (Copies of TRs are available from the Defense Technical Information Center (DTIC), 8725 John J. Kingman Rd., Ste 0944, Fort Belvoir VA 22060-621 8. Copies of TOS are available from OC- ALCTTILUB, 7851 Arnold St., Ste 209, Tinker AFB OK 73145-9147.) IRIG 10

40、6 Telemetry Standards INTERRANGE INSTRUMENTATION GROUP (IRIG) IRIG 118 Test Methods for Telemetry Systems and Subsystems (Copies are available from: Range Commanders Council, ATTN: STEWS-SA-R, White Sands Missile Range NM 88002-51 1 O.) 2.3 Non-Government publications. The following document(s) form

41、 a part of this document to the extent specified herein. Unless otherwise specified, the issue of the documents which are DoD adopted are those listed in the issue of the DoDISS, and supplement thereto. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,

42、-JSSG-2010-12 AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM D 2261 ASTM D 2262 Standard Test Method for Tearing Strength of Fabrics by the Tongue (Single Rip) Procedure (Constant-Rate-of-Extension Tensile Testing Mach ne) Standard Test Method for Tearing Strength of Woven Fabrics by the Ton

43、gue (Single Rip) Met hod (Constant-Rate-of-Traverse Tensile Testing Machine) (DoD adopted) (Application for copies should be addressed to the American Society for Testing and Materials, 1 O0 Barr Harbor Dr., West Conshohocken PA 19428-2959.) AMERICAN WELDING SOCIETY (AWS) AWS-C3.4 Torch Brazing (DoD

44、 adopted) AWS-C3.5 Brazing, Induction (DoD adopted) AWS-C3.6 Furnace Brazing (DoD adopted) AW S-C3.7 Aluminum Brazing, Specification For (DoD adopted) (Application for copies should be addressed to the American Welding Society, 550 N. LeJeune Rd., Ste 100, Miami FL 331 26-5699.) SOCIETY OF AUTOMOTIV

45、E ENGINEERS (SAE) AMs-H-6088 Heat Teatment of Aluminum Alloys AS 8015 Minimum Performance Standards for Parachute Assemblies and Components, Personnel (Application for copies should be addressed to the Society of Automotive Engineers, Inc, 400 Commonwealth Dr., Warrendale PA 15096-0001 .) 2.4 Order

46、of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 3. REQUIREMENTS 3.1 Cr

47、ew Systems Engineering (see JSSG-2010-1). 3.2 Crew Systems Automation, Information, and ControllDisplay Management (see JSSG-2010-2). 3.3 CockpiUCrew StationlCabin (see JSSG-2010-3). 3.4 Aircrew Alerting (see JSSG-2010-4). 3.5 Aircraft Lighting (see JSSG-2010-5). 6 Provided by IHSNot for ResaleNo re

48、production or networking permitted without license from IHS-,-,-JSSG-2010-12 m 9024470 0000125 872 m JSSG-2010-12 3.6 Sustenance and Waste Management (S for example: “The parachute shall be designed for auxiliary deceleration of the F-1 O00 aircraft during landing roll out.“ The functional definitio

49、n of the parachute or decelerator subassembly should be stated in the second blank to define the scope of the effort. For example: in the case of a personnel parachute, the acquisition may be only for a new parachute canopy, in another case, it may be for a canopy, and container, in another case it may be for a complete system of harness, container, and canopy. A functional definition should reflect the scope of the acquisition, .e., The term “