AIR FORCE DOD-HDBK-343-1986 DESIGN CONSTRUCTION AND TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT《一类空间设备的设计 制造及测试设备》.pdf
《AIR FORCE DOD-HDBK-343-1986 DESIGN CONSTRUCTION AND TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT《一类空间设备的设计 制造及测试设备》.pdf》由会员分享,可在线阅读,更多相关《AIR FORCE DOD-HDBK-343-1986 DESIGN CONSTRUCTION AND TESTING REQUIREMENTS FOR ONE OF A KIND SPACE EQUIPMENT《一类空间设备的设计 制造及测试设备》.pdf(80页珍藏版)》请在麦多课文档分享上搜索。
1、DOD-HDBK-343 (USAF)01 FEBRUARY 1986MILITARY HANDBOOKDESIGN, CONSTRUCTION, AND TESTINGREQUIREMENTS FORONE OF A KIND SPACE EQUIPMENTNO DELIVERABLE DATA REQUIREDBY THIS DOCUMENT FSC 1810DISTRIBUTION STATEMENT A Approved for public release: distribution unlimited.Provided by IHSNot for ResaleNo reproduc
2、tion or networking permitted without license from IHS-,-,-DOD-HDBK-343 (USAF)01 FEBRUARY 1986DEPARTMENT OF THE AIR FORCEWashington, D.C. 20330Design, Construction, and Testing Requirementsfor One of a Kind Space Equipment1. This Military Handbook is approved for use by theDepartment of the Air Force
3、, and is available for use by allDepartments and Agencies of the Department of Defense.2. Beneficial comments (recommendations, additions,deletions) and any pertinent data which may be of use inimproving this document should be addressed to:USAF Space Division, SD/ALMP. o. Box 92960Worldway Postal C
4、enterLos Angeles, CA 90009-2960by using the self-addressed Standardization Document ImprovementProposal (DD Form 1426) appearing at the end of this document orby letter.iiProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-DOD-HDBK-343 (USAF)01 FEBRUARY
5、1986The high reliability required of all space equipment isachieved by the designs, design margins, and by themanufacturing process controls imposed at each and every levelof assembly. The design and design margins should assure thatthe space equipment is capable of performing in the spaceenvironmen
6、t . The manufacturing process controls are intended toassure that a known quality product is manufactured to meet thedesign requirements and that any changes required can be madebased on a known baseline. Attention to every detail isrequired throughout development, manufacture. qualification.transpo
7、rtation. and preflight testing to assure successfuloperations of the space equipment.For high-priority, long-life. complex space equipment, highreliability is usually achieved by strict compliance to themilitary specifications and standards that document therequirements and good practices needed to
8、achieve long life.Programs for these types of space equipment are generallystructured to provide extensive checks and balances. withdetailed reviews of each step by independent personnel. toassure that no problem is overlooked. Particular attention isgiven in the design to eliminating single-point f
9、ailure modes,wherever practicable. Special design analysis, specialscreening during manufacturing.and other quality provisionsthat will assure reliability are implemented on any remainingsingle-point failure items to avoid latest defects. For theseprograms. a full qualification program is conducted
10、on each ofthe components, on each of the space experiments, and on eachspace vehicle involved.Not all space equipment is high priority or long life.Many space programs are for a single mission that is of shortduration, and the equipment may be relatively simple, or involveonly one experiment.When co
11、mpared to long-life, more complexprograms,these one of a kind space programs often presentexcellent opportunities to save substantial time and money inthe acquisition. There is still a requirement for highreliability, because a flight failure in space is seldom costeffective.The real problem is to i
12、dentify those cost-savingmeasures that are reasonable for each program and that will notincrease risks in an unacceptable way. This military handbookis intended to address those issues and various other facets ofengineering information pertinent to requirements for one of akind space equipment. The
13、handbook provides the basis for aconsistent technical approach for such programs in order toachieve,in a cost-effective way, the high reliability required.The material presented is intended as a baseline of requirementsthat should be tailored to the needs of each program.iiiProvided by IHSNot for Re
14、saleNo reproduction or networking permitted without license from IHS-,-,-DOD-HDBK-343 (USAF)01 FEBRUARY 1986FOREWORD (continued)Section 1, Scope. states the purpose of this handbook.Section 2 is the list of documents referenced in the text of thehandbook. Section 3 presents definitions for various c
15、lasses ofspace programs and equipment, as well as the definitions for thevarious levels of assembly terms used. Note that the programcharacteristics imposed by the statement of work and datadelivery requirements of the acquisition contract determine theprogram class. The equipment characteristics im
16、posed by theprogram peculiar specifications referenced in the acquisitioncontract determines the equipment class. There is no requirementthat the equipment class and the program class be the same.That could be the case, but almost any mix can be visualized tomeet unique program requirements. Section
17、 4 presents a seriesof tables comparing typical attributes of the various classes toprovide a summary overview that may be helpful. Tables I, II,and III are matrices of some of the baseline program ormanagement related items that may be used by the government indefinitizing the Statement of Work or
18、other contract provisionsfor various classes of programs.In contrast. Tables IV through IX are matrices thatsummarize the technical requirements presented in detail inSections 5 through 10 of this handbook for various classes ofvehicles or experiments.A program peculiar specification for acertain cl
19、ass of space equipment would typically incorporate thegeneral technical requirements by extracting or referencing theapplicable requirements from Sections 5 through 10 of thishandbook. For the convenience of those preparing spaceequipment specifications,these sections of the handbook addressthe requ
20、irements in essentially the same sequence. format, andorganization that would be addressed in a program peculiarspecification. Section 5 addresses equipment characteristics,Section 6 general design requirements,Section 7 requirementsfor computer resources. Section 8 manufacturing requirements.Sectio
21、n 9 storage and handling requirements, and Section 10addresses quality assurance provisions.Section 11, Notes,provides guidance information on tailoring of requirements andon the classification process.The requirements documented here for one of a kind spaceequipment were given guidance from several
22、 NASA and Air Forcedocuments. In particular. the Experimenters Planning Guide forDepartment of Defense Space Test Program (The Air Force SpaceDivision Report SD-TR-83-24) should be used in coordination withthis document in that it provides many lessons learned fromflying one of a kind experiments ov
23、er the last twenty years. Inaddition. this Experimenters Planning Guide includes furtherguidance for integration, launch and orbit operations support.ivProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-DOD-HDBK-343 (USAF)01 FEBRUARY 1986CONTENTSProvide
24、d by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-DOD-HDBK-343 (USAF)01 FEBRUARY 1986CONTENTS (Continued)viProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-DOD-HDBK-343 (USAF)01 FEBRUARY 1986CONTENTS (Continued
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