AIR FORCE MIL-STD-1576-1984 ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS《空间系统的电子系统的安全要求和试验方法》.pdf
《AIR FORCE MIL-STD-1576-1984 ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS《空间系统的电子系统的安全要求和试验方法》.pdf》由会员分享,可在线阅读,更多相关《AIR FORCE MIL-STD-1576-1984 ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS《空间系统的电子系统的安全要求和试验方法》.pdf(148页珍藏版)》请在麦多课文档分享上搜索。
1、3 MIL-STD-157b SA W 797991L 0063635 O d MIL-mSTD-1576 (USAF) 31 JULY t984 MLITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS NO DELIVERABLE DATA REQUIRED BY THIS DOCUMENT Provided by IHSNot for ResaleNo reproduction or networking permitted without lice
2、nse from IHS-,-,-MIL-STD-LS76 SA W 74777LL 00b3b3b 2 W MIL-STD- 15 7 6 ( USAF 31 July 1984 DEPARTMENT OF THE AIR FORCE Washington, D C 20330 Electroexplosive Subsystems Safety Requirements and Test Methods for Space Sys teas MIL-STD-1576 (USAF). 1. This Military Standard is approved for use by the D
3、epartment 0.f the Air Force, and is available for use by all Departments and Agencies of the Department of Defense. 2. Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addreased to: Hq SD/ALM, Box 92960, Los A
4、ngeles, CA 90009 by using the self-addressed Standardization Document Improvement Proposal (DD 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-,-,-MIL-STD-1576 (USAI?) 31 July 1984 FOREWORD T
5、his St.anqard establishes the general requirements and test methods for the design and development of electroexplosive subsystems to preclude hazards from unintentional initiation and from failure to fire. These requirements apply to all subsystems utilizing electrically initiated explosive or pyrot
6、echnic components. This Standard applies to all space vehicle systems (e.g., launch vehicles, upper stages, boosters, payloads, and related systems). iii Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-1576 (USAI?). 31 July 1984 THIS PAGE LEF
7、T BLANK INTENTIONALLY Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-1576 SA 7977911 00b3637 B -i Paragraph _- . 1.0 1.1 1.2 1*2.1 1.3 . 1.4 2.0 2.1 2.2 3.0 3.1.1 3.1.2 3.1.3 3.1.5 3.1 . 3.i.4 3.1.8 3.1.9 3.1.-10 3.1.11 I 3.1.12 3.1.13 3.1.1
8、4 . 3.1.-15 3.1.16 3.1.17 3 1 . 19 3.1.20 3.1.21 3.1.18 3.1022 3.1.23 3.1.24 3.1.25 3.1.26 3.1.27 3.1.2a 3.1.29 3.1.30 3.1.31 3.1.32 3.1.33 3.1.34 MIL-STD-1576 (USAF) 31 July 1984 CONTENTS Page SCQPE . . 1 Purpose . - . 1 TestMethods . -1 Revision of Test Methods . 1 Application . 1 . Minimum Requir
9、ements 2 REFERENCED DOCUMENTS o v o 0% . . 3 IssueS.of Documents 3 . Other Publications 4 DEFINITIONS 7 Termsused 7 Arm/Disarm (A/D) Device . 7 Bridgewire 7 Catastrophic Hazard 7 Conductive Mix 7 Conductive Mix EED 7 Critical Hazard 7 Dudding 7 Electroexplosive Device (EED) - 7 Electroexplosive Subs
10、ystem (EES) . 8 Exploding Bridgewire (EBW) Device . 9 . 8 Exploding Foil Device a Explosiv Train (Explosive Transfer Assembly) D 8 Firing Circuits . 8 . Firing Control Circuit . . . . . 8 Firing Output Circuit 8 Firing Source a Firing Source Circuit 8 Host.Vehcle. 8 Isolation Filter/Isolation Filter
11、 Connection Radio Frequency (RF) . . 10 Maximum No-Fire Level .- . 10 Monitor Circuit . 10 NASA Standard Initiator (NSI) . . . . 10 Non-Standard Parts. Materials. and Processes . . v 10 Optical Coverage 10 Payload 10 Production Lot 10 RotorLead 10 Safety Critical Function . i 10 Safe and Arm (SM) De
12、vice . 11 SafePlug 11 Safe/ArmPlug 11 AmPlUg 0.0 b 0.0 7 Electromagnetic Environment . .- .I . a Minimum All-Fire Level Safe and Arm devices, Arm/Disarm switches, relays and all electrical . wiring used to monitor, control, arm and fire ordnance are specifically included. This Standard applies to al
13、l space vehicle systems (e.g., launch vehicles, upper stages, boosters, payloads, and related systems using EEDs). 1.2 TestMethods. The test methods described herein have been prepared to: a. Specify laboratory test conditions for electroexplosive subsystems and components which will produce test re
14、sults that are equivalent to those which would beexperienced in the actual operational environ-. ment and which will permit reproducibility of test results. e b. Describe all test methods for electroexplosive subsystems and comppnents needed to ensure compliance with the requirements of the speclf i
15、cation. . c. Provide Test Method 2208 as a Standard method far RF dudding evaluation if required by the procuring activity. 1.2.1 Revision of Test Methods. Revisions of each test method shall be indicated by a revision number following the method numbr. For example., the first revision of Test Metho
16、d 1101 would be 1101.1, the second revision would be 1101.2, et cetera. 1.3 Application. This Standard is applicable to the entire electroexploaive subsystem life cycle, up. to the time when the electroexplosive subsystem no longer presents a hazard to personnel, launch site facilities and manned or
17、 reusable space systems, This Standard a-lso applies to expendable launch vehicles which present these types of hazards. a. This. Standard is intended to be used by procuring activities for . establishing all of the electroexplosive subsystem safety requirements to be included in specifications fort
18、he design and development of new hardware for new or old space systems. b. This Standard is intended to be uaed by procuring activities and government safety organization for a safety evaluation of previously -1- Provided by IHSNot for ResaleNo reproduction or networking permitted without license fr
19、om IHS-,-,-MIL-STD-1576 SA m 9499931 OOd3bLc Methods of Testing (5.2) Colors (5.12.6) Test Methods.for Electronic and Electrical Component Parts (Method 1111) Nondes truc tive Testing Personnel . Qualification and Certification (Eddy . Current, Liquid Penetrant, Magnetic Particle, Radiographic and U
20、ltrasonic) (Method 1404) . . Inspection, Radiographic (Method 1103) Ammunition Data Card (4.6) . Lot Numbering of Ammunition (4.6) Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-MIL-STD-L576 SA 99949LL 0063650 7 MIL-STD-1512 MIL-STD-1546 MIL-STD-154
21、7 MIL-STD-1576 (USAF) 31 July 1984 Electroexplosive Subsystems, Electrically Initiated, Design Requirements and Test Methods (l.3.d, Appendix 50.2.1, 50.2.1.3) Parts, Materials, and Processes Standardization, Control and Management Program for Spacecraft and Launch Vehicles (3.1.38, 4.5.1, 4.5.3, 4.
22、5.4, 6.9.1, 6.9.2) Technical Requirements for Parts, Materials, and Processes for Spacecraft and Launch Vehicles (6.8.3) PUBLICATIONS DOD DOD 5154 a 4s Ammunition and Explosive Safety Standards (6.5) ADL-TD-3 DOD Authorized Data List (6.11) APTO 11A-1-47 Explosive Hazard Classification Procedures (6
23、.5) (Copies of specifications , standards, drawings, and publications required by contractors in connection with specific procurement functions should be obtained from the contracting activity or as directed by the contracting of f icer) 2.2 Other Publications. The following documents form a part of
24、 this standard to the extent specified herein. Unless otherwise indicated, the issue in effect on date of invitation for bids or request for proposal shall apply. AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM) ASTM E-545 Determining Image Quality in Thermal Neutron Radiographic Testing (Method 14
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