REG NASA-STD-8719 24 ANX W CHG 2-2012 ANNEX TO NASA-STD 8719 24 NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS REQUIREMENTS TABLE.pdf

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1、 NASA TECHNICAL STANDARD ANNEX (with Change 2) to NASA-STD 8719.24 National Aeronautics and Space Administration Washington, DC 20546 Approved: 2011-08-26 Change 2 Approved: 2012-06-19 ANNEX TO NASA-STD 8719.24 NASA EXPENDABLE LAUNCH VEHICLE PAYLOAD SAFETY REQUIREMENTS: REQUIREMENTS TABLE Requests f

2、or relief from the requirements in this document are processed through the NASA Safety and Mission Assurance Technical Authority APPROVED FOR PUBLIC RELEASE DISTRIBUTION IS UNLIMITED Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Annex to NASA-STD-8

3、719.24- Initial Issue with Change 2 FOREWORD This Annex to NASA-STD 8719.24 is published by the National Aeronautics and Space Administration (NASA) as the template for developing project range safety programs after removal of this cover page. For background on the development of the requirements se

4、t below, see the base NASA-STD 8719.24. Comments and questions concerning the contents of this publication should be referred to the National Aeronautics and Space Administration, Director, Safety and Assurance Requirements Division, Office of Safety and Mission Assurance, Washington, DC 20546 or vi

5、a “Feedback” in the NASA Technical Standards System at http:/standards.nasa.gov. /s/ August 26, 2011 Bryan OConnor Approval Date Chief, Safety and Mission Assurance Change 1 approved: _Wilson B. Harkins_ dated: January 26, 2012Change 2 approved: _ dated: _ DOCUMENT HISTORY LOG Status Document Revisi

6、on Approval Date Description Baseline 2011-08-26 Initial Release (JWL4) Annex Change 1 2012-01-26 - Page 3: Corrected PSWG Chair signature block; - Pages 187 Vol 3, para13.1.1.1 and Vol 7, removed revision from ST/SG/AC.10.1; - Vol 7 page 404, bolded “hazardous materials” definition header (JWL4) An

7、nex Change 2 2012-06-19 Throughout document: Corrected 18 typographical errors (Administrative Change) (JWL4) This document is subject to reviews per Office of Management and Budget Circular A-119, Federal Participation in the Development and Use of Voluntary Standards (02/10/1998) and NPR 7120.10,

8、Technical Standards for NASA Programs and Projects. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TAILORED REQUIREMENTS FOR PROJECT Name From: NASA-STD-8719.24 Ch 1 Annex Ch 2, June 19, 2012 Logo PROJECT NAME XXX XX Month 201X Revision: X PROJECT N

9、AME SAFETY REQUIREMENTS Prepared for: NASA Center Under contract: Contract Number COMPLIANCE WITH THIS PUBLICATION IS MANDATORY Prepared by: Companys Name Companys Address Companys Phone Number _ _ Prepared by (Name) Name Preparer Title Project Manager Organization NASA Center Date: _ Date: _ _ _ Na

10、me Name Project SMA Technical Authority Launch Services Program SMA Technical Authority NASA Center NASA Center Date: _ Date: _ _ _ Name Name Organization Payload Safety Working Group Chairperson Date: _ Date: _ Provided by IHSNot for ResaleNo reproduction or networking permitted without license fro

11、m IHS-,-,-TAILORED REQUIREMENTS FOR PROJECT Name Page 4 of 412 From: NASA-STD-8719.24 Ch 1 Annex Ch 2, June 19, 2012 FOREWORD The Original Text column of the following requirements matrix contains the NASA Expendable Launch Vehicle (ELV) payload safety requirements that are to be tailored for each N

12、ASA ELV payload project, as required by NPR 8715.7, “Expendable Launch Vehicle Payload Safety Program.” The NASA ELV payload safety requirements are the result of a joint effort by NASA and U.S. Air Force Range Safety representatives (30thand 45thSpace Wings) to establish an approved baseline from A

13、FSPCMAN 91-710, “Range Safety User Requirements,” and applicable NASA safety requirements and also address unique issues associated with NASA payload safety design and operations. The NASA ELV payload safety requirements apply to all NASA ELV payload projects launched from an Air Force, NASA, or oth

14、er range/launch site. The NASA ELV payload safety requirements supplement NPR 8715.7 and satisfy AFSPCMAN 91-710 when applied to NASA ELV launches from Air Force launch ranges. As such, they provide a streamlined starting point for the safety requirements tailoring process that is required for each

15、NASA ELV payload project per NPR 8715.7. The NASA ELV payload safety requirements (as tailored for each specific project) are mandatory for each NASA ELV payload project and are to be applied to associated contracts and/or agreements. Additional requirements may be imposed by other organizations, in

16、cluding other launch ranges, commercial payload processing facility operators, or launch vehicle contractors. This document does not alter or otherwise modify the authority or roles and responsibilities delineated by statute or policy applicable to the Air Force, NASA, or other organizations partici

17、pating in a NASA ELV payload project. As outlined in ASPCMAN 91-710, the Space Wing Commanders have overall launch authority and responsibility for public safety at Air Force ranges. The Director, NASA Wallops Flight Facility has similar authority and responsibility for launches originating from Wal

18、lops Flight Facility. AFSPCMAN 91-710 requirements not applicable to NASA ELV payloads were eliminated from the following NASA ELV payload safety requirements tailoring matrix. This results in irregular numbering of paragraphs where certain paragraph(s) may appear to be skipped or missing because th

19、ey were not applicable. Additionally, in some cases entire inapplicable volumes or chapters may be missing and are not included in the tailoring matrix. The absence of these requirements does not alter the Air Force Range Safety authority. The project may add back any AFSPCMAN 91-710 requirements th

20、at are pertinent to their project upon agreement by the projects Payload Safety Working Group (PSWG) and Range Safety representatives. Questions pertaining to the requirements in this document and applicable local safety requirements should be brought to the attention of the payload projects PSWG. P

21、er NPR 8715.7, Payload Project Offices will contact the NASA ELV Payload Safety Manager as early as practical in the projects Concept and Technology Development, Phase A, to establish the projects PSWG and initiate the payload safety review and approval process, which includes the requirements tailo

22、ring process. The NASA ELV Payload Safety Manager is responsible for maintaining and keeping the NASA ELV payload safety requirements current and coordinating all changes with the NASA ELV Payload Safety Agency Team and the Air Force Range Safety 30thand 45thSpace Wing Safety Offices. The NASA ELV P

23、ayload Safety Manager contact information and the NASA ELV payload safety requirements tailoring matrix are available on the NASA ELV Payload Safety Program website at: http:/kscsma.ksc.nasa.gov/ELVPayloadSafety/Default.html. Note: This Foreword provides background information that is applicable to

24、all NASA ELV payload projects. It is not to be tailored and shall remain as part of each final project-specific safety requirements document. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TAILORED REQUIREMENTS FOR PROJECT Name Page 5 of 412 From: N

25、ASA-STD-8719.24 Ch 1 Annex Ch 2, June 19, 2012 TABLE OF CONTENTS1VOLUME 1: POLICIES AND PROCEDURES 12CHAPTER 1 INTRODUCTION 12 1.1 Objective . 12 1.2 Applicability . 13 1.3 Basis for the Requirements 14 CHAPTER 2 RESPONSIBILITIES AND AUTHORITIES . 15 2.1 General . 15 2.2 Headquarters Air Force Space

26、 Command Responsibilities 15 2.3 Space Wing Responsibilities 15 2.4 Federal Aviation Administration Responsibilities 16 2.5 Payload Project Responsibilities 16 CHAPTER 3 RANGE SAFETY POLICY 18 3.1 General . 18 3.2 Prelaunch and Launch Operations: 18 3.3 Launch Area Safety 18 3.4 Launch Complex Safet

27、y . 20 CHAPTER 4 PSWG and RANGE SAFETY PROCESSES . 21 4.1 Range Safety and Payload Projects Interface Process . 21 4.6 Equivalent Level of Safety (ELS) Determinations and Waivers 21 CHAPTER 5 SAFETY AUTHORIZATIONS, SAFETY APPROVALS, AND DOCUMENTATION 23 5.1 General . 23 CHAPTER 6 INVESTIGATING AND R

28、EPORTING MISHAPS AND INCIDENTS 24 6.1 Mishaps and Incidents Involving Air Force Personnel and Resources . 24 6.2 Non-Air Force Personnel and Resources on Air Force Property 24 6.3 Reporting Space Launch System Anomalies . 24 CHAPTER 7 CHANGES TO THIS PUBLICATION . 25 ATTACHMENT 1 THE NASA ELV PAYLOA

29、D SAFETY REQUIREMENTS TAILORING PROCESS 26 A1.1 Introduction: 26 A1.2 Tailoring Process 28 1This document follows the paragraph numbering used in AFSPCMAN 91-710 for applicable payload requirements. AFSPCMAN 91-710 requirements that are not applicable to NASA ELV payloads were eliminated, which resu

30、lted in an irregular numbering of paragraphs. In some cases, entire inapplicable volumes or chapters were not included in this document. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TAILORED REQUIREMENTS FOR PROJECT Name Page 6 of 412 From: NASA-S

31、TD-8719.24 Ch 1 Annex Ch 2, June 19, 2012 ATTACHMENT 2 SYSTEM SAFETY PROGRAM REQUIREMENTS 31 A2.1 Introduction . 31 A2.2 System Safety Program Tasks 31 ATTACHMENT 3 SUBMITTING NONCOMPLIANCE REQUESTS . 43 A3.1 Introduction . 43 A3.2 Submitting Noncompliance Requests 44 ATTACHMENT 4 ACCEPTABLE RISK CR

32、ITERIA . 46 A4.1 Introduction 46 VOLUME 3: PAYLOADS AND GROUND SYSTEMS REQUIREMENTS 47 CHAPTER 1 INTRODUCTION 47 1.1 General . 47 1.2 Organization of the Volume . 47 CHAPTER 2 RESPONSIBILITIES AND AUTHORITIES . 49 2.1 Payload Safety Working Group (PSWG) 49 2.2 Payload Project Responsibilities. . 49

33、CHAPTER 3 GENERAL DESIGN POLICY . 50 3.2 Systems Without Specific Design Criteria 50 CHAPTER 4 DOCUMENTATION REQUIREMENTS. 51 4.1 System Safety Plan Hazard Analyses 51 4.2 Safety Data Package (SDP) (MSPSP) . 51 4.3 SDP Associated Test Plans and Test Results 52 4.4 Nondestructive Examination Plans 52

34、 CHAPTER 6 MATERIAL HANDLING EQUIPMENT AND PERSONNEL WORK PLATFORMS 53 6.1 Material Handling Equipment 53 6.3 Removable, Extendible, and/or Hinged Personnel Work Platforms . 62 6.4 Lifting Personnel with a Crane 63 6.5 Flight Hardware Used to Lift Critical Loads and Clampbands. 63 CHAPTER 7 ACOUSTIC

35、 HAZARDS 65 7.1 Acoustic Design Standards. 65 7.2 Acoustic Data Requirements 65 CHAPTER 8 NON-IONIZING RADIATION SOURCES 66 8.1 Radio Frequency Emitters 66 8.2 Laser Systems . 68 CHAPTER 9 RADIOACTIVE (IONIZING) RADIATION SOURCES . 73 9.1 Radioactive Source Design Standards and Controls . 73 9.2 Rad

36、ioactive Sources Carried on Payloads . 74 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TAILORED REQUIREMENTS FOR PROJECT Name Page 7 of 412 From: NASA-STD-8719.24 Ch 1 Annex Ch 2, June 19, 2012 CHAPTER 10 HAZARDOUS MATERIALS . 77 10.1 Hazardous Ma

37、terials Selection Criteria . 77 10.2 Hazardous Materials Test Requirements . 77 10.3 Hazardous Materials Environmental Requirements 78 10.4 Hazardous Materials Data Requirements 78 10.5 Process Safety Management and Risk Management Plan 78 CHAPTER 11 GROUND SUPPORT PRESSURE, VACUUM, AND HAZARDOUS ST

38、ORAGE SYSTEMS . 79 11.1 Ground Support Pressure Vacuum and Storage Systems Requirements 79 11.2 Ground Support Pressure Systems Requirements . 79 11.3 Ground Support Pressure Systems Certification and Recertification . 113 CHAPTER 12 FLIGHT HARDWARE PRESSURE SYSTEMS AND PRESSURIZED STRUCTURES 118 12

39、.1 Flight Hardware Pressure System and Pressurized Structure General Requirements. . 118 12.2 Flight Hardware Pressure Vessel Design, Analysis, and Test Requirements . 140 12.4 Flight Hardware Special Pressurized Equipment Design, Analysis, and Test Requirements. . 153 12.5 Flight Hardware Pressure

40、System Component Design and Test Requirements . 159 12.6 Flight Hardware Pneumatic System Design Requirements. . 171 12.7 Flight Hardware Hydraulic System Design and Test Requirements. . 174 12.8 Flight Hardware Hypergolic Propellant System Design and Test Requirements 176 12.9 Flight Hardware Cryog

41、enic Systems Design and Test Requirements 179 12.10 Flight Hardware Pressure Systems Data Requirements 184 CHAPTER 13 ORDNANCE SYSTEMS . 187 13.1 Ordnance Hazard Classification . 187 13.2 Ordnance System General Requirements 188 13.3 Ordnance Electrical Circuits 189 13.4 Initiator Electrical Circuit

42、s . 193 13.5 Ordnance Safety Devices . 194 13.6 Ordnance Initiating Devices . 201 13.7 Explosive Transfer Systems and Receptor Ordnance . 205 13.8 Ordnance Test Equipment 206 13.9 Ordnance and Non-Explosive Initiator Data Requirements 208 CHAPTER 14 ELECTRICAL AND ELECTRONIC EQUIPMENT . 209 14.1 Ele

43、ctrical and Electronic Ground Support Equipment and Flight Hardware General Design Requirements and Standards 209 14.2 EGSE Design Requirements 214 14.3 Electrical and Electronic Flight Hardware . 219 CHAPTER 15 MOTOR VEHICLES . 222 15.1 General 222 15.2 Motor Vehicles Other Than Lift Trucks 222 15.

44、3 Lift Trucks 223 CHAPTER 16 COMPUTER SYSTEMS AND SOFTWARE. 225 16.1 General 225 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-TAILORED REQUIREMENTS FOR PROJECT Name Page 8 of 412 From: NASA-STD-8719.24 Ch 1 Annex Ch 2, June 19, 2012 16.2 Determina

45、tion of Safety Critical Computer System Functions . 226 16.3 Hardware and Software Safety Design Requirements 226 16.4 Software Requirements 230 16.5 Computer System and Software Data Requirements 232 CHAPTER 17 WESTERN RANGE SEISMIC DESIGN 233 17.1 Applicability of Design and/or Anchorage or Restra

46、int Requirements 233 17.2 Basis for Design 233 17.3 WR Seismic Data Requirements 235 17.4 Earthquake Emergency Planning and Post Recovery Response . 235 CHAPTER 18 SOLID ROCKET MOTORS, ROCKET MOTOR SEGMENTS, AND ROCKET MOTOR COMPONENTS 236 18.1 General . 236 18.2 Failure Modes, Effects, and Critical

47、ity Analysis (FMECA) and Operational Hazards Analysis (OHA) . 236 18.3 Lightning Effects Hazard Analysis 236 18.4 Solid Rocket Motor and Motor Segment Data Requirements 236 ATTACHMENT 1 SAFETY DATA PACKAGE (MISSILE SYSTEM PRELAUNCH SAFETY PACKAGE) 237 A1.1 Introduction . 237 A1.2 Preparation Instruc

48、tions 237 A1.4 Modifications to the Safety DATA PACKAGE (SDP) 264 ATTACHMENT 2 HANDLING STRUCTURES INITIAL AND PERIODIC TEST REQUIREMENT FLOWPATH . 265 ATTACHMENT 3 HAZARD AREA CLASSIFICATION . 267 VOLUME 6: GROUND AND LAUNCH PERSONNEL, EQUIPMENT, SYSTEMS, AND MATERIAL OPERATIONS SAFETY REQUIREMENTS . 270 CHAPTER 1 INTRODUCTION 271 1.1 Applicability . 271 1.2