1、541 Commercial Space Transportation, FAA, DOT Pt. 417 APPENDIX B OF PART 415SAFETY REVIEW DOCUMENT OUTLINE This appendix contains the format and numbering scheme for a safety review docu-ment to be filed as part of an application for a launch license as required by subpart F of part 415. The applica
2、ble sections of parts 413, 415, and 417 of this chapter are referenced in the outline below. SAFETY REVIEW DOCUMENT 1.0 Launch Description (415.109) 1.1 Launch Site Description 1.2 Launch Vehicle Description 1.3 Payload Description 1.4 Trajectory 1.5 Staging Events 1.6 Vehicle Performance Graphs 2.0
3、 Launch Operator Organization (415.111) 2.1 Launch Operator Organization (415.111 and 417.103 of this chapter) 2.1.1 Organization Summary 2.1.3 Organization Charts 2.1.4 Office Descriptions and Safety Func-tions 3.0 Launch Personnel Certification Program (415.113 and 417.105 of this chapter) 3.1 Pro
4、gram Summary 3.2 Program Implementation Document(s) 3.3 Table of Safety Critical Tasks Per-formed by Certified Personnel 4.0 Flight Safety (415.115) 4.1 Initial Flight Safety Analysis 4.1.1 Flight Safety Sub-Analyses, Methods, and Assumptions 4.1.2 Sample Calculation and Products 4.1.3 Launch Specif
5、ic Updates and Final Flight Safety Analysis Data 4.2 Radionuclide Data (where applicable) 4.3 Flight Safety Plan 4.3.1 Flight Safety Personnel 4.3.2 Flight Safety Rules 4.3.3 Flight Safety System Summary and Preflight Tests 4.3.4 Trajectory and Debris Dispersion Data 4.3.5 Flight Hazard Areas and Sa
6、fety Clear Zones 4.3.6 Support Systems and Services 4.3.7 Flight Safety Operations 4.3.8 Unguided Suborbital Launch Vehicles (where applicable) 5.0 Ground Safety (415.117) 5.1 Ground Safety Analysis Report 5.2 Ground Safety Plan 6.0 Launch Plans (415.119 and 417.111 of this chapter) 6.1 Launch Suppo
7、rt Equipment and Instru-mentation Plan 6.2 Configuration Management and Control Plan 6.3 Frequency Management Plan 6.4 Flight Termination System Electronic Piece Parts Program Plan 6.5 Accident Investigation Plan 6.6 Local Agreements and Public Coordina-tion Plan 6.7 Hazard Area Surveillance and Cle
8、arance Plan 6.8 Communications Plan 7.0 Launch Schedule (415.121) 7.1 Launch Processing Schedule 8.0 Computing Systems and Software (415.123) 8.1 Hardware and Software Descriptions 8.2 Flow Charts and Diagrams 8.3 Logic Diagrams and Software Design Descriptions 8.4 Operator User Manuals and Document
9、a-tion 8.5 Software Hazard Analyses 8.6 Software Test Plans, Test Procedures, and Test Results 8.7 Software Development Plan 9.0 Unique Safety Policies, Requirements and Practices (415.125) 10.0 Flight Safety System Design and Oper-ation Data (415.127) 10.1 Flight Safety System Description 10.2 Flig
10、ht Safety System Diagram 10.3 Flight Safety System Subsystem De-sign Information 10.4 Flight Safety System Analyses 10.5 Flight Termination System Environ-mental Design 10.6 Flight Safety System Compliance Ma-trix 10.7 Flight Termination System Installa-tion Procedures 10.8 Tracking System Validatio
11、n Proce-dures 11.0 Flight Safety System Test Data (415.129) 11.1 Testing Compliance Matrix 11.2 Test Program Overview and Schedule 11.3 Flight Safety System Test Plans and Procedures 11.4 Test Reports 11.5 Reuse of Flight Termination System Components 12.0 Flight Safety System Crew Data (415.131) 12
12、.1 Position Descriptions 12.2 Certification and Training Program De-scription 13.0 Safety at End of Launch (415.133) Docket No. FAA20007953, 71 FR 50536, Aug. 25, 2006 PART 417LAUNCH SAFETY Subpart AGeneral and License Terms and Conditions Sec. 417.1 General information. 417.3 Definitions and acrony
13、ms. 417.5 Reserved 417.7 Public safety responsibility. 417.9 Launch site responsibility. 417.11 Continuing accuracy of license appli-cation; application for modification of li-cense. VerDate Mar2010 13:23 Feb 23, 2011 Jkt 223046 PO 00000 Frm 00551 Fmt 8010 Sfmt 8010 Y:SGML223046.XXX 223046WReier-Avi
14、les on DSKGBLS3C1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-542 14 CFR Ch. III (1111 Edition) 417.1 417.13 Agreement with Federal launch range. 417.15 Records. 417.17 Launch reporting requirements and launch specific updates. 417.19
15、 Registration of space objects. 417.21 Financial responsibility require-ments. 417.23 Compliance monitoring. 417.25 Post launch report. 417.26417.100 Reserved Subpart BLaunch Safety Responsibilities 417.101 Scope. 417.103 Safety organization. 417.105 Launch personnel qualifications and certification
16、. 417.107 Flight safety. 417.109 Ground safety. 417.111 Launch plans. 417.113 Launch safety rules. 417.115 Tests. 417.117 Reviews. 417.119 Rehearsals. 417.121 Safety critical preflight operations. 417.123 Computing systems and software. 417.125 Launch of an unguided suborbital launch vehicle. 417.12
17、7 Unique safety policies, require-ments, and practices. 417.129 Safety at end of launch. 417.130417.200 Reserved Subpart CFlight Safety Analysis 417.201 Scope and applicability. 417.203 Compliance 417.205 General. 417.207 Trajectory analysis. 417.209 Malfunction turn analysis. 417.211 Debris analysi
18、s. 417.213 Flight safety limits analysis. 417.215 Straight-up time analysis. 417.217 Overflight gate analysis. 417.218 Hold-and-resume gate analysis. 417.219 Data loss flight time and planned safe flight state analyses. 417.221 Time delay analysis. 417.223 Flight hazard area analysis. 417.224 Probab
19、ility of failure analysis. 417.225 Debris risk analysis. 417.227 Toxic release hazard analysis. 417.229 Far-field overpressure blast effects analysis. 417.231 Collision avoidance analysis. 417.233 Analysis for an unguided suborbital launch vehicle flown with a wind weighting safety system. Subpart D
20、Flight Safety System 417.301 General. 417.303 Command control system require-ments. 417.305 Command control system testing. 417.307 Support systems. 417.309 Flight safety system analysis. 417.311 Flight safety system crew roles and qualifications. Subpart EGround Safety 417.401 Scope. 417.402 Compli
21、ance. 417.403 General. 417.405 Ground safety analysis. 417.407 Hazard control implementation. 417.409 System hazard controls. 417.411 Safety clear zones for hazardous op-erations. 417.413 Hazard areas. 417.415 Post-launch and post-flight-attempt hazard controls. 417.417 Propellants and explosives. A
22、PPENDIX A TO PART 417FLIGHT SAFETY ANALYSIS METHODOLOGIES AND PRODUCTS FOR A LAUNCH VEHICLE FLOWN WITH A FLIGHT SAFETY SYSTEM APPENDIX B TO PART 417FLIGHT HAZARD AREA ANALYSIS FOR AIRCRAFT AND SHIP PROTECTION APPENDIX C TO PART 417FLIGHT SAFETY ANALYSIS METHODOLOGIES AND PRODUCTS FOR AN UNGUIDED SUB
23、ORBITAL LAUNCH VEHICLE FLOWN WITH A WIND WEIGHTING SAFETY SYSTEM APPENDIX D TO PART 417FLIGHT TERMI-NATION SYSTEMS, COMPONENTS, INSTALLA-TION, AND MONITORING APPENDIX E TO PART 417FLIGHT TERMI-NATION SYSTEM TESTING AND ANALYSIS APPENDIX F TO PART 417 RESERVED APPENDIX G TO PART 417NATURAL AND TRIG-G
24、ERED LIGHTNING FLIGHT COMMIT CRI-TERIA APPENDIX H TO PART 417 RESERVED APPENDIX I TO PART 417METHODOLOGIES FOR TOXIC RELEASE HAZARD ANALYSIS AND OPERATIONAL PROCEDURES APPENDIX J TO PART 417GROUND SAFETY ANALYSIS REPORT AUTHORITY: 49 U.S.C. 7010170121. SOURCE: Docket No. FAA20007953, 71 FR 50537, Au
25、g. 25, 2006, unless otherwise noted. Subpart AGeneral and License Terms and Conditions 417.1 General information. (a) Scope. This part sets forth (1) The responsibilities of a launch operator conducting a licensed launch of an expendable launch vehicle; and (2) The requirements for maintaining a lau
26、nch license obtained under part 415 of this chapter. Parts 413 and 415 of this chapter contain requirements for preparing a license application to con-duct a launch, including information VerDate Mar2010 13:23 Feb 23, 2011 Jkt 223046 PO 00000 Frm 00552 Fmt 8010 Sfmt 8010 Y:SGML223046.XXX 223046WReie
27、r-Aviles on DSKGBLS3C1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-543 Commercial Space Transportation, FAA, DOT 417.3 reviewed by the FAA to conduct a pol-icy, safety, payload, and environmental review., and a payload determination.
28、(b) Applicability. (1) The administra-tive requirements for filing material with the FAA in subpart A of this part apply to all licensed launches from a Federal launch range or a non-Federal launch site, except where noted. (2) The safety requirements of sub-parts B through E of this part apply to a
29、ll licensed launches of expendable launch vehicles. See paragraphs (d) and (e) of this section for exceptions to this provision. (c) Meets intent certification. For a licensed launch from a Federal launch range, a launch operator need not dem-onstrate to the FAA that an alter-native means of satisfy
30、ing a require-ment of this part provides an equiva-lent level of safety for a launch if writ-ten evidence demonstrates that a Fed-eral launch range has, by the effective date of this part, granted a meets in-tent certification, including through tailoring, that applies to the require-ment and that l
31、aunch. See paragraph (f) of this section for exceptions to this provision. Written evidence includes: (1) Range flight plan approval, (2) Missile system pre-launch safety package, (3) Preliminary and final flight data packages, (4) A tailored version of EWR 1271, (5) Range email to the FAA stating t
32、hat the MIC was approved, or (6) Operation approval. (d) Waiver. For a licensed launch from a Federal launch range, a require-ment of this part does not apply to a launch if written evidence dem-onstrates that a Federal launch range has, by the effective date of this part, granted a waiver that allo
33、ws non-compliance with the requirement for that launch. See paragraph (f) of this section for exceptions to this provision. Written evidence includes: (1) Range flight plan approval, (2) Missile system pre-launch safety package, (3) Preliminary and final flight data packages, (4) A tailored version
34、of EWR 1271, (5) Range email to the FAA stating that the waiver was approved, or (6) Operation approval. (e) Grandfathering. For a licensed launch from a Federal launch range, a requirement of this part does not apply to the launch if the Federal launch ranges grandfathering criteria allow noncompli
35、ance with the requirement for that launch. See paragraph (f) of this section for exceptions to this pro-vision. (f) Exceptions to Federal launch range meets intent certifications, waivers, and grandfathering. Even if a licensed launch from a Federal launch range satisfies paragraph (c), (d), or (e)
36、of this section for a requirement of this part, the requirement applies and a launch operator must satisfy the requirement, obtain FAA approval of any alter-native, or obtain FAA approval for any further noncompliance if (1) The launch operator modifies the launch vehicles operation or safety charac
37、teristics; (2) The launch operator uses the launch vehicle, component, system, or subsystem in a new application; (3) The FAA or the launch operator determines that a previously unfore-seen or newly discovered safety hazard exists that is a source of significant risk to public safety; or (4) The Fed
38、eral launch range pre-viously accepted a component, system, or subsystem, but did not then identify a noncompliance to a Federal launch range requirement. (g) Equivalent level of safety. The re-quirements of this part apply to a launch operator and the launch opera-tors launch unless the launch oper
39、ator clearly and convincingly demonstrates that an alternative approach provides an equivalent level of safety. 417.3 Definitions and acronyms. For the purpose of this part, Command control system means the portion of a flight safety system that includes all components needed to send a flight termin
40、ation control signal to an onboard vehicle flight termination system. A command control system starts with any flight termination acti-vation switch at a flight safety crew console and ends at each command- transmitting antenna. It includes all intermediate equipment, linkages, and software and any
41、auxiliary transmitter stations that ensure a command signal VerDate Mar2010 13:23 Feb 23, 2011 Jkt 223046 PO 00000 Frm 00553 Fmt 8010 Sfmt 8010 Y:SGML223046.XXX 223046WReier-Aviles on DSKGBLS3C1PROD with CFRProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS
42、-,-,-544 14 CFR Ch. III (1111 Edition) 417.3 will reach the onboard vehicle flight termination system from liftoff until the launch vehicle achieves orbit or can no longer reach a populated or other protected area. Command destruct system means a por-tion of a flight termination system that includes
43、 all components on board a launch vehicle that receive a flight termination control signal and achieve destruction of the launch vehicle. A command destruct system includes all receiving antennas, receiver decoders, explosive initiating and transmission devices, safe and arm devices and ord-nance ne
44、cessary to achieving destruc-tion of the launch vehicle upon receipt of a destruct command. Conjunction on launch means the ap-proach of a launch vehicle or any launch vehicle component or payload within 200 kilometers of a manned or mannable orbiting object (1) During the flight of an unguided subo
45、rbital rocket; or (2) For an orbital launch vehicle dur-ing (i) The ascent to initial orbital inser-tion and through at least one complete orbit; and (ii) Each subsequent orbital maneu-ver or burn from initial park orbit, or direct ascent to a higher or interplan-etary orbit. Countdown means the tim
46、ed sequence of events that must take place to ini-tiate flight of a launch vehicle. Crossrange means the distance meas-ured along a line whose direction is ei-ther 90 degrees clockwise (right crossrange) or counter-clockwise (left crossrange) to the projection of a launch vehicles planned nominal ve
47、-locity vector azimuth onto a horizontal plane tangent to the ellipsoidal Earth model at the launch vehicles sub-vehi-cle point. The terms right crossrange and left crossrange may also be used to indicate direction. Data loss flight time means the short-est elapsed thrusting time during which a laun
48、ch vehicle flown with a flight safety system can move from its normal trajectory to a condition where it is possible for the launch vehicle to endanger the public. Destruct means the act of termi-nating the flight of a launch vehicle flown with a flight safety system in a way that destroys the launc
49、h vehicle and disperses or expends all remaining propellant and renders remaining en-ergy sources non-propulsive before the launch vehicle or any launch vehicle component or payload impacts the Earths surface. Downrange means the distance meas-ured along a line whose direction is parallel to the projection of a launch vehicles planned nominal velocity vec-tor azimuth into a horizontal plane tangent to the ellipso
