SSP_50852_Baseline.Doc

SSP 50852

Baseline

H-II Transfer Vehicle (HTV) 1 Verification Matrix

International Space Station Program

Baseline

June 2008

National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas

REVISION AND HISTORY PAGE

PREFACE

H-II Transfer Vehicle 1 (HTV) Verification Matrix This document is developed and maintained by the Vehicle Office. The initial baseline release is under the control of the Vehicle Control Board (VCB). The VCB delegates control and approval authority for futire updates and/or revisions to the VCB.

INTERNATIONAL SPACE STATION PROGRAM

H-II Transfer Vehicle 1 (HTV) Verification Matrix

CONCURRENCE

june 2008

INTERNATIONAL SPACE STATION PROGRAM

Verification Matrix

CONCURRENCE

june 2008

INTERNATIONAL SPACE STATION PROGRAM

Verification Matrix

LIST OF CHANGES

JUNE 2008

All changes to paragraphs, tables, and figures in this document are shown below:

Board Name

Entry Date

Change

Paragraph(s)

June 2008

Baseline

All

TABLE OF CONTENTS

PARAGRAPH

PAGE

1-11.0 INTRODUCTIOn

1.1

PURPOSE

1-1 1.2

SCOPE

1-1 1.3

PRECEDENCE

1-1 1.4

DELEGATION OF AUTHORITY

1-1 1.5 verb application

1-1 1.6 deviation/waiver

1-2 2.0

DOCUMENTS

2-1 2.1 applicable documents

2-1 2.2 reference documents

2-1 3.0

INTERFACING HARDWARE DESCRIPTION

3-1 3.1

ISS DESCRIPTION

3-1 3.1.1

ISS SYSTEM DESCRIPTION

3-1 3.1.2

USOS DESCRIPTION

3-1 3.2

HTV DESCRIPTION

3-2 4.0 HTV Verification

4-1 4.1

VERIFICATION ROLES AND RESPONSIBILITIES

4-1 4.1.1 Primary owner RESPONSIBILITIES

4-1 4.1.2 Secondary owner RESPONSIBILITIES

4-1 4.1.3

T&V RESPONSIBILITIES

4-2

APPENDIX

A Acronyms and abbreviations

A-1 B glossary

B-1 C open work items

C-1

TABLE

1C-1 to be determined items

C- C-2

TO BE RESOLVED ISSUES

C-1 d-1 SSP 50273 Verification Matrix

D-1 e-1 SSP 50438 part 1 verification matrix

E-1

1.0 INTRODUCTIOn

The H-II Transfer Vehicle (HTV) 1 Verification Matrix defines the verification ownership, and correlates the dependencies and requirements for the completion of integration and verification of the Japan Aerospace Exploration Agency (JAXA) HTV 1 segment to the International Space Station (ISS).

1.1 PURPOSE

This is the main document that identifies the organizational roles and responsibilities involved in verification of the requirements for the HTV 1 vehicle.

This document formalizes the requirement ownership and verification commitment within National Aeronautics and Space Administration (NASA) to address the verification tasks required to confirm compliance with the requirements of SSP 50273, Segment Specification for the H-II Transfer Vehicle.

1.2 SCOPE

This document defines the requirement ownership and associated information for the verification of the HTV Segment with the ISS.

1.3 PRECEDENCE

In the event of a conflict, the documents shall apply in the following order of precedence:

A.

SSP 50273, Segment Specification for the H-II Transfer Vehicle B.

SSP 50438, International Space Station to H-II Transfer Vehicle Interface Control Document, Part 1 SSP 50273 and SSP 50438 define the requirements specified in this document and shall take precedence over this document.

1.4 DELEGATION OF AUTHORITY

This document is approved by, and is subject to, the Vehicle Control Board (VCB) using the change control process defined in SSP 50123, Configuration Management Handbook. The Vehicle Office assigns a book manager for maintenance of this document. Changes to the baselined SSP 50852 must be dispositioned and approved by the VCB.

1.5 verb application

The verb “shall” will be used to indicate a requirement. The verb “will” may be used to express a declaration of purpose or in cases where simple future tenses are required but not to articulate a requirement binding on the ISS participants.

1.6 deviation/waiver

All requests for deviation or waiver of this document must be submitted to the NASA Vehicle Office Manager or their delegated authorities who control SSP 50852 for approval signature.

2.0 DOCUMENTS

2.1 applicable documents

The following documents include specifications, models, standards, guidelines, handbooks, and other special publications. The documents listed in this paragraph are applicable to the extent specified herein. Inclusion of applicable documents herein does not in any way supersede the order of precedence identified in Paragraph 1.3 of this document.

2.2 reference documents

The following documents contain supplemental information to guide the user in the application of this document. These reference documents may or may not be specifically cited within the text of this document.

3.0 INTERFACING HARDWARE DESCRIPTION

3.1 ISS DESCRIPTION

3.1.1 ISS SYSTEM DESCRIPTION

The ISS is an international endeavor being developed by NASA, JAXA, the European Space Agency (ESA), the Agenzia Spaziale Italia (ASI), the Canadian Space Agency (CSA), and the Federal Space Agency (Roscosmos). The ISS consists of pressurized modules and unpressurized systems and elements that form a human base in low earth orbit. The ISS provides science capabilities for microgravity, materials, life science research and development, earth and stellar observation as well as other technology development and demonstration by the United States (U.S.) and the International Partners.

The ISS is comprised of the United States On-Orbit Segment, (USOS), International Ground System (IGS), ESA Columbus module, JAXA Japanese Experiment Module (JEM), Roscosmos Russian Segment (RS), ASI Multi-Purpose Logistics Modules (MPLM), and the CSA Mobile Servicing System (MSS). The NASA Space Shuttle, the RS Progress vehicle, JAXA H-II Transfer Vehicle (HTV), Commercial Orbital Transport Systems (COTS), and ESA Automated Transfer Vehicle (ATV) are cargo transportation systems for the ISS.

The ISS development is accomplished in stages using a pre-defined sequence of assembly flights. Every physical station configuration in each stage shall be verified. The assembly sequence flight numbers will be used to reference the verification reporting. Changes within an assembly stage will be considered in the verification of that stage.

3.1.2 USOS DESCRIPTION

The USOS is an earth orbiting facility which houses experiment payloads, distributes resource utilities, and supports permanent human habitation for conducting research and science experiments in a micro gravity environment. The USOS supplies the following services and capabilities to the ISS: electric power generation, storage, distribution and control; primary communications and data links to ground support facilities; environmental control and life support; thermal control and heat rejection; navigation & control; data processing; storage and transportation; crew health care; housekeeping; personal hygiene; food preparation and storage; extravehicular activity access; payload utilities; attitude control; pointing support and robotics system control.

The U.S. pressurized modules contain equipment to provide laboratory, habitation, logistics re-supply, and overall Station command and control functions. The U.S. pressurized elements include the U.S. Laboratory Module (U.S. Lab), the Node 1, the Node 2, the Node 3, the Airlock, Pressurized Mating Adapters, and the Cupola. The Nodes are pressurized, environmentally controlled elements that serve to connect the U.S. Lab, and the International Partners' modules. With four radial ports and two axial ports each, the Nodes are the building blocks for the pressurized elements for the ISS. Node 2 serves primarily as the berthing location for the Pressurized Mating Adapter (PMA)-2, the forward end of the U.S. Lab, the Columbus module, the JEM, and the Mini-Pressurized Logistics Module and HTV when it arrives at the International Space Station on its re-supply missions

The U.S. unpressurized elements include the Integrated Truss Assembly (ITA), the Unpressurized Cargo Carriers (UCC), the Photovoltaic (PV) power modules, the Control Moment Gyro (CMG), and the external central Thermal Control Subsystem (TCS), Mobile Transporter (MT), and storage and logistics carriers and platforms.

3.2 HTV DESCRIPTION

The HTV is an automated, unmanned cargo transportation system developed by the JAXA for the ISS. This system is composed of the H-II Transfer Vehicle, the HTV Operations System, the HTV Proximity Communication System [HTV Proximity (PROX) or PROX], and the HTV Laser Radar Reflector [HTV Laser Radar Reflector (LRR) or LRR]. The HTV transports pressurized and unpressurized cargos (experiment equipment and materials, system equipment, crew items, consumable, etc.) to the ISS. It can also reload nonrecoverable items from the ISS for disposal and perform destructive reentry.

The HTV is composed of the pressurized section of the Pressurized Logistics Carrier (PLC), the Unpressurized Logistics Carrier (ULC), the Exposed Pallet (EP), the Avionics Module and the Propulsion Module. The pressurized section carries the pressurized cargos. The unpressurized section holds unpressurized cargos. The unpressurized cargos are attached to the Exposed Pallet and the entire pallet is transferred to and from the HTV to ISS via the Space Station Remote Manipulator System (SSRMS) and JEM Remote Manipulator System (RMS). The Avionics Module has the functions for navigation and guidance of the HTV and generates control commands to the Propulsion Module. It also has the functions for communication, data processing, and power supply to the components. The Propulsion Module receives commands from the Avionics Module and controls the trajectory and the attitude of the HTV. The HTV System is defined in SSP 50273.

4.0 HTV Verification

The HTV 1 verification matrices for SSP 50273 and SSP 50438, Part 1 defines requirement ownership as well as the Estimated Completion Date (ECD). The matrices will contain (but not limited to) the requirement, title, paragraph number, primary and secondary owners, JAXA contacts (for reference only), dependencies and comments along with verification status. The baseline versions of the matrices are contained in Appendix D and E respectively. The matrices will be updated and maintained on the NASA/OB3 Vehicle Integration Office / HTV International Partner Verification website at: http://iss-www.jsc.nasa.gov/nwo/vh1/tvcp_itv/web/JAXAHTV.shtml

4.1 VERIFICATION ROLES AND RESPONSIBILITIES

Each organization assigned to support verification of a requirement will maintain a Comment List in accordance with JHX2007119, H-II Transfer Vehicle (HTV-1) Post Qualification Review (PQR) Execution Plan, for each requirement. A copy of the Comment List will be provided to Test & Verification (T&V) on completion of the verification activities for the specific PQR Board.

4.1.1 Primary owner RESPONSIBILITIES

The owners are responsible for ensuring the verification evidence provided to them is complete and sufficient for requirement closure, and ready for T&V signature.

NOTE: The owners of the SSP 50438 ISS side requirements are exceptions to this statement and must provide verification evidence for closure.

The primary owner will be the focal contact point for coordination with JAXA owners. While independent verification is acceptable, coordination with secondary owners and other engineering disciplines, as required, is highly encouraged. The primary owner will be responsible for signing the Verification Compliance Notice (VCN) when they are satisfied that the requirement has been successfully verified.

4.1.2 Secondary owner RESPONSIBILITIES

Secondary owners are responsible for their portion of the requirement only. They are encouraged to coordinate with the primary owner for verification closure. They should coordinate their JAXA communication with the primary owner, but may conduct their own coordination as required.

Secondary owners will provide T&V a written confirmation of verification closure along with their Comment List when satisfied their portion of the requirement has been successfully verified.

4.1.3 T&V RESPONSIBILITIES

T&V will provide each requirement owner notification of receipt of the verification document and the location of the documents. T&V will review the documents to ensure accuracy and completeness in conjunction with the initial notification. Any discrepancies will be noted by T&V and relayed to the NASA requirement owner as well as the JAXA owner

T&V will monitor the requirement closure and provide assistance in obtaining additional information required and/or corrections to documentation provided as verification evidence. On receipt of final verification from the primary and all secondary owners, T&V will sign the VCN and forward the information to the Launch Package Manager for closure.

Appendix A - Acronyms and abbreviations

Appendix B - glossary Cargo

The cargo is composed of the Net Cargo and configurable equipment containers. Net Cargo comprises the actual cargo delivered to the Space Station by the HTV, excluding tankage, secondary structure, piping, etc. which are included in the cargo carrier budget

Component

The component constitutes an integral part of a subsystem or system, combines various parts, devices and/or structures, and performs an independent function in operation of the subsystem or the system. Primary examples of components are actuators, valves, batteries, transmitters, receivers, multiplexers and other discrete electronic devices.

Development Model

The development model is made for the development tests that are performed to finalize the prototype model design and testing methods (e.g., collection and verification of information related to design, analysis, manufacture and testing). The development model includes engineering models, thermal models, structural models, attitude control models, and antenna radiation pattern models.

Engineering Model

The engineering model is a test article used to establish electrical and functional designs of a HTV. As it basically has the same configuration as the launch HTV, it is used as a “mockup” to develop the layout of components, assembly procedures and handling methods, as well as for electromagnetic compatibility test.

Flight Model

The flight model includes components, subsystems and systems that will be actually launched and operated in orbit. The flight model is subjected to the acceptance tests, upon completion of which systems are accepted for launching while components and subsystems can be incorporated into the flight model.

Integration

The act of mating hardware and/or software components, subsystems, systems or elements at their respective interfaces and verifying the compatibility and proper operation of the resulting entity. Integration, as used in this sense, is an integral part of the verification process.

Logistics

The art and science of management, engineering, and technical activities concerned with determining requirements, system design, and supplying and maintaining resources to support objectives, plans and operations.

Logistics Carrier The Logistics Carrier is defined as the fixed structure required accommodating the cargo.

Operational Modes

The operational modes for a component, assembly, subsystem, or system include all combinations of operational configurations or conditions that can occur in orbit, including power condition, redundancy management mode, operation mode of a component and subsystem.

Protoflight Model

The protoflight model is the model originally specified as the prototype model, which was, in whole or part, subjected to qualification tests and was re-specified as the flight model after evaluation and refurbishment as necessary. Otherwise It refers to the model previously specified for both prototype and flight purposes and required to be subjected to environmental tests that consist of various requirements of acceptance and qualification tests.

Proximity Operation

The operation of one spacecraft in the vicinity of another spacecraft with the relative positions stabilized and the attitude rate small enough to preclude the requirements for re-rendezvous.

Software

Computer programs and computer databases: As used in a Computer Based Control System (CBCS) context, “software” refers to all flight software regardless of the media on which the software resides, including software that resides on hardware devices (i.e., firmware).

Structure Development Model

The structure development model is a test article used to finalize structural design of the HTV. While it is structurally identical to the launch HTV, it is equipped with dummy parts and components that have the same weight, center of gravity and inertial efficiency. The structure development model is used for mechanical environmental tests such as vibration, shock and acoustic tests.

Subassembly

The subassembly consists of two or more parts that can be disassembled or replaced as a unit.

Subsystem

The subsystem is an assembly of two or more components using a support structure and interconnected cabling or piping required to fix the components in position. The subsystem consists of functionally related components required to achieve a specific function. Primary examples of the subsystems used in HTV are electrical, attitude control, telemetry command, structural and thermal control, and propulsion subsystems.

Validation

A set of activities performed to ensure that each product reflects an accurate interpretation and execution of requirements and meets a level of functionality and performance that is acceptable to users.

Verification

A set of activities performed to ensure that facilities, hardware and software products, and operational and acceptance procedures comply with the requirements imposed upon them.

Appendix C - open work

Table C-1 lists the specific To Be Determined (TBD) items in the document that are not yet known. The TBD is inserted as a placeholder wherever the required data is needed and is formatted in bold type within brackets. The TBD item is numbered based on the section where the first occurrence of the item is located as the first digit and a consecutive number as the second digit (i.e., <TBD 4-1> is the first undetermined item assigned in Section 4 of the document). As each TBD is solved, the updated text is inserted in each place that the TBD appears in the document and the item is removed from this table. As new TBD items are assigned, they will be added to this list in accordance with the above described numbering scheme. Original TBDs will not be renumbered.

Table C-1 to be determined items

Table C-2 lists the specific To Be Resolved (TBR) issues in the document that are not yet known. The TBR is inserted as a placeholder wherever the required data is needed and is formatted in bold type within brackets. The TBR issue is numbered based on the section where the first occurrence of the issue is located as the first digit and a consecutive number as the second digit (i.e., <TBR 4-1> is the first unresolved issue assigned in Section 4 of the document). As each TBR is resolved, the updated text is inserted in each place that the TBR appears in the document and the issue is removed from this table. As new TBR issues are assigned, they will be added to this list in accordance with the above described numbering scheme. Original TBRs will not be renumbered.

table C-2 TO BE RESOLVED ISSUES

APPENDIX D – SSP 50273 VERIFICATION MATRIX

table d-1 SSP 50273 Verification Matrix (Page 1 of 38)

table d-1 SSP 50273 Verification Matrix (Page 2 of 38)

HTV-001

OPS

HTV-002

HTV-003

HTV-004

OPS

HTV-005

HTV-006

HTV-007

HTV-008

HTV-009

HTV-010

HTV-011

HTV-012

HTV-013

table d-1 SSP 50273 Verification Matrix (Page 3 of 38)

HTV-017

HTV-018

HTV-019

OPS

HTV-020

OPS

HTV-021

HTV-022

HTV-023

HTV-024

OPS

HTV-025

HTV-026

HTV-027

S&MA

OPS

HTV-028

HTV-029

GROUND SEGMENT

S&MA

C&DH

CBCS

HTV-030

EVR

IVPAT

table d-1 SSP 50273 Verification Matrix (Page 4 of 38)

HTV-034

HTV-035

HTV-036

HTV-037

HTV-038

HTV-039

3.3.2.1

HTV-040

C&DH

RPOC

PROX-001

HTV-041

PROX-002a

HTV-042

PROX-004A

HTV-043

OPS

HTV-044

OPS

HTV-045

HTV-046

SMC

PROX-005C

HTV-047

C&T

OPS

PROX-006

HTV-048

table d-1 SSP 50273 Verification Matrix (Page 5 of 38)

PROX-007B

HTV-049

PROX-008A

HTV-050

PROX-009B

HTV-051

OPS

PROX-010A

HTV-052

HTV-053

PROX-011

HTV-054

PROX-12A

HTV-055

PROX-013a

HTV-056

PROX-14B

HTV-057

HTV058

RPOC

SMC

OPS

HTV-059

SMC

HTV-060

HTV-061

SMC

HTV-062

SMC

HTV-063

table d-1 SSP 50273 Verification Matrix (Page 6 of 38)

SMC

OPS

HTV-064

C&T

GROUND SEGMENT

OPS

HTV-065

C&T

PROX-15B

C&T

HTV-066

PROX-016

HTV067

PROX-017

HTV-068

Ground Segment

HTV-069

HTV-070

PROX-018

HTV-071

PROX-019

HTV-072

HTV-073

HTV-074

HTV-075

HTV-076

lrr-001

HTV-077

table d-1 SSP 50273 Verification Matrix (Page 7 of 38)

CDH SW

OPS

HTV-078

CDH SW

OPS

HTV-079

CDH SW

OPS

HTV-080

HTV-081

HTV-082

CDH SW

HTV-083

HTV-084

HTV-085

HTV-087

HTV-088

HTV-089

3.2.2.3.3 (incl. all sub- paragraphs)

3.2.2.3.4 (incl. all sub- paragraphs)

HTV-090

HTV-091

table d-1 SSP 50273 Verification Matrix (Page 8 of 38)

HTV-092

HTV-093

HTV-094

HRR-001

HTV-095

HRR-002

HTV-096

HRR-003

HTV-097

HTV-098

HTV-099

HTV-100

HTV-101

HTV-103

HTV-104

SMC

PROX-220

HTV-105

SMC

PROX-221

HTV-106

CBCS

PROX-222

HTV-107

table d-1 SSP 50273 Verification Matrix (Page 9 of 38)

CBCS

PROX-223

HTV-108

HTV-109

HTV-111

HTV-112

HTV-113

PROX-020

HTV-114

HTV-115

PROX-021

HTV-116

HTV-117

HTV-118

HTV-119

table d-1 SSP 50273 Verification Matrix (Page 10 of 38)

PROX-022

PROX-023

PROX-024A

PROX-026B

LRR-002

LRR-003

LRR-004

LRR-005

LRR-006

PROX-027

PROX-028

PROX-029A

PROX-030B

PROX-031

PROX-032A

HTV-120

PROX-033

PROX-034

table d-1 SSP 50273 Verification Matrix (Page 11 of 38)

PROX-035

PROX-036

PROX-037B

HTV-121

PROX-038

PROX-039

PROX-040A

PROX-041

PROX-042B

HTV-122

PROX-043B

HTV-123

PROX-44B

PROX-045A

GROUND SEGMENT

PROX-046B

PROX-047B

IVPAT

PROP

EP-001

HTV-124

table d-1 SSP 50273 Verification Matrix (Page 12 of 38)

HTV-127

HTV-128

HTV-129

HTV-130

HTV-131

HTV-132

EP-002

HTV-133

HTV-134

HTV-135

HTV-136

EP-003

EP-004

EP-005

EP-006

EP-007

table d-1 SSP 50273 Verification Matrix (Page 13 of 38)

EP-008

EP-009

EP-010

EP-011

EP-012

EP-13

EP-014

EP-015

table d-1 SSP 50273 Verification Matrix (Page 14 of 38)

HTV-168

HTV-169

HTV-170

3.1.1.4

HTV-171

HTV-172

HTV-173

EP-016

HTV-174

table d-1 SSP 50273 Verification Matrix (Page 15 of 38)

HTV175

HTV-176

HTV-177

HTV-178

HTV179

HTV-180

HTV-181

HTV-182

3.2.2.5 (incl. all sub- paragraphs)

3.4.1.1.1 (incl. all sub- paragraphs)

3.2.2.2.5.5.1

HTV-183

EP-017

3.2.2.1.4

3.2.2.1.5

HTV-186

PROX-048

HTV-187

PROX-049

HRR-004

HTV-188

S&MA

RPOC

EPS

PROP

SMC

PROX-050

HRR-005

HTV-189

table d-1 SSP 50273 Verification Matrix (Page 16 of 38)

S&MA

RPOC

EPS

PROP

PROX-051

HRR-006

HTV-190

HTV-191

PROX-052

HRR-007

HTV-192

CBCS

PROX-053

HRR-008

HTV-193

PROX-054

LRR-008

PROX-055A

LRR-009

PROX-056

LRR-010

PROX-058

LRR-011

PROX-059

LRR-012

PROX-060

PROX-061

PROX-062

table d-1 SSP 50273 Verification Matrix (Page 17 of 38)

LRR-013

EP-018

HTV-194

LRR-014

EP-019

HTV-195

HTV-196

PROX-063

LRR-015

EP-021

HTV-197

PROX-064

LRR-016

EP-022

HTV-198

PROX-065

LRR-017

EP-023

HTV-199

PROX-066

LRR-018

EP-024

HTV-200

PROX-067B

LRR-019

EP-025

HTV-201

table d-1 SSP 50273 Verification Matrix (Page 18 of 38)

PROX-068A

LRR-020

EP-026

HTV-202

PROX-069A

LRR-021

EP-027

HTV-203

PROX-070A

LRR-022

EP-028

HTV-204

LRR-023

EP-029

HTV-205

HTV-206

HTV-207

HTV-208

GNC

LRR-024

HTV-209

GNC

LRR-025

HTV-210

HTV-211

HTV-212

HTV-213

HTV-214

HTV-215

table d-1 SSP 50273 Verification Matrix (Page 19 of 38)

PROX-071

LRR-026

HRR-009

EP-030

HTV-216

PROX-072

HTV-217

PROX-073

EP-031

HTV-218

PROX-074

EP-032

HTV-219

PROX-075

EP-033

HTV-220

HTV-221

PROX-076

EP-034

HTV-222

PROX-077

EP-035

HTV-223

PROX-078

EP-036

HTV-224

PROX-079

EP-037

HTV-225

table d-1 SSP 50273 Verification Matrix (Page 20 of 38)

Cargo Integration

PROX-080

LRR-027

HRR-010

HTV-227

Cargo Integration

PROX-081

LRR-028

HRR-011

HTV-228

Cargo Integration

PROX-083

LRR-029

HRR-012

HTV-229

Cargo Integration

PROX-084

LRR-030

HRR-013

HTV-230

PROX-085

HRR-014

HTV-231

HTV-232

PROX-086

LRR-031

EP-038

HTV-233

Cargo Integration

PROX-087

LRR-032

HRR-015

HTV-234

Cargo Integration

PROX-088

LRR-033

HRR-016

HTV-235

table d-1 SSP 50273 Verification Matrix (Page 21 of 38)

Cargo Integration

PROX-089

LRR-034

HRR-017

HTV-236

Cargo Integration

PROX-090

LRR-035

HRR-018

HTV-237

PROX-091

HTV-238

Cargo Integration

PROX-092

HTV-239

PROX-093

LRR-036

HRR-019

EP-039

HTV-240

PROX-094

HTV-241

HTV-242

Cargo Integration

PROX-095

LRR-037

HRR-020

EP-040

HTV-243

Cargo Integration

PROX-096

LRR-038

HRR-021

EP-021

HTV-244

PROX-097A

LRR-039

HRR-022

HTV-245

table d-1 SSP 50273 Verification Matrix (Page 22 of 38)

PROX-098

HRR-023

HTV-246

PROX-099

HRR-024

HTV-247

PROX-100

HRR-025

HTV-248

PROX-101

HRR-026

HTV-2…