Attachment E-3 GXSUIID.pdf

Effective Date: August 13, 2021 418-XO-GXSUIID-0030 Expiration Date: Five years from date of last signature Baseline Version 1.2 Responsible Organization: GeoXO Flight Project/Code 418

Geostationary Extended Observations (GeoXO) Sounder (GXS)

Unique Instrument Interface Document (UIID) Signature page

Prepared by:

Electronically approved by: 04/23/2021

Nicolaas du Toit Date GeoXO Flight Project, Instrument Systems Engineer NASA GSFC, Code 418

Reviewed by:

Electronically approved by: 04/12/2021

Alexander Krimchansky Date GeoXO Flight Project, Mission Systems Engineer NASA GSFC, Code 599

Approved by:

Electronically approved by: 04/20/2021

Jason H. Hair Date GeoXO Flight Project, Project Manager NASA GSFC, Code 418

/GeoXO Flight Project GXS Sounder

GXSUIID

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

Version: 1.2 Printed by: rkhoover Printed on: Wednesday, December 22, 2021

No filter applied.

No sort applied.

Generated from DOORS 9.7.2.4

Contents

1 1Scope (CCR X00044A)

1.1 1Document Overview (CCR X00044A)

1.2 1Requirements Terminology (CCR X00044A)

1.3 2Order of Precedence (CCR X00044A)

2 3Documents (CCR X00044A)

2.1 3Applicable Documents (CCR X00044A)

2.2 3Reference Documents (CCR X00044A)

3 4Allocations

3.1 4Command and Data Handling

3.1.1 4Instrument-to-Spacecraft Science Rate

3.1.2 4Telemetry Data Rate

3.1.3 4Application Process Identifiers

3.1.4 4GeoXO Reliable Data Delivery Protocol Packet Rate (CCR X00044A)

3.2 4Power

3.2.1 4Average Operational Power

3.2.2 4Maximum Operational Power

3.2.3 4Average Survival Power

3.2.4 4Maximum Survival Power

3.3 5Mechanical

3.3.1 5Mass Properties

3.3.2 5Cabling Between Units

3.3.3 5Volume

3.3.4 5Optical Port Field-of-View

3.3.5 5Radiator Field-of-View

3.3.6 6Field-of-View in the +X direction (CCR X00044A)

3.3.7 6Mounting

3.4 6Mechanical Disturbances (CCR X00044A)

3.4.1 6Integrated Angular Momentum

3.4.2 6Angular Momentum Limits

3.4.3 7Instrument Translation Acceleration Limits

3.4.4 9Predicted Interface Force and Torque (PIFT) Responses

3.4.5 10Spacecraft Mounting Stiffness

3.4.6 10External Sourced Translation Acceleration Limits

Project: GeoXO Flight Project GXS Sounder Module: GXSUIID Baseline Version: 1.2

Contents ii

3.4.7 12Instrument Torque Limit (CCR X00044A)

3.5 12Thermal

3.6 12Instrument Purge Requirements

4 13Constraints

5 14GIRD Deviations

6 15Design Verification Requirements

6.1 15Radiated Emissions, Electric Field (RE 102)

6.2 15Reserved (CCR X00044A)

7 16Acronyms

Contents iii

Page 1 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID118

GXSUIID119

GXSUIID120

GXSUIID121

GXSUIID122

GXSUIID123

GXSUIID124

GXSUIID125

GXSUIID126

GXSUIID127

Object Number

1.0-1

1.0-2

1.0-3

1.0-4

1.0-5

1.0-6

1.1

1.1.0-1

1.2

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

1 Scope (CCR X00044A) The purpose of this Unique Instrument Interface Document (UIID) is two-fold. The first is to allocate GeoXO series spacecraft resources to the Hyperspectral Sounder Instrument (GXS). The second is to serve as a core building block on which the GXS-spacecraft interface can be designed. The spacecraft integrating contractor and the GXS contractor will meet each of their respective interface requirements as defined in this document. (CCR X00044A)

This UIID will govern the development of an Interface Control Document (ICD) which will be a joint activity of the GXS and spacecraft contractors. (CCR X00044A)

The GXS ICD establishes the details of the electrical, communications, mechanical, thermal, integration and test, and command and data handling (C&DH) interfaces between the GXS instrument and the GeoXO spacecraft. After the ICD is signed and approved by all parties, the spacecraft contractor will maintain the ICD. (CCR X00044A)

The GXS is a hyperspectral infrared passive radiometric sounder used to collect environmental data as part of a 3-axis stabilized geostationary (GEO) weather satellite system of the GEO-eXtended Observations (GeoXO) program. The GXS will collect radiance observations of the earth’s atmosphere with both spectral and horizontal resolution that will yield vertical temperature and moisture information. Winds can also be derived from rapid mesoscale observations. GXS will provide hyperspectral geostationary operational observations for soundings of the western hemisphere for the first time. GXS data will enhance convective storm nowcasting as well as improve numerical weather production (NWP) in short range weather forecasting and longer range weather prediction. (CCR X00044A)

Data availability, radiometric quality, simultaneous data collection, coverage rates, scan flexibility, and minimizing data loss due to the sun are prime requirements of the system. The instrument requires primary power, and command input data from the spacecraft. Instrument output data to the spacecraft contains instrument information, instrument telemetry and ancillary data. (CCR X00044A)

The sensor units contain the optical system, scanner, detectors and their cooling/heating systems and directly related electronics. The electronics unit contains the power supply module, command, control, and data processing circuitry. If required, an auxiliary electronics unit may be used for active detector temperature regulation.

(CCR X00044A)

1.1 Document Overview (CCR X00044A)

Together, the General Interface Requirements Document (GIRD) and the GXS UIID establish the GXS-spacecraft interface requirements. The GIRD applies to all GeoXO instruments while the GXS UIID is specific to the GXS. Section 1 explains the use of this document. Section 2 lists reference documents. Section 3 allocates spacecraft resources, such as mass, power, and data rate, to the GXS instrument. Section 4 contains government-accepted operation constraints. Section 5 contains government-accepted deviations from the GIRD. Section 6 contains Design Verification Requirements. Section 7 contains a list of acronyms used within this document. (CCR X00044A)

1.2 Requirements Terminology (CCR X00044A)

Page 2 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID128

GXSUIID129

GXSUIID130

GXSUIID131

GXSUIID132

GXSUIID133

GXSUIID134

GXSUIID135

GXSUIID136

GXSUIID137

GXSUIID138

GXSUIID139

GXSUIID140

GXSUIID141

Object Number

1.2.0-1

1.2.0-2

1.2.0-3

1.2.0-4

1.2.0-5

1.2.0-6

1.2.0-7

1.2.0-8

1.2.0-9

1.2.0-10

1.2.0-11

1.2.0-12

1.3

1.3.0-1

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

The following requirements terminology is used throughout this document: (CCR X00044A)

The term “shall” designates a requirement that must be achieved and is synonymous with the term “threshold.” (CCR X00044A)

The term “should” designates a desired level of performance the government would like the contractor to strive towards achieving and is synonymous with the term “goal.”

(CCR X00044A)

All other terms, including “will”, only designate statements of fact or intentions of the government and are not to be interpreted as contractor requirements. (CCR X00044A)

The term “TBD” means, “to be determined.” This is applied to requirements or values that have not been defined. The contractor is responsible for proposing a requirement or value and its corresponding rationale for all TBD requirements. (CCR X00044A)

TBD requirement proposals are to be made in coordination with the government and may involve other contractors. (CCR X00044A)

The contractor should request approval from the government before proceeding with its proposed TBD requirement or value. (CCR X00044A)

The term “TBR” means, “to be reviewed.” This is applied to requirements or values that are subject to review by the government and the contractor. The contractor should review and suggest a modified value and rationale for all TBR requirements. The “TBR” provides an indication that the value may change upon review. (CCR X00044A)

TBR requirement proposals will be made in coordination with the government and may involve other contractors. (CCR X00044A)

The contractor should request approval from the government before proceeding with its proposed TBR requirement or value. (CCR X00044A)

The term “TBS” means, “to be supplied.” The government will supply TBS requirements. The government will provide a date or milestone at which each TBS requirement will be supplied. (CCR X00044A)

The orbit reference frame (ORF), and the body reference frame (BRF), and defined in the GIRD. (CCR X00044A)

1.3 Order of Precedence (CCR X00044A)

The order of precedence of interface requirements documents is the UIID at the highest level, followed in order by the GIRD, ICD, and Instrument Description Document (IDD). (CCR X00044A)

Page 3 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID142

GXSUIID143

GXSUIID145

GXSUIID144

GXSUIID146

Object Number

2.1

2.1.0-1

2.2

2.2.0-1

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

2 Documents (CCR X00044A)

2.1 Applicable Documents (CCR X00044A)

The following documents of the exact issue shown form a part of this UIID to the extent specified herein. In the event of conflict between the documents referenced and the contents of this UIID the latter will be the superseding requirement.

1. MIL-STD-461G – Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment, 11 December 2015

2. 418-XO-GXIGIRD-0025 - General Interface Requirements Document (GIRD)

(CCR X00044A)

2.2 Reference Documents (CCR X00044A)

The following documents provide reference material for part of this document.

1. CCSDS 133.0-B-2 - Space Packet Protocol, Blue Book, Issue 2, June 2020

2. CCSDS 301.0-B-4 - Time Code Formats. Blue Book. Issue 4, November 2010

3. 418-XO-RPT-0039 GOES Reliable Data Delivery Protocol (GRDDP)

(CCR X00044A)

Page 4 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID26

GXSUIID27

GXSUIID28

GXSUIID29

GXSUIID30

GXSUIID31

GXSUIID32

GXSUIID33

GXSUIID34

GXSUIID35

GXSUIID36

GXSUIID37

GXSUIID38

GXSUIID39

GXSUIID40

GXSUIID41

GXSUIID42

GXSUIID43

GXSUIID44

Object Number

3.0-1

3.1

3.1.1

3.1.1.0-1

3.1.2

3.1.2.0-1

3.1.3

3.1.3.0-1

3.1.4

3.1.4.0-1

3.2

3.2.1

3.2.1.0-1

3.2.2

3.2.2.0-1

3.2.3

3.2.3.0-1

3.2.4

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

3 Allocations The GeoXO spacecraft provides communications, power and a platform for the Sounder instrument. The following paragraphs allocate these resources to Sounder. (CCR X00044A)

3.1 Command and Data Handling

3.1.1 Instrument-to-Spacecraft Science Rate

The instrument science and engineering data rate, including all overhead associated with Consultative Committee for Space Data Systems (CCSDS) packetization by the instrument, at the spacecraft interface shall not exceed 150 million bits per second when averaged over any 5 second period. (CCR X00044A)

3.1.2 Telemetry Data Rate

Housekeeping telemetry data rate, including all overhead associated with CCSDS packetization by the instrument, at the spacecraft interface shall not exceed 1024 bits per second when averaged over any 5 second period.

3.1.3 Application Process Identifiers

The Sounder shall use no more than 255 consecutive Application Process Identifiers (APIDs) for science, telemetry, and command packets.

3.1.4 GeoXO Reliable Data Delivery Protocol Packet Rate (CCR

X00044A)

The Sounder shall transmit to the spacecraft no more than 400 GOES Reliable Data Delivery Protocol (GRDDP) Packets per second. (CCR X00044A)

3.2 Power

3.2.1 Average Operational Power

The Sounder shall draw operational average power, inclusive of heaters, of no more than 615 Watts from up to six total feeds including primary and redundant feeds.

Operational average power is the total power into an instrument averaged over any 5 minute period. (CCR X00044A)

3.2.2 Maximum Operational Power

The Sounder shall draw operational maximum power of no more than 984 Watts.

Operational maximum power is the total power into an instrument averaged over any 20ms period. (CCR-X00018)

3.2.3 Average Survival Power

The Sounder shall draw average survival power of no more than 400 Watts. Average survival power is the total power into an instrument averaged over any 72 minute period. (CCR-X00018)

3.2.4 Maximum Survival Power

Page 6 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID114

GXSUIID117

GXSUIID147

GXSUIID148

GXSUIID59

GXSUIID60

GXSUIID61

GXSUIID62

GXSUIID63

GXSUIID64

GXSUIID65

GXSUIID66

GXSUIID67

GXSUIID68

Object Number

3.3.5.0-2

3.3.6

3.3.6.0-1

3.3.6.0-2

3.3.7

3.3.7.0-1

3.3.7.0-2

3.3.7.0-3

3.4

3.4.0-1

3.4.1

3.4.1.0-1

3.4.2

3.4.2.0-1

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

The spacecraft shall provide the sensor unit’s radiator face a 2π steradian field-of-view to space excepting a field-of-view blockage with less than 3 W back loading. (CCR-

X00018) (CCR X00044A)

3.3.6 Field-of-View in the +X direction (CCR X00044A)

The spacecraft shall provide on the sensor unit's +X face a clear calibration FOV of 7.5 degrees centered on the X-axis, in the X-Z plane, and 52.0 degrees centered on the X-axis, in the X-Y plane. (CCR X00044A)

The spacecraft shall provide on the sensor unit's +X face a calibration glint free FOV of 66 degrees centered on the X-axis, in the X-Z plane, and 80 degrees centered on the X-axis, in the X-Y planes. Glint is defined as stray light from structures such as solar panels, antennas, or other sensors. (CCR X00044A)

3.3.7 Mounting

The spacecraft shall provide the instrument sensor unit a nadir-facing mounting surface.

The sensor unit mechanical interface shall lie within the anti-nadir plane of the sensor unit envelope.

The instrument sensor unit shall use kinematic mounts for its mechanical interface to the spacecraft.

3.4 Mechanical Disturbances (CCR X00044A)

These requirements apply while the instrument is in orbit and operating.

3.4.1 Integrated Angular Momentum

The absolute value of the high pass filtered angular momentum integrated with respect to time shall not exceed the values listed in Filtered Integrated Angular Momentum Limits table. The filter is a second order Butterworth filter with a -3 dB cutoff frequency at 0.01 Hz.

Filtered Integrated Angular Momentum Limits

Limit

Axis (N‐m‐s2)

Roll 0.50

Pitch 0.30

Yaw 0.50

(CCR-X00018) (CCR X00044A)

3.4.2 Angular Momentum Limits

The absolute value of the high pass filtered angular momentum produced by the sensor unit referenced at the satellite center of mass shall not exceed the values listed in the Angular Momentum Limits table. The high pass filter is a second order Butterworth filter with a -3 dB cutoff frequency at 0.01 Hz. The satellite center of mass will be within 2 meters of the centroid of the sensor unit mounts.

Page 7 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID68

GXSUIID69

GXSUIID70

GXSUIID71

Object Number

3.4.2.0-1

3.4.2.0-2

3.4.3

3.4.3.0-1

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

Angular Momentum Limits

Limit

Axis (N‐m‐s)

Roll 0.10

Pitch 0.05

Yaw 0.10

(CCR-X00018)

The absolute value of the band pass filtered instrument angular momentum in each orthogonal axis shall not exceed the values listed in the One-Sixth Octave Band Filtered Angular Momentum Limits table. The bandpass filters for this requirement are defined as a series of eighth-order Butterworth bandpass filters with -3 dB bandwidth of one sixth of an octave. The first filter in the series has its center frequency at 0.015625 Hz, and the center frequencies for the series are spaced at one-twelfth octave up to 10 Hz. The Bandpass‐Filtered Angular Momentum Limits apply to filters with center frequency greater than f1 and less than or equal to f2.

One-Sixth Octave Band Filtered Instrument Angular Momentum Limits f1 (Hz) f2 (Hz)

Limit (N-m-s)

0.01 0.25 0.050

0.25 1.0 0.020

1.0 10.0 0.015

(CCR X00044A)

3.4.3 Instrument Translation Acceleration Limits

The translational accelerations induced by the instrument sensor at each mount shall not exceed the limits specified in the Instrument-to-Spacecraft Linear Acceleration Limits table below. The accelerations are those induced by operation of the sensor unit while mounted to a flexible interface. The limits apply to each orthogonal axis after the acceleration is filtered using an eighth-order band pass Butterworth filter with -3dB frequencies at f1 and f2. Note that the filter has a fourth-order roll-off on both sides of the response.

Page 12 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID116

GXSUIID149

GXSUIID90

GXSUIID91

GXSUIID92

GXSUIID94

Object Number

3.4.7

3.4.7.0-1

3.5

3.5.0-1

3.6

3.6.0-1

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

3.4.7 Instrument Torque Limit (CCR X00044A)

At any time during the operational mode of the spacecraft, the sum of the magnitude of the instrument sensor unit’s uncompensated torques and the magnitude of its uncompensated linear forces multiplied by a lever arm of 2 meters shall not exceed

0.15 N-m. (CCR X00044A)

3.5 Thermal

The total heat transfer to the spacecraft of all instrument electronics units shall not exceed 220 Watts.

3.6 Instrument Purge Requirements

The spacecraft shall provide a continuous GN2 purge to the integrated Sounder sensor module when not under vacuum via the t-0 purge system.

Page 13 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID95

GXSUIID96

GXSUIID97

Object Number

4.0-1

4.0-2

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

4 Constraints In order to ensure proper instrument performance or to prevent possible instrument damage, the following Government-approved constraints are imposed by the instrument developer on spacecraft integration and test activities, including launch, activation and operations.

No constraints have been identified at this time.

Page 14 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID98

GXSUIID99

Object Number

5.0-1

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

5 GIRD Deviations This section identifies GIRD requirements that the Government has deviated from for this instrument. Where appropriate, corresponding GIRD paragraph titles and numbers are identified in parentheses.

Page 15 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID100

GXSUIID101

GXSUIID102

GXSUIID103

GXSUIID104

GXSUIID105

GXSUIID106

GXSUIID107

GXSUIID108

GXSUIID109

GXSUIID110

GXSUIID111

Object Number

6.0-1

6.1

6.1.0-1

6.1.0-2

6.2

6.2.0-1

6.2.0-2

6.2.0-3

6.2.0-4

6.2.0-5

6.2.0-6

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

6 Design Verification Requirements The following requirements represents only a portion of the overall system verification ( i.e., contractor derived requirements are not described) that must be integrated into the total system program which verifies that the system will meet the mission requirements. A system performance verification program documenting the overall verification plan, implementation, and results is required which will provide traceability from mission specification requirements to launch and initial on-orbit capability. This will also provide the baseline for tracking on-orbit performance versus pre-launch capability.

6.1 Radiated Emissions, Electric Field (RE 102)

Radiated narrow band electric field levels generated by the instrument shall not exceed the levels specified in the Sensor Unit and Electronics Unit Notches Table.

Radiated Emissions Notch Table

Frequency Range (MHz) Rationale Test Limit, dBuV/meter

1560 - 1595 GPS L1 C/A

GPS L1 C 5

1210.1 – 1245.1 GPS L2 C 5

1164.45 – 1188.45 GPS L5 5

2033.5 - 2037.5 CDAS Cmd, ORTT&C Cmd 12

(CCR X00044A)

The test procedure used for this test shall be in accordance with MIL-STD-461G, RE102. (CCR X00044A)

6.2 Reserved (CCR X00044A)

Reserved (CCR X00044A)

Reserved (CCR X00044A)

Reserved (CCR X00044A)

Reserved (CCR X00044A)

Reserved (CCR X00044A)

Reserved (CCR X00044A)

Page 16 of 16 Printed Wednesday, December 22, 2021

ID

GXSUIID112

GXSUIID113

Object Number

7.0-1

418-XO-GXSUIID-0030, RM Version, GeoXO Sounder (GXS) Unique Instrument Interface Document (UIID)

7 Acronyms APID Application Process Identifier

BRF Body Reference Frame

C&DH Command and Data Handling

CCSDS Consultative Committee for Space Data Systems

GIRD General Interface Requirements Document

GOES Geostationary Operational Environmental Satellite

GRDDP GOES-R Reliable Data Delivery Protocol

GSFC Goddard Space Flight Center

GXS GeoXO Sounder (CCR X00044A)

Hz Hertz

ICD Interface Control Document

IDD Instrument Description Document kg kilogram m meter

Mbps million bits per second mg milli-g’s (where g is gravitational acceleration at Earth surface)

NASA National Aeronautics and Space Administration

ORF Orbit Reference Frame

PORD Performance and Operational Requirements Document

SRS Shock Response Spectra

TBD to be determined

TBR to be resolved

TBS to be specified

UIID Unique Instrument Interface Document

Effective Date: August 13, 2021 418-XO-GXSUIID-0030 Expiration Date: Five years from date of last signature Baseline Version 1.2 Responsible Organization: GeoXO Flight Project/Code 418

Document Change Record (DCR)

CCR GeoXO#:X00012 Rev: Title: 418-XO-GXSUIID-0030: GeoXO Sounder UIID baseline Contract # N/A GOES S/C: GeoXO Effectivity: Instruments CCB Status: Approved Doc #: 418-XO-GXSUIID-0030 CCB Date: 04/20/2021 Doc Version: 1.0 Contract Mod#: N/A DOORs Version: 1.0 Doc Change Date: April 20, 2021 DOORs ID #: 1.0

CCR GeoXO#:X00018 Rev: Title: GXSUIID: Updates for phase A Contract # N/A GOES S/C: GeoXO Effectivity: Instruments CCB Status: Approved Doc #: 418-XO-GXSUIID-0030 CCB Date: 08/13/2021 Doc Version: 1.1 Contract Mod#: N/A DOORs Version: 1.1 Doc Change Date: Aug. 13, 2021 DOORs ID #: Modify: GXSUIID41 (1.2.2.0-1), 43 (1.2.3.0-1), 45 (1.2.4.0-1), 58 (1.3.5.0-1), 66 (1.4.1.0-1), 68 (1.4.2.0-1), 86 (1.4.5.0-1), 114 (1.3.5.0-2) Add: GXSUIID115 (1.4.5.0-2)

CCR GeoXO#:X00044 Rev: A Title: GXSUIID: Changes for phase A Contract # N/A GOES S/C: GeoXO Effectivity: Instruments CCB Status: Approved Doc #: 418-XO-GXSUIID-0030 CCB Date: 11/16/2021 Doc Version: 1.2 Contract Mod#: N/A DOORs Version: 1.2 Doc Change Date: Nov. 16, 2021 DOORs ID #: Modify: GXSUIID27 (3.0-1), 30 (3.1.1.0-1), 35 (3.1.4), 36 (3.1.4.0-1), 39

(3.2.1.0-1), 58 (3.3.5.0-1), 114 (3.3.5.0-2), 63 (3.4), 66 (3.4.1.0-1), 69 (3.4.2.0-2), 71 (3.4.3.0-1), 72 (3.4.3.0-2), 86 (3.4.5.0-1), 88 (3.4.6.0-1), 89 (3.4.6.0-2), 115 (3.4.5.0-2), 103 (6.1.0-1), 104 (6.1.0-2), 105 (6.2), 106 (6.2.0-1), 107 (6.2.0-2), 108 (6.2.0-3), 109 (6.2.0-4), 110 (6.2.0-5), 111 (6.2.0-6), 113 (7.0-1), 115 (3.4.5.0-2), 117 (3.3.6)

Add: GXSUIID118 (1), 119 (1.0-1), 120 (1.0-2), 121 (1.0-3), 122 (1.0-4), 123 (1.0-5), 124 (1.0-6), 125 (1.1), 126 (1.1.0-1), 127 (1.2), 128 (1.2.0-1), 129 (1.2.0-2), 130 (1.2.0-3), 131 (1.2.0-4), 132 (1.2.0-5), 133 (1.2.0-6), 134 (1.2.0-7), 135 (1.2.0-8), 136 (1.2.0-9), 137 (1.2.0-10), 138 (1.2.0-11), 139 (1.2.0-12), 140 (1.3), 141 (1.3.0-1), 142 (2), 143 (2.1), 145 (2.1.0-1), (144 (2.2), 146 (2.2.0-1), 117 (3.3.6), 147 (3.3.6.0-1), 148 (3.3.6.0-2), 116 (3.4.7), 149 (3.4.7.0-1);

Delete: GXSUIID105 (6.2), 106 (6.2.0-1), 107 (6.2.0-2), 108 (6.2.0-3), 109 (6.2.0-4), 110 (5.2.0-5), 111 (6.2.0-6), [replaced original text with “Reserved’; DI retains for potential future use;]