Attachment E-4 OCXUIID.pdf

Effective Date: August 12, 2021 418-XO-OCXUIID-0062 Expiration Date: Five years from date of last signature Baseline Version 1.1 Responsible Organization: GeoXO Flight Project/Code 418

Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX)

Unique Instrument Interface Document (UIID) Signature page

Prepared by:

Electronically approved by: 05/19/2021

Marc D. Rafal Date GeoXO Flight Project, Instrument Systems Engineer NASA GSFC, Code 418

Reviewed by:

Electronically approved by: 08/03/2021

Steven W. Bidwell Date GeoXO Flight Project, Mission Systems Engineer NASA GSFC, Code 418

Approved by:

Electronically approved by: 08/12/2021

Monica Todirita Date GeoXO Flight Project, Deputy Project Manager NOAA GSFC, Code 418

/GeoXO Flight Project OCX

OCXUIID

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique Instrument Interface Document (UIID)

Version: 1.1 Printed by: rkhoover Printed on: Thursday, February 10, 2022

No filter applied.

No sort applied.

Generated from DOORS 9.7.2.4

Contents

1 1Scope

1.1 1Document Overview

1.2 1Requirements Terminology

1.3 2Order of Precedence

2 3Documents

2.1 3Applicable Documents

2.2 3Reference Documents

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

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 6Optical Port Field-of-View

3.3.5 7Radiator Field-of-View

3.3.6 7Field-of-View in the +X direction

3.3.7 7Mounting

3.4 7Instrument-to-Spacecraft Disturbances

3.4.1 7Integrated Angular Momentum

3.4.2 7Angular Momentum Limits

3.4.3 8Instrument Translation Acceleration Limits

3.4.4 10Predicted Interface Force and Torque (PIFT) Responses

3.4.5 10Spacecraft Mounting Stiffness

3.4.6 11External Sourced Translation Acceleration Limits

Project: GeoXO Flight Project OCX Module: OCXUIID Baseline Version: 1.1

Contents ii

3.5 12Thermal

3.6 12Instrument Purge Requirements

3.7 12Instrument Torque Limit (CCR X00052)

4 13Constraints

5 14GIRD Deviations

5.1 14Attitude Rate Error

6 15Design Verification Requirements

6.1 15Radiated Emissions, Electric Field (RE 102)

6.2 15Radiated Emissions in DCS Receiver Bands

7 17Acronyms

Contents iii

Page 1 of 17 Printed Thursday, February 10, 2022

ID

OCXUIID1

OCXUIID2

OCXUIID3

OCXUIID4

OCXUIID5

OCXUIID6

OCXUIID7

OCXUIID8

OCXUIID9

OCXUIID10

OCXUIID11

Object Number

1.0-1

1.0-2

1.0-3

1.0-4

1.0-5

1.1

1.1.0-1

1.2

1.2.0-1

1.2.0-2

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

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

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

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

The OCX is a hyperspectral imager in geostationary, or GEO, orbit. Hyperspectral imaging collects and processes information from across the electromagnetic spectrum including visible light, near-infrared and ultraviolet frequencies to create a highly detailed view of physical and biological conditions in coastal waters. The instruments will collect data on a three-axis body-stabilized satellite in geosynchronous orbit.

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.

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.

1.1 Document Overview

Together, the General Interface Requirements Document (GIRD) and the OCX UIID establish the OCX-spacecraft interface requirements. The GIRD applies to all GeoXO instruments while the OCX UIID is specific to the OCX. 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 OCX 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.

1.2 Requirements Terminology

The following requirements terminology is used throughout this document:

The use of “shall” designates a requirement that must be met. (CCR X00052)

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ID

OCXUIID12

OCXUIID13

OCXUIID14

OCXUIID125

OCXUIID15

OCXUIID16

OCXUIID17

OCXUIID18

OCXUIID19

OCXUIID20

OCXUIID21

OCXUIID22

OCXUIID23

Object Number

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

1.2.0-13

1.3

1.3.0-1

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

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.”

The use of “will” designates a statement of fact or intention of the government.

(CCR X00052)

The term “TBD” means, “to be determined” and is used when no value is available with subsequent study needed to obtain it. (CCR X00052)

The use of “may” designates that permission has been granted by the government.

(CCR X00052)

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

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

The term “TBR” means means “to be refined/reviewed” for a value that is subject to review for appropriateness and is subject to revision. The vendor is liable for compliance with the information marked “TBR” as if the “TBR” notation did not exist. (CCR X00052)

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

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

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.

The orbit reference frame (ORF), and the body reference frame (BRF), will be as defined in the GIRD.

1.3 Order of Precedence

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).

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ID

OCXUIID24

OCXUIID25

OCXUIID26

OCXUIID27

OCXUIID28

Object Number

2.1

2.1.0-1

2.2

2.2.0-1

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

2 Documents

2.1 Applicable Documents

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)

2.2 Reference Documents

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

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ID

OCXUIID29

OCXUIID30

OCXUIID31

OCXUIID32

OCXUIID33

OCXUIID34

OCXUIID35

OCXUIID36

OCXUIID37

OCXUIID38

OCXUIID39

OCXUIID40

OCXUIID41

OCXUIID42

OCXUIID43

OCXUIID44

OCXUIID45

OCXUIID46

OCXUIID47

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-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

3 Allocations The GeoXO spacecraft shall provide communications, power, and a platform for the OCX instrument. The following paragraphs allocate these resources to OCX.

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 65 million bits per second (TBR) when averaged over any 5 second period.

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 OCX 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

The OCX shall transmit to the spacecraft no more than 400 GRDDP Packets per second. (CCR X00052)

3.2 Power

3.2.1 Average Operational Power

The OCX shall draw operational average power, inclusive of heaters, of no more than 150 Watts from up to four (TBR) total feeds including primary and redundant.

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

3.2.2 Maximum Operational Power

The OCX shall draw operational maximum power of no more than 240 Watts (TBR).

Operational maximum power is the total power into an instrument averaged over any 20ms period.

3.2.3 Average Survival Power

The OCX shall draw average survival power of no more than 100 (TBR) Watts.

Average survival power is the total power into an instrument averaged over any 72 minute period.

3.2.4 Maximum Survival Power

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ID

OCXUIID48

OCXUIID49

OCXUIID50

OCXUIID51

OCXUIID52

OCXUIID53

OCXUIID54

OCXUIID55

OCXUIID56

OCXUIID57

OCXUIID58

Object Number

3.2.4.0-1

3.3

3.3.0-1

3.3.1

3.3.1.0-1

3.3.2

3.3.2.0-1

3.3.2.0-2

3.3.3

3.3.3.0-1

3.3.3.0-2

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

The OCX shall draw maximum survival power of no more than 150 (TBR) Watts.

Survival maximum power is the total power into an instrument averaged over any 20ms period.

3.3 Mechanical

The requirements in this section shall apply to the structural and mechanical components of the instrument flight units (sensor unit, electronics unit and, if applicable, auxiliary electronics unit).

3.3.1 Mass Properties

The OCX, including all units and cabling between units, shall have mass less than 152 (TBR) kilograms.

3.3.2 Cabling Between Units

If there are external units mounted directly to the spacecraft, the OCX shall operate with cable lengths between its units up to, but not exceeding, 4m. (CCR X00052)

Cables between OCX units shall be the responsibility of the OCX contractor.

3.3.3 Volume

The OCX sensor shall be mounted on the Earth Pointing Platform (EPP) of the spacecraft.

The OCX Sensor Unit stowed and operational (deployed) configurations, including mounts, thermal blankets and connectors, shall have dimensions that do not exceed the limits provided below.

Depth (Z direction, Nadir): 1500 millimeters Width (X direction, parallel to orbit): 1220 millimeters Height (Y direction, normal to orbit): 1230 millimeters

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ID

OCXUIID58

OCXUIID59

OCXUIID60

OCXUIID61

Object Number

3.3.3.0-2

3.3.4

3.3.4.0-1

3.3.4.0-2

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

Rationale: The narrow dimension allows for other instruments to share the EPP with the OCX

3.3.4 Optical Port Field-of-View

The Instrument LOS shall nominally be aligned with the +Z axis in the Body Reference Frame (BRF) as defined in the GIRD. (CCR X00052)

The spacecraft shall provide the sensor unit’s optical port a clear field-of-view within 65o of nadir as shown in the following figure.

Optical Port Field-of-View

(CCR X00052)

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ID

OCXUIID62

OCXUIID63

OCXUIID64

OCXUIID65

OCXUIID66

OCXUIID67

OCXUIID68

OCXUIID69

OCXUIID70

OCXUIID71

OCXUIID72

OCXUIID73

OCXUIID74

OCXUIID75

OCXUIID76

Object Number

3.3.5

3.3.5.0-1

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

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

3.3.5 Radiator Field-of-View

The instrument shall dedicate the +Y face of the instrument for a radiator surface with the axis in the Body Reference Frame (BRF) as defined in the GIRD.

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 50 W back loading.

3.3.6 Field-of-View in the +X direction

The spacecraft will provide 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 X00052)

The spacecraft will 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 X00052)

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 include kinematic mounts for its mechanical interface to the spacecraft. (CCR X00052)

3.4 Instrument-to-Spacecraft Disturbances

These requirements shall 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. (CCR X00052)

OCX Integrated Angular Momentum Limits

Axis

Limit

(N‐m‐s2) roll 0.5 pitch 0.35 yaw 0.5

3.4.2 Angular Momentum Limits

Page 8 of 17 Printed Thursday, February 10, 2022

ID

OCXUIID77

OCXUIID78

OCXUIID79

OCXUIID80

Object Number

3.4.2.0-1

3.4.2.0-2

3.4.3

3.4.3.0-1

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

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.

OCX Angular Momentum Limits

Axis Limit

(N‐m‐s) roll 0.1 pitch 0.05 yaw 0.1

The absolute value of the bandpass-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.

(CCR X00052)

OCX Bandpass‐Filtered Angular Momentum Limits f1 f2

Limit

(N‐m‐s)

0.01 0.25 0.05

0.25 1 0.02

1 10 0.015

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 Bandpass 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 bandpass 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.

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ID

OCXUIID104

OCXUIID105

Object Number

4.0-1

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) 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 17 Printed Thursday, February 10, 2022

ID

OCXUIID106

OCXUIID107

OCXUIID108

OCXUIID109

Object Number

5.0-1

5.1

5.1.0-1

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) 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.

5.1 Attitude Rate Error

The instrument shall meet all image performance requirements while amplitudes of the instrument mounting frame (IMF) angular rates per axis relative to the ORF and the total spacecraft angular rate data latency are less than the limits in the Instrument Limit for Angular Rate Error vs Latency Figure provided below. This requirement supersedes the GIRD54 requirement.

Total Spacecraft Gyro Signal Latency and Angular Rate Error Trade Space Figure

Page 15 of 17 Printed Thursday, February 10, 2022

ID

OCXUIID110

OCXUIID111

OCXUIID112

OCXUIID113

OCXUIID114

OCXUIID115

OCXUIID116

OCXUIID117

OCXUIID118

OCXUIID119

Object Number

6.0-1

6.1

6.1.0-1

6.1.0-2

6.1.0-3

6.2

6.2.0-1

6.2.0-2

6.2.0-3

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) 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.

6.1 Radiated Emissions, Electric Field (RE 102)

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

Radiated narrow band electric field levels generated by the instrument shall not exceed the levels specified in Figure RE102-3 of MIL-STD-461G, applicable to fixed wing external.

Radiated narrow band electric field levels generated by the instrument shall not exceed the levels specified in the Radiated Emissions Notch Table.

Sensor Unit and Electronics Unit Notches Table

Frequency Range (MHz)

Rationale Test Limit, dBuV/ meter

1560 - 1595 GPS L1 C/A

GPS L1 C

1210.1 – 1245.1 GPS L2 C 5

1164.45 – 1188.45 GPS L5 5

2033.5-2037.5 CDAS Cmd, ORTT&C

Cmd

Note: When S/C vendor selects GPS Band to be used other bands will be released.

(CCR X00052)

6.2 Radiated Emissions in DCS Receiver Bands

Radiated emission measurements in the DCS receiver bands shall be made in accordance with MIL-STD-461G, RE102 with the EMI meter replaced by a spectrum analyzer preceded by a low noise pre-amplifier such that the test system noise figure is equal to or less than 3 dB, e.g., an HP-8566 spectrum analyzer preceded by a MITEQ AU-2A-0550 pre-amplifier or equivalent.

The spectrum analyzer levels and the difference in the levels shall be recorded for both white noise and spurious signals before and after power is applied to the instrument clock and control signals.

The test antenna shall be tuned to the center of the frequency band specified in DCS EMC Test Parameters Table.

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ID

OCXUIID120

OCXUIID121

OCXUIID122

Object Number

6.2.0-4

6.2.0-5

6.2.0-6

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) Unique

Instrument Interface Document (UIID)

Prior to making the actual measurements, the test antenna shall be de-mated and the cable terminated with 50 ohms for self-calibration.

The noise floor of the measuring equipment shall be verified to be lower than the specified maximum signal level in a 100 Hz resolution bandwidth.

Radiated emission levels generated by the instrument shall not exceed the maximum signal levels specified in the DCS EMC Test Parameters Table below.

DCS (401.700 to 402.400 MHZ) EMC Test Parameters Table

Unit Name Designated Frequency

Band (MHz)

Measurement Bandwidth

(Hz)

Dwell Time

(Seconds)

Minimum Measurement Time Analog Measurement

Receiver (sec/kHz)

Max. Field Intensity (dBuV/m)

Electronics Unit Within the S/C

Bus Faraday cage

401.700- 402.400

100 0.015 0.15 -8

Sensor Unit Outside S/C Bus

Faraday Cage

(OCX)

401.700- 402.400

100 0.015 0.15 -24

(CCR X00052)

Page 17 of 17 Printed Thursday, February 10, 2022

ID

OCXUIID123

OCXUIID124

Object Number

7.0-1

418-XO-OCXUIID-0062, RM Version, Geostationary Extended Observations (GeoXO) Ocean Color Instrument (OCX) 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 EPP Earth Pointing Platform GOES Geostationary Operational Environmental Satellite GSFC Goddard Space Flight Center OCX Ocean Color Instrument for GeoXO Hz Hertz ICD Interface Control Document IDD Instrument Description Document IMF Instrument Mounting Frame kg kilogram m meter Mbps million bits per second 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 12, 2021 418-XO-OCXUIID-0062 Expiration Date: Five years from date of last signature Baseline Version 1.1 Responsible Organization: GeoXO Flight Project/Code 418

Document Change Record (DCR)

CCR GeoXO#: X00019 Rev: A Title: 418-XO-OCXUIID-0062 Baseline OCX UIID Contract # N/A GOES S/C: GeoXO Effectivity: Instruments CCB Status: Approved Doc #: 418-XO-OCXUIID-0062 CCB Date: 08/12/2021 Doc Version: 1.0 Contract Mod#: N/A DOORs Version: 1.0 Doc Change Date: August 12, 2021 DOORs ID #: All

CCR GeoXO#: X00052 Rev: Title: OCXUIID: Update Req for Phase A Contract # N/A GOES S/C: GeoXO Effectivity: Instruments CCB Status: Approved Doc #: 418-XO-OCXUIID-0062 CCB Date: 02/04/2022 Doc Version: 1.1 Contract Mod#: N/A DOORs Version: 1.1 Doc Change Date: Feb. 4, 2022 DOORs ID #: Modify: OCXUIID11 (1.2.0-2), 13 (1.2.0-4), 14 (1.2.0-5), 17 (1.2.0-9), 39 (3.1.4.0-1), 54 (3.3.2.0-1), 60 (3.3.4.0-1), 61 (3.3.4.0-2), 66 (3.3.6.0-1), 67 (3.3.6.0-2), 71 (3.3.7.0-3), 75 (3.4.1.0-1), 78 (3.4.2.0-2), 80 (3.4.3.0-1), 81 (3.4.3.0-2), 98 (3.4.6.0-1), 99 (3.4.6.0-2), 115 (6.1.0-3), 122 (6.2.0-6)

Add: OCXUIID125 (1.2.0-6), 126 (3.7), 127 (3.7.0-1)