Attachment B_ACX_PORD.pdf

Effective Date: 418-XO-ACXPORD-0121 Responsible Organization: GeoXO Flight Project/Code 418 Draft Version 0.11a

To verify the correct version of this document, please contact the GeoXO Series Configuration Management Office.

Geostationary Extended Observations (GeoXO) Atmospheric Composition (ACX)

Performance and Operational Requirements Document

(PORD)

Signature page

Prepared by:

Erin M. Farrell Date GeoXO Flight Project, Instrument Systems Engineer NASA GSFC, Code 418

Reviewed by:

Phillip A. Driggers Date GeoXO Flight Project, Instrument Manager

Sergey Krimchansky Date GeoXO Flight Project, Instrument Systems Manager

Approved by:

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

/GeoXO Flight Project ACX

ACXPORD

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended Observations (GeoXO) Atmospheric Composition (ACX) Performance and Operational Requirements Document (PORD) Phase B

Version: 0.11 (a) Printed by: hlhedger Printed on: Friday, August 4, 2023

No filter applied.

No sort applied.

Generated from DOORS 9.7.2.4

Contents

1 1Scope

1.1 1Identification

1.2 1Mission Review

1.3 1Document Overview

1.4 1Terminology

1.5 2Definitions

1.6 4Requirement Applicability

2 5Documents

2.1 5Applicable Documents

2.2 5Reference Documents

3 6Sensor Requirements

3.1 6Sensor Definition

3.1.1 6ACX Modes

3.1.1.1 6Safe Mode

3.1.1.2 7Normal Operational Mode

3.1.1.3 7Diagnostic Mode

3.1.1.4 8Outgassing

3.1.2 8On-Orbit Operations

3.1.2.1 8Scanning Across the Sun

3.1.2.2 8Eclipse

3.1.2.3 8Operations After Maneuvers

3.1.2.3.1 8Spacecraft Maneuvers

3.1.2.3.2 9Post Storage Activation

3.1.2.4 9Detector Operating Temperatures

3.2 9Normal Operational Mode Sensor Requirements

3.2.1 9Coverage

3.2.1.1 9Coverage Rate

3.2.1.2 10Flexible and Efficient Imaging Pattern

3.2.1.3 10Simultaneity

3.2.1.4 10Data Latency

3.2.2 11Channel Definitions, SNR, Dynamic Range

3.2.2.1 11Baseline

3.2.2.2 13System Spectral Resolution

Project: GeoXO Flight Project ACX Module: ACXPORD Baseline Version: 0.11 (a)

Contents ii

3.2.2.2.1 13Spectral Response Envelope

3.2.2.2.2 13Within Channel Spectral Response Uniformity

3.2.2.2.3 14Channel Center Wavelength Knowledge

3.2.3 14Spatial Resolution and Sampling

3.2.3.1 14System Modulation Transfer Function

3.2.3.2 15Spatial Response Uniformity

3.2.3.3 15Ringing from a Sharp Edge

3.2.4 15Image Navigation and Registration

3.2.4.1 15Star Sensing

3.2.4.2 15INR Performance Requirements

3.2.4.2.1 16Navigation

3.2.4.2.2 16Frame-to-Frame Registration

3.2.4.2.3 16Within Frame Registration

3.2.4.2.4 16Channel-to-Channel Registration

3.2.5 16Radiometric Accuracy and Precision

3.2.5.1 16Repeatability

3.2.5.1.1 16Pixel-to-Pixel

3.2.5.2 16Coherent Noise

3.2.5.3 17Calibration of Channels

3.2.5.4 18Spatial Uniformity of Data

3.2.5.5 18Crosstalk

3.2.5.5.1 18Channel-to-Channel

3.2.5.5.2 18Within Channel

3.2.5.6 18Blooming

3.2.5.7 18Quantization Step Size

3.2.5.8 19Reserved

3.2.5.9 19Polarization

3.2.5.9.1 19Polarization Control

3.2.6 19System Linearity

3.2.7 19Data Compression

3.2.7.1 19Lossless Data Compression

3.2.7.2 19Lossy Compression

3.2.7.3 20Vizualization Algorithm

3.2.7.4 20Stray Light

4 21Design Requirements

4.1 21Reliability

4.2 21Redundancy

4.2.1 21Redundant Component Selectability

Contents iii

4.2.2 21Interchangeability of Flight Model Units

4.2.3 21Reserved

4.3 21Mechanical Requirements

4.3.1 21Design Limit Loads

4.3.2 22Yield Strength

4.3.3 22Ultimate Strength

4.3.4 23Unit Stiffness

4.3.5 23Critical Members Design Values

4.3.6 23Redundant Members Design Values

4.3.7 23Selective Design Values

4.3.8 23Fracture Control

4.3.9 24Mechanisms

4.3.10 25Pressurized Units

4.3.11 25Alignment Reference

4.3.12 25Precision Component Assembly

4.4 25Thermal Requirements

4.4.1 25Mission Allowable Temperatures

4.4.2 26Thermal Gradients

4.4.3 26Non-Operational Temperatures

4.4.4 26Thermal Control Hardware

4.4.5 26Detector Cooling Margin

4.4.6 27Radiator

4.4.7 27Heat Pipe (Two-phase Heat Transfer Device)

4.5 27Power Requirements

4.5.1 27Power Regulators and Supplies

4.5.2 27Fuses

4.5.3 27Covers for test Connectors

4.5.4 28Keyed Connectors

4.6 28Onboard Processors Requirements

4.6.1 28Flight Load Non-Volatile Memory

4.6.2 28Commandable Reinitialization

4.6.3 28Deterministic Power-on Configuration

4.6.4 28Fail-safe Recovery Mode

4.7 28Flight Software Requirements

4.7.1 28Language and Methodology

4.7.2 28Flight Software Upload

4.7.3 28Flexibility and Ease of Software Modification

4.7.4 29Version Identifiers

Contents iv

4.7.5 29Flight Processor Resource Sizing

4.7.6 30Software Event Logging

4.7.7 30Warm Restart

4.7.7.1 30Processor Re-Start

4.7.7.2 30Autonomous Re-Start

4.7.8 30Memory Integrity

4.7.8.1 30Memory Verification

4.7.8.2 30Bit Error Detection and Correction

4.7.9 30Memory Dump

4.7.10 31Telemetry Cadence and Dwell Control

4.7.11 31Long-Duration Test

4.7.12 31Unnecessary and Unreachable Software

5 32Ground Support Equipment and Development

5.1 32Electrical System Test Equipment

5.2 32Flight Software Development Environment

5.3 32Ground Processing Demonstration System

5.4 33FM and GSE Shipping Containers

6 34ACX Simulators

6.1 34ACX Instrument Hardware Simulator (ACX-IHS)

6.2 34ACX Instrument Software Simulator (ACX-ISS)

7 36FM Design Verification Requirements

7.1 36Powered-on Operating Time and Trouble-Free Performance Testing

7.2 36Structural and Mechanical Verification Requirements

7.2.1 36Mechanical Test Factors and Duration

7.2.2 38Minimum Workmanship

7.2.3 39Testing in Flight Configuration

7.2.4 39Structural Proof Testing

7.2.5 39Modal Survey Characterization

7.2.6 40Structural Qualification

7.2.7 40Deployment and Articulation Verification

7.2.8 40Life Test

7.2.9 40Mechanical Clearance Verification

7.3 41Electromagnetic Compatibility Verification

7.3.1 41General

7.3.2 41Electrostatic Arc-Discharge Susceptibility

7.3.2.1 41External Surface-to-Surface direct discharge

Contents v

7.3.2.2 41Deep Dielectric Charging

7.3.2.3 41ESD Characteristics

7.4 42Thermal Test Requirements

7.4.1 42General

7.4.1.1 42Thermal Test Chronology

7.4.1.2 42Pressure

7.4.2 42Thermal Vacuum

7.4.2.1 42Transition Rates

7.4.2.2 43Corona Operation

7.4.2.3 43Hot and Cold Start Demonstrations

7.4.2.4 43Heater Verification

7.4.2.5 43Flight Temperature Sensor Verification

7.4.3 43TV Thermal Cycling

7.4.3.1 43Cumulative Cycles

7.4.3.2 44Ambient Pressure Thermal Cycling Substitution

7.4.3.3 44Qualification, Protoflight and Acceptance Temperatures

7.4.3.4 45Survival Heater Verification

7.4.3.5 45Temperature test tolerances

7.4.3.6 45Plateau Criteria

7.4.4 45Thermal Balance (TB)

7.4.4.1 45Balance Points

7.4.4.2 45 Instrument Configuration

7.4.4.3 46Accuracy and Knowledge

7.4.4.4 46Steady State Criteria

7.5 46Test Condition Tolerances

8 49Acronyms

Contents vi

Page 1 of 50 Printed Friday, August 4, 2023

ID

ACXPORD1

ACXPORD2

ACXPORD3

ACXPORD4

ACXPORD5

ACXPORD6

ACXPORD7

ACXPORD8

ACXPORD9

ACXPORD10

ACXPORD11

ACXPORD534

ACXPORD536

ACXPORD537

ACXPORD12

ACXPORD15

Object Number

1.1

1.1.0-1

1.2

1.2.0-1

1.2.0-2

1.2.0-3

1.2.0-4

1.3

1.3.0-1

1.4

1.4.0-1

1.4.0-2

1.4.0-3

1.4.0-4

1.4.0-5

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended Observations (GeoXO) Atmospheric Composition (ACX)

Performance and Operational Requirements Document (PORD)

1 Scope

1.1 Identification

This Performance and Operational Requirements Document (PORD) sets forth the performance requirements for the National Oceanic and Atmospheric Administration (NOAA) Geostationary eXtended Observations (GeoXO) Atmospheric Composition (ACX) instrument.

1.2 Mission Review

The ACX is a hyperspectral, UV through visible imaging spectrometer used to measure environmental data as part of a 3-axis stabilized, geostationary satellite system. The ACX remotely collects imagery of the superregional region for national air quality forecasting capability, hazard forecasting, and fire pollutant forecasting and warnings.

The ACX objectives are as follows:

⦁ Provide new NOAA atmospheric composition operational data that will be used by NOAA and other public and private agencies to produce forecasts of air quality and pollution.

The ACX provides data to the Ground System via the spacecraft communication system. The Ground System takes the data, spacecraft telemetry data, orbit determination data and other required information and autonomously generates radiometrically calibrated and navigated data (Level 1b data) for the NOAA users.

The Ground System procured by the Government will implement algorithms developed by the ACX contractor. The Ground System will calibrate and navigate the data to generate Level 1b data.

1.3 Document Overview

This document contains all performance requirements for the ACX instrument and Ground Support Equipment (GSE). This document, the General Interface Requirements Document (GIRD), and the ACX Unique Instrument Interface Document (UIID) define all instrument to spacecraft interfaces for the ACX instrument.

1.4 Terminology

The use of “shall” designates a requirement that must be met.

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

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

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

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

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ID

ACXPORD19

ACXPORD20

ACXPORD21

ACXPORD22

ACXPORD23

ACXPORD24

ACXPORD25

ACXPORD26

ACXPORD13

ACXPORD27

ACXPORD28

ACXPORD29

ACXPORD547

ACXPORD31

Object Number

1.5

1.5.0-1

1.5.0-2

1.5.0-3

1.5.0-4

1.5.0-5

1.5.0-6

1.5.0-7

1.5.0-8

1.5.0-9

1.5.0-10

1.5.0-11

1.5.0-12

1.5.0-13

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

1.5 Definitions

Throughout this document, the following definitions apply:

Accuracy: Refers to the error in a measurement that is the difference between the measurement result and the object to be measured (the measured or true value). It includes both systematic and random errors. Systematic errors must be estimated from an analysis of the experimental conditions and techniques. Random errors can be determined, and reduced, through repeated measurements under identical conditions.

Albedo: Refers to the fraction of the solar spectrum taken from the default MODTRAN solar irradiance file (newkur.dat) that is reflected by the Earth at the top of the atmosphere assuming a Lambertian surface (see ACX Radiances for values).

All requirements/all performance requirements/all operational requirements: Refers to any performance characteristic or requirement in the ACX PORD, ACX UIID, and the GIRD.

Band: A set of channels.

Channel: A measurement that is an aggregate of one or more spectral samples that meets or exceeds ACX requirements.

Collection: The set of all frames from all telescopes for a single integration period.

Credible Failure: A failure condition that has a reasonable likelihood of occurrence over the mission life. With consideration of reliability analysis and engineering experience, the Government technical authority will determine credibility of failure.

For the purposes of this document, failures of structure, pressure vessels, and pressurized lines and fittings are not considered credible failure modes if those elements comply with the applicable requirements of this document.

Derived Noise Equivalent Delta Radiance (NEdN): Refers to the NEdN required to meet the Noise Equivalent Delta Temperature (NEDT) specification or Signal-to- Noise Ratio (SNR) specification.

Detector sample or element: Refers to the output of a physical detector after the Analog-to-Digital (A/D) converter and Time Delay and Integration (TDI) processing, if applicable.

Eclipse: Defined as when the solar disk is completely occulted by the Earth or Moon, as viewed from the satellite.

Fixed Grid Angle: Refers to North/South (NS) and East/West (EW) Euler angles defined as follows. Starting with the orbit reference frame (ORF) in GIRD62 at the ideal satellite location, a positive NS angle is a rotation of the ORF about its +x axis, and a positive EW angle is a subsequent rotation of the rotated frame about its +y axis. The +z axis of the final frame is the line of sight (LOS) represented by the EW and NS fixed-grid angles.

Frame: Collection of pixels from a contiguous region as commanded by a minimum bounding rectangle.

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ID

ACXPORD32

ACXPORD33

ACXPORD568

ACXPORD569

ACXPORD570

ACXPORD571

ACXPORD572

ACXPORD34

ACXPORD35

ACXPORD573

ACXPORD36

Object Number

1.5.0-14

1.5.0-15

1.5.0-16

1.5.0-17

1.5.0-18

1.5.0-19

1.5.0-20

1.5.0-21

1.5.0-22

1.5.0-23

1.5.0-24

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

Fully Functional Configuration: Being able to perform the following functions: scene radiance measurement; radiometric calibration; star sensing; on-orbit monitoring of calibration sources and instrument response changes; acquisition of sensor health and status data; generation of sensor, calibration, monitoring, health and status data streams; and reception and execution of command and control data.

Launch: The time between lift off and the separation of the GeoXO satellite from the launch vehicle.

Level 0: Raw data reconstructed to unprocessed instrument data at full space-time resolution with all available supplemental information to be used in subsequent processing (e.g., ephemeris, health and safety) appended.

Level 1a: Unpacked and reformatted Level 0 data with all supplemental information to be used in subsequent processing appended. Data generally presented as full space/time resolution. A wide variety of sub-level products are possible. Note: For ACX, data are not resampled.

Level 1b data: Unpacked and reformatted Level 0 data with all supplemental information to be used in subsequent processing appended. Radiometric calibration and navigation are applied to produce parameters in physical units. Data generally presented as full space/time resolution. Note: For ACX, data are not resampled.

Level 2+: Retrieved environmental variables (e.g., sea surface temperature) and higher products.

Mission Allowable Temperatures (MAT): Mission Allowable Temperatures are the established range of temperatures that instrument units are permitted to experience while operating in orbit. MAT are established based upon analytical temperature predictions with appropriate margin based on the state of the thermal design. MAT encompasses worst-case operating temperature predictions, uncertainty, and any contractor desired temperature margin.

Navigation: Refers to the determination of the location of each pixel relative to a fixed reference, namely for the ACX, the Geodetic Reference System 80 (GRS80) geoid viewed from the idealized geostationary position, with latitude and longitude information appended in the Level 1b product.

Navigation Error: Refers to the angular error of locations in the fixed-grid angles.

Non-operational Temperatures (NOT): Non-operational Temperatures are the established range of temperatures that instrument units are permitted to experience while not operating and not powered. NOT represent the permissible range while the hardware is powered off. Survival heaters maintain hardware at or above the cold NOT limits and passive design maintains hardware below the upper NOT limits. NOT are also known as non-operating MAT.

Pixel: All spectral channels associated with a given spatial resolution element after processing (detector element projection), including calibration and navigation (Level 1b).

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ID

ACXPORD37

ACXPORD38

ACXPORD39

ACXPORD40

ACXPORD41

ACXPORD42

ACXPORD43

ACXPORD44

ACXPORD45

ACXPORD46

ACXPORD47

ACXPORD48

Object Number

1.5.0-25

1.5.0-26

1.5.0-27

1.5.0-28

1.5.0-29

1.5.0-30

1.5.0-31

1.5.0-32

1.5.0-33

1.6

1.6.0-1

1.6.0-2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

Polarization Sensitivity: Defined as the ratio of the difference between maximum and minimum output to the sum of the maximum and minimum output obtained when the plane of incoming 100% linearly polarized radiation is rotated through 180 degrees.

Precision: Refers to the standard deviation of a statistically meaningful number of samples of a measurement.

Registration: Refers to maintaining the spatial relationship between pixels within frames, between frames, and between channels.

SNR: Signal-to-Noise Ratio.

Spectral Sample: A measurement within a channel that may or may not be aggregated for transmission to the ground.

Superregional ACX: Defined as a rectangle 8.0215° x 4.8129°, the equivalent at nadir of 5000 kilometer East/West x 3000 kilometer North/South, nominally centered at 30° N and 97° W.

Swath: Refers to any set of detector samples that are collected during a continuous scan or stepping of the detectors over the scene, in a horizontal fashion, which covers the entire horizontal extent of the scene.

Task: Repeating data collection pattern providing coverage of one or more observing regions.

Unit: A functional subdivision of a subsystem and generally a self-contained combination of items performing a function necessary for the subsystem's operation.

Examples are electronics unit and sensor unit.

1.6 Requirement Applicability

The requirements in this ACX PORD pertain to the ACX ‘system’, which may include motors, optics, detectors, signal processing electronics and software, and ground processing. The ACX contractor is not responsible for the whole Ground System, but certain specifications may require some level of ground processing after collection but before data distribution, i.e. decompression, re-sampling, and calibration.

All requirements apply over the entire life of the instrument. Data performance requirements, such as Modulation Transfer Function (MTF) and Image Navigation and Registration (INR), apply to data after all ground processing, except as indicated.

Page 5 of 50 Printed Friday, August 4, 2023

ID

ACXPORD49

ACXPORD50

ACXPORD51

ACXPORD52

ACXPORD53

Object Number

2.1

2.1.0-1

2.2

2.2.0-1

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

2 Documents

2.1 Applicable Documents

The following form a part of this specification to the extent specified herein.

1) CCSDS Recommendation for Space Data System Standards, Image Data Compression, CCSDS 122.0-B-2, September 2017.

2) CCSDS Recommendation for Space Data System Standards, Low- Complexity Lossless and Near-Lossless Multispectral and Hyperspectral Image Compression, CCSDS 123.0-B-2, February 2019.

3) Structural Design and Test Factors of Safety for Spaceflight Hardware, NASA, Document Number NASA-STD-5001B

4) General Environmental Verification Standard (GEVS) for GSFC Flight Programs and Projects, Document Number GSFC-STD-7000B

5) NASA Payload Safety Requirements, NASA-STD-8719.24A with NASA- STD-8719.24-ANNEX Rev B

6) Geostationary eXtended Observations (GeoXO) Flight Project Atmospheric Composition (ACX) Radiances Upwelling Document, Document Number 418-XO-RPT-0075

2.2 Reference Documents

The following reference documents are in DOORS.

1. Report concerning Space Data System Standards: LOSSLESS

MULTISPECTRAL AND HYPERSPECTRAL IMAGE COMPRESSION,

Informational Report CCSDS 120.2-G-2, GREEN BOOK, December 2022

2. SPECTRAL PREPROCESSING TRANSFORM FOR MULTISPECTRAL

AND HYPERSPECTRAL IMAGE COMPRESSION Recommended Standard, CCSDS 122.1-B-1, BLUE BOOK, September 2017.

3. Moving Mechanical Assemblies for Space and Launch, AIAA S-114A-2020, Jan. 14, 2021

4. General Specification for Assemblies, Moving Mechanical, for Space and Launch Vehicles, Document Number MIL-A-83577B

5. Space Mechanisms Handbook, Document Number NASA TP-1999-206988, March 1, 2002

Page 6 of 50 Printed Friday, August 4, 2023

ID

ACXPORD54

ACXPORD55

ACXPORD56

ACXPORD57

ACXPORD58

ACXPORD59

ACXPORD60

ACXPORD61

ACXPORD62

ACXPORD63

ACXPORD64

ACXPORD65

Object Number

3.1

3.1.1

3.1.1.0-1

3.1.1.0-2

3.1.1.0-3

3.1.1.0-4

3.1.1.0-5

3.1.1.0-6

3.1.1.1

3.1.1.1.0-1

3.1.1.1.0-2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3 Sensor Requirements

3.1 Sensor Definition

3.1.1 ACX Modes

The ACX shall execute commands to individually enable and disable each autonomous function.

Rationale: Autonomous capability needs to be able to be disengaged as well.

The ACX shall initiate all commanded mode transitions in no more than 20 seconds after receipt of command.

Rationale: Mode transitions should occur rapidly for operators.

The ACX shall make limits and triggers of autonomous functions changeable by command.

Rationale: Autonomous functions should be controlled by operators if there is a special need to do so.

The ACX shall transition from its current mode to any other mode without causing permanent damage to itself.

Rationale: Mode transitions should occur without damage.

The ACX shall indicate the mode of the instrument in housekeeping telemetry.

Rationale: Knowledge of instrument modes is needed for data processing.

The ACX shall provide command and housekeeping telemetry functions in all powered modes.

Rationale: Command and housekeeping telemetry is necessary for monitoring instrument health at all times.

3.1.1.1 Safe Mode

The ACX shall implement a Safe Mode.

Rationale: The ACX needs a Safe Mode to enable straightforward storage.

The ACX shall be in a thermally, electrically, and optically safe configuration for an indefinite period of time while in Safe Mode.

Rationale: Safe Mode of instrument enables a thermally and optically safe configuration for storage.

Page 7 of 50 Printed Friday, August 4, 2023

ID

ACXPORD66

ACXPORD67

ACXPORD68

ACXPORD69

ACXPORD70

ACXPORD71

ACXPORD202

ACXPORD203

ACXPORD72

ACXPORD73

ACXPORD74

ACXPORD75

Object Number

3.1.1.1.0-3

3.1.1.2

3.1.1.2.0-1

3.1.1.2.0-2

3.1.1.3

3.1.1.3.0-1

3.1.1.3.0-2

3.1.1.3.0-3

3.1.1.3.0-4

3.1.1.3.0-5

3.1.1.3.0-6

3.1.1.3.0-7

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

The ACX shall enter Safe Mode upon receipt of a ground command, receipt of an autonomous safe mode command from the observatory, or detection of internal faults capable of causing permanent damage to the instrument.

Rationale: The ACX needs to employ the Safe Mode after fault detection to ensure that there is time for recovery.

3.1.1.2 Normal Operational Mode

The ACX shall be in a fully functional configuration while in Normal Operational Mode.

Rationale: Normal mode is used for observations that require full functionality.

The ACX shall meet all performance requirements while in Normal Operational Mode without receiving commands or data loads for a minimum of 7 days.

Rationale: Autonomy is required for a period of 7 days, without impacting performance.

3.1.1.3 Diagnostic Mode

The ACX shall implement a Diagnostic Mode.

Rationale: Diagnostic mode is needed for diagnosing anomalies.

The ACX shall enter Diagnostic Mode only on command.

The ACX data transmission rate in Diagnostic Mode shall comply with the allocation in the ACX UIID.

The ACX shall be in a fully functional configuration while in Diagnostic Mode.

Rationale: Diagnostic mode must be fully functional.

The ACX shall by command send telemetry for selected channels while in Diagnostic Mode.

Rationale: Diagnostic mode will afford commandable channel engagement for diagnosing anomalies.

The ACX shall by command send the individual measurement in those cases where Time Delay and Integration (TDI) data is digitally processed off the focal plane while in Diagnostic Mode.

Rationale: Diagnostic mode will send data from TDI if employed to help in validation and in assessing anomalies.

The ACX shall by command send data from all detectors while in Diagnostic Mode without exceeding the telemetry allocation given to ACX.

Rationale: Diagnostic mode will send data from all detectors to help in validation and in assessing anomalies.

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ID

ACXPORD76

ACXPORD77

ACXPORD78

ACXPORD79

ACXPORD80

ACXPORD81

ACXPORD82

ACXPORD86

ACXPORD549

ACXPORD87

ACXPORD88

ACXPORD89

ACXPORD91

ACXPORD92

Object Number

3.1.1.3.0-8

3.1.1.3.0-9

3.1.1.3.0-10

3.1.1.4

3.1.1.4.0-1

3.1.1.4.0-2

3.1.2

3.1.2.1

3.1.2.1.0-1

3.1.2.2

3.1.2.2.0-1

3.1.2.3

3.1.2.3.1

3.1.2.3.1.0-1

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

The ACX shall by command send the same data both compressed and uncompressed if the data is capable of being compressed while in Diagnostic Mode.

Rationale: Diagnostic mode will send compressed and uncompressed data to help in validation and in assessing anomalies.

The ACX shall by command send all bits from the A to D converter while in Diagnostic Mode.

Rationale: Diagnostic mode will send all bits to help in validation and in assessing anomalies.

The ACX shall by command send dwell data (increased samples per second of a particular telemetry measurand) while in Diagnostic Mode.

Rationale: Diagnostic mode dwell data will help in validation and in assessing anomalies.

3.1.1.4 Outgassing

Reserved

The post-launch outgas period shall be no longer than 14 days.

Rationale: The ACX will sublimate and evaporate contaminants from hardware to prevent contamination from jeopardizing performance while outgassing.

3.1.2 On-Orbit Operations

3.1.2.1 Scanning Across the Sun

The ACX shall survive the presence of the sun within the Field of Regard (FOR) without sustaining any permanent degradation in performance.

Rationale: The sun must not result in damage to the instrument.

3.1.2.2 Eclipse

During eclipse season, the ACX shall meet performance requirements.

Rationale: Eclipse season is the approximately 6 week period around the equinoxes.

3.1.2.3 Operations After Maneuvers

3.1.2.3.1 Spacecraft Maneuvers

With the exception of a yaw flip, the ACX shall meet all radiometric, coverage and INR requirements within 2 minutes after the spacecraft interface has returned to being within specification following spacecraft maneuvers.

Rationale: If the spacecraft executes a different maneuver than a yaw flip, the instrument recovery will occur in this short duration after the interface is restored to nominal conditions.

Page 9 of 50 Printed Friday, August 4, 2023

ID

ACXPORD93

ACXPORD94

ACXPORD95

ACXPORD96

ACXPORD97

ACXPORD98

ACXPORD99

ACXPORD100

ACXPORD101

ACXPORD102

ACXPORD103

ACXPORD104

Object Number

3.1.2.3.2

3.1.2.3.2.0-1

3.1.2.4

3.1.2.4.0-1

3.1.2.4.0-2

3.2

3.2.1

3.2.1.1

3.2.1.1.0-1

3.2.1.1.0-2

3.2.1.1.0-3

3.2.1.1.0-4

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.1.2.3.2 Post Storage Activation

The ACX shall meet all requirements within 2 days of turn-on after post storage activation.

3.1.2.4 Detector Operating Temperatures

The ACX detector setpoint temperature shall be selectable by command to ensure radiometric performance during degradation at end of life.

Rationale: This provides for set point temperature adjustments near the operating temperature range that may be needed due to gain changes or troubleshooting.

The ACX detector temperature shall be included in telemetry to support radiometric performance assessment.

Rationale: ACX may be thermally sensitive due to its detectors and thermal telemetry will provide information for potential corrections and troubleshooting.

3.2 Normal Operational Mode Sensor Requirements

3.2.1 Coverage

3.2.1.1 Coverage Rate

Note that these coverage requirements define a capability and not a definitive operational scenario. Rather, NOAA anticipates operating ACX in an asynchronous manner that uses information from other instruments and models to identify potential regions for scanning/stepping by ACX. To perform its tasks, commanding of ACX for these targeted observations will be based on priorities and availability.

The ACX shall acquire concurrently within 1 hour:

a) Superregional_ACX or another user programmed region consistent with this coverage rate

b) Any other observations required to meet radiometric and INR requirements

Rationale: When covering the superregional ACX, the coverage including all calibrations will take 1 hour or less to ensure a timely coverage rate for the instrument that may be used to cover smaller areas in proportionally smaller times.

The ACX shall interrupt current operations by command and start the acquisition of a new frame, after a frame coordinate upload, within 30 seconds.

Rationale: The ACX must be commandable to cover regions of interest. Regions will be covered with the same instrument coverage rate, with smaller areas taking proportionally less time.

All corresponding frames in consecutive revisits shall be spaced at an average time of no more than 1 hour with peak deviation of no more than +/- 30 seconds.

Rationale: The ACX revisit of the entire region should be repeatable if commanded with a regular cadence with limited temporal deviation to support operations.

Page 10 of 50 Printed Friday, August 4, 2023

ID

ACXPORD105

ACXPORD106

ACXPORD107

ACXPORD108

ACXPORD109

ACXPORD110

ACXPORD113

ACXPORD114

ACXPORD115

ACXPORD116

ACXPORD117

Object Number

3.2.1.2

3.2.1.2.0-1

3.2.1.2.0-2

3.2.1.2.0-3

3.2.1.2.0-4

3.2.1.2.0-5

3.2.1.3

3.2.1.3.0-1

3.2.1.3.0-2

3.2.1.4

3.2.1.4.0-1

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.2.1.2 Flexible and Efficient Imaging Pattern

The ACX sensor shall observe an area of commanded size anywhere within the FOR when commanded.

Rationale: Permits flexible tasking of ACX to regions of interest.

The scan area and geographic location shall be selectable from one frame to the next.

Rationale: Permits flexible tasking of ACX to regions of interest.

The ACX shall be designed such that the Earth-scanning patterns are fully programmable on-orbit.

Rationale: Permits flexible tasking of ACX to regions of interest.

The ACX shall accept fixed grid coordinates for all imaging patterns.

Rationale: Permits mapping to fixed grid.

The ACX shall set the center location of each frame to Fixed Grid Frame coordinates specified by command.

Rationale: Permits centering on fixed grid point for ease of Fixed Grid mapping.

3.2.1.3 Simultaneity

Corresponding pixels in all spectral channels shall be calculated from detector samples that are collected within 20 seconds of each other.

Rationale: Spectrally simultaneous observations provide observations of the same features and avoid artifacts in resulting data.

All adjacent pixels shall be calculated from detector samples collected within 45 seconds of each other.

Rationale: This limits shearing in an image composed of multiple individual observations.

3.2.1.4 Data Latency

The ACX shall contribute to the total data latency for the Level 1b product of no more than 10 minutes for any coverage region.

Data latency is measured from the time the instrument acquires all samples for a scene to the time the image is available for dissemination on the ground as Level 1b data. The ACX contribution to data latency includes delay of delivery of data to the spacecraft and delay due to ground algorithm processing (i.e. INR).

Rationale: Latency between the last observation of the input data to the level 1b processing and the availability of the data for further processing should be as short as practical.

Page 11 of 50 Printed Friday, August 4, 2023

ID

ACXPORD120

ACXPORD121

ACXPORD122

ACXPORD123

Object Number

3.2.2

3.2.2.1

3.2.2.1.0-1

3.2.2.1.0-2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.2.2 Channel Definitions, SNR, Dynamic Range

3.2.2.1 Baseline

The ACX shall collect hyperspectral data in the range 0.300 – 0.500 micrometers

(um) and 0.540 – 0.740 um.

Rationale: A large number of narrow adjacent spectral samples allows for flexibility for current and future algorithm development to distinguish atmospheric species.

The ACX SNR, computed for each spectral sample, shall be greater than or equal to values in the Minimum SNR table below for the at-aperture radiance provided in the ACX Radiances file, document number, 418-XO-RPT-0075. The SNR for any wavelength not listed in the Minimum SNR Table will be determined by linear interpolation of the two nearest SNR values in the Table 1.

Rationale: These SNR values are needed to detect atmospheric radiance properties to enable higher level product generation.

Page 12 of 50 Printed Friday, August 4, 2023

ID

ACXPORD123

Object Number

3.2.2.1.0-2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

Page 13 of 50 Printed Friday, August 4, 2023

ID

ACXPORD123

ACXPORD124

ACXPORD125

ACXPORD126

ACXPORD127

ACXPORD128

Object Number

3.2.2.1.0-2

3.2.2.1.0-3

3.2.2.2

3.2.2.2.1

3.2.2.2.1.0-1

3.2.2.2.2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

Figure 1. ACX signal-to-noise ratio as a function of wavelength.

Note: The linearly interpolated SNR value of 1143 at a wavelength of 0.650 um.

All ACX channels shall have sufficient dynamic range for measurements between 0 to Nmax, which is defined as 110% albedo solar spectrum, without saturation of any detector element.

Rationale: Dynamic range of Earth scene signals need to be observed without saturation. Non-Lambertian clouds can yield more than 110% albedo response.

3.2.2.2 System Spectral Resolution

3.2.2.2.1 Spectral Response Envelope

The ACX spectral resolution shall be less than or equal to 0.0006 um, with at least three spectral samples per resolution element.

Rationale: Spectral resolution is important for retrieving molecular column density profiles used in air quality assessment.

Note: That the spectral resolution element width is the full width half maximum

(FWHM).

3.2.2.2.2 Within Channel Spectral Response Uniformity

Page 14 of 50 Printed Friday, August 4, 2023

ID

ACXPORD129

ACXPORD130

ACXPORD131

ACXPORD132

ACXPORD133

ACXPORD134

ACXPORD135

Object Number

3.2.2.2.2.0-1

3.2.2.2.3

3.2.2.2.3.0-1

3.2.3

3.2.3.1

3.2.3.1.0-1

3.2.3.1.0-2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

Any relative spectral features, excluding terrestrial features, present in the ratio of the ACX Spring Equinox reference spectrum (from ACX Radiances file) convolved with the measured spectral response across the FPA divided by the TOA irradiance (from ACX Radiances file) divided by pi, convolved with the measured spectral response shall be less than half the derived NEdN divided by TOA irradiance divided by pi.

3.2.2.2.3 Channel Center Wavelength Knowledge

The spectral sample center wavelength shall be reported to within an accuracy of 0.02nm.

Rationale: Spectral-sample center information across the FOV is needed for reliable higher-level product usage.

3.2.3 Spatial Resolution and Sampling

3.2.3.1 System Modulation Transfer Function

The spatial resolution is defined by the sensor system sinusoidal MTF. The following MTF values (exact specification is in cycles/radian) are consistent with a resolution of 5 km x 5 km equivalent area in all channels, but may have a different form factor.

The spatial frequencies, when referenced to kilometers, are measured at nadir.

The ACX system MTF shall meet the requirements in the MTF Equal Spatial Directions Requirements Table after any ground processing, in the presence of jitter and after any lossy compression/decompression.

Table 2. MTF Equal Spatial Directions Requirements Table

All Channels

Spatial Period (km/cycle)

Spatial Frequency (cycles/radian)

System MTF

40.0 900.0 0.90

20.0 1800.0 0.73

13.3 2700.0 0.53

10.0 3600.0 0.32

Page 15 of 50 Printed Friday, August 4, 2023

ID

ACXPORD136

ACXPORD137

ACXPORD138

ACXPORD139

ACXPORD140

ACXPORD141

ACXPORD142

ACXPORD143

ACXPORD144

ACXPORD145

ACXPORD146

Object Number

3.2.3.2

3.2.3.2.0-1

3.2.3.2.0-2

3.2.3.3

3.2.3.3.0-1

3.2.4

3.2.4.1

3.2.4.1.0-1

3.2.4.2

3.2.4.2.0-1

3.2.4.2.0-2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.2.3.2 Spatial Response Uniformity

Effects of co-registration and jitter may be ignored for the purposes of evaluating these requirements.

The normalized radiance difference due to spatial response differences between corresponding pixels in any two spectral channels located X (continuous variable) microradians from an edge of a 1000 by 1000 microradian or larger target with radiance equal to Nmax surrounded by a large region of radiance equal to or less than 5% Nmax shall be less than 4% of the step function for an rms over the sampling-to-edge phasing and the channel-to-channel relative phasing. The values of X include all distances between ± 1400 microradians in both directions.

Rationale: Requirement limits signal contamination from bright scene regions into dark scene regions.

3.2.3.3 Ringing from a Sharp Edge

For both the North/South and East/West edges, the ACX shall not overshoot the top of an edge or undershoot the bottom of edge by more than 2% of the height of the edge where:

a) The height and the overshoot/undershoot are measured in radiance units.

b) The edge delineates a 10% albedo region from a 90% albedo.

c) The overshoot is averaged over all phases of the detector sample grid to edge position.

Rationale: Requirement limits ringing response or overshoot near a sharp edge.

3.2.4 Image Navigation and Registration

3.2.4.1 Star Sensing

If autonomous star sensing is required to meet navigation requirements, the ACX shall have an on-board star catalog provided by the ACX contractor, which is loadable and modifiable from the ground and covers a span of two weeks.

Rationale: If employed, star sensing will require a star catalog and not rely on operators.

3.2.4.2 INR Performance Requirements

All INR requirements listed herein refer to location error of detector samples as expressed in fixed-grid angles; i.e., the requirements apply to the end-to-end system, taking all instrument, spacecraft, and ground processing effects into account. Unless otherwise specified, all INR requirements in this document are specified as North/South and East/West fixed-grid angles, in microradians, 3-sigma, and all daily hours of operation.

In the context of ACX INR, 3-sigma error is defined to be equal to the 99.73rd percentile of the absolute values of all INR error observations collected over a daily 24-hour window. When INR requirements are temporarily suspended, due to Sun/Earth geometry or maneuver outages (including recovery time), the raw errors during the requirements suspension period should be ignored.

Page 16 of 50 Printed Friday, August 4, 2023

ID

ACXPORD147

ACXPORD149

ACXPORD150

ACXPORD151

ACXPORD152

ACXPORD153

ACXPORD155

ACXPORD156

ACXPORD157

ACXPORD158

ACXPORD161

ACXPORD162

ACXPORD163

ACXPORD168

ACXPORD169

Object Number

3.2.4.2.1

3.2.4.2.1.0-1

3.2.4.2.2

3.2.4.2.2.0-1

3.2.4.2.3

3.2.4.2.3.0-1

3.2.4.2.4

3.2.4.2.4.0-1

3.2.4.2.4.0-2

3.2.5

3.2.5.1

3.2.5.1.1

3.2.5.1.1.0-1

3.2.5.2

3.2.5.2.0-1

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.2.4.2.1 Navigation

The ACX navigation error shall not exceed 53 microradians, 3-sigma, per axis.

3.2.4.2.2 Frame-to-Frame Registration

Frame-to-frame registration error shall not exceed 46 microradians, 3-sigma, per axis. Frame-to-frame registration error is the difference in navigation error for an earth location in two consecutive frames within the same channel.

3.2.4.2.3 Within Frame Registration

Within a frame in the same channel, any two pixels shall be separated by the known fixed distance to within an error of 53 microradians, 3-sigma, measured radially.

3.2.4.2.4 Channel-to-Channel Registration

Channel-to-channel registration error, or co-registration error, is the difference in line-of-sight fixed-grid angles between spectral channels for any given pixel in the same frame.

Rationale: Co-registration for Level 1b applies to true line-of-sight fixed grid angles rather than the knowledge of those angles.

Co-registration errors between any two spectral channels shall not exceed a max of 28 microradians, on a 3-sigma, per axis basis.

3.2.5 Radiometric Accuracy and Precision

3.2.5.1 Repeatability

3.2.5.1.1 Pixel-to-Pixel

For all channels, while viewing a stable, uniform calibration source over expected geostationary environmental conditions and calibration frequency, the ACX shall have a pixel-to-pixel repeatability less than the derived NEdN. Channels will be characterized as if viewing a 100% albedo calibration source.

Rationale: Pixel-to-pixel repeatability should be less than the required noise level to not interfere with scene data collection.

3.2.5.2 Coherent Noise

For all channels, while viewing a stable, uniform calibration source over expected geostationary environmental conditions and calibration frequency, the ACX shall have no spatial coherent noise spectral component exceedances. The spatial coherent noise is defined as the variation in the 2-D Fourier transform of the pixel output of a square region of 0.084 radian by 0.084 radian following all calibration, sampling and detrending. An exceedance is defined as any spatial frequency whose scaled Fourier coefficients are greater than 25 percent of the derived NEdN. The scaled Fourier coefficients are defined using the following equations to scale the amplitude to match the amplitude of a single harmonic.

Page 17 of 50 Printed Friday, August 4, 2023

ID

ACXPORD169

ACXPORD170

ACXPORD171

ACXPORD172

ACXPORD173

ACXPORD174

Object Number

3.2.5.2.0-1

3.2.5.3

3.2.5.3.0-1

3.2.5.3.0-2

3.2.5.3.0-3

3.2.5.3.0-4

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

Where x(j,l) are the radiances, N and M are the image size in pixels and Xa are the scaled Fourier coefficients. Detrending allows the removal of scene trends by subtracting the filtered scene using a square box car filter that is 10% of the minimum scene dimension. Edge effects of detrending may be reduced by using a symmetric boundary condition.

Note: The width of bin is defined by the fixed grid spacing. Channels will be characterized as if viewing a 100% albedo calibration source.

Rationale: Coherent noise in a level 1b product should be less than the one fourth of the noise level to avoid interference.

3.2.5.3 Calibration of Channels

The ACX shall have an on-board calibration capability.

Rationale: An on-board calibration capability of high quality improves near real time calibration accuracy compared to that of vicarious calibration.

The ACX shall have an on-board calibration capability for all channels that provides absolute accuracy with traceability to NIST of 3%, 1-sigma, or less in the earth albedo measurements for the scene of 100% albedo.

Rationale: Traceability to NIST (as documented in the SOW) provides improved absolute accuracy for near real time calibration.

The ACX shall have a calibration capability for all channels that provides drift in absolute calibrated radiances of no more than 2% over the ACX operational lifetime.

Rationale: Instrument degradation over the lifetime, if not corrected in processing, may be misunderstood and changing geophysical parameters over time. Degradation of the instrument and correction method(s) need to be understood and reported to the Government for use in near real time through the instrument contractor calibration algorithms (updating calibration coefficients).

The ACX shall have a calibration capability for all channels that provides RMS repeatability of 0.2% or less. This requirement is met when no fewer than N independent calibrations are performed as closely as possible together in time and the RMS variation in each calibration coefficient is less than the specified level. N is the number of calibrations required to state at the 90% confidence level that the requirement has been met.

Rationale: Short term RMS repeatability of this level ensures high quality relative accuracy calibration.

Page 18 of 50 Printed Friday, August 4, 2023

ID

ACXPORD175

ACXPORD176

ACXPORD177

ACXPORD178

ACXPORD179

ACXPORD180

ACXPORD181

ACXPORD182

ACXPORD183

ACXPORD184

ACXPORD185

ACXPORD186

Object Number

3.2.5.4

3.2.5.4.0-1

3.2.5.4.0-2

3.2.5.5

3.2.5.5.1

3.2.5.5.1.0-1

3.2.5.5.2

3.2.5.5.2.0-1

3.2.5.6

3.2.5.6.0-1

3.2.5.7

3.2.5.7.0-1

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.2.5.4 Spatial Uniformity of Data

The ACX shall have less than 0.3%, 1-sigma, change in response in the calibrated pixel data over the FOR while viewing a stable, uniform calibration source over expected geostationary environmental conditions and calibration frequency.

Channels will be characterized as if viewing a 100% albedo calibration source.

Rationale: Calibrated data needs to be spatially uniform so that variations in the data are not misinterpreted to be real signal variations.

3.2.5.5 Crosstalk

3.2.5.5.1 Channel-to-Channel

The ACX channel-to-channel (electrical, optical, spatial, spectral) crosstalk shall be less than the derived NEdN. Channel-to-channel crosstalk is defined as the change in any channel output when one channel's illumination is changed from 0.1 Nmax to a radiance of Nmax while all other channels remain illuminated at a radiance level less than 0.1 Nmax.

Rationale: Crosstalk between any spectral channels needs to be less than the noise level to minimize spectral artifacts in the data that may be misunderstood to be real features in the data.

3.2.5.5.2 Within Channel

Non-adjacent pixel to pixel within channel cross talk, not including diffraction, shall be less than the derived NEdN. Within channel crosstalk is defined as the change in any non-adjacent pixel when one pixel’s radiance is changed from 0.1 Nmax to a radiance of Nmax while all other pixels in the same band remain illuminated at a radiance level less than 0.1 Nmax.

Rationale: Crosstalk within a spectral channel needs to be less than the noise level to minimize artifacts in the data that may be misunderstood to be real features in the data.

3.2.5.6 Blooming

In all directions from the edge of a 500 by 500 microradian bright target at twice Nmax, all detector outputs in all channels shall recover to normal operation within 600 microradians.

Rationale: Specular solar glint regions are limited to within this spatial distance from the solar sub-point.

3.2.5.7 Quantization Step Size

The quantizing step size for all detector samples shall be less than half the derived NEdN.

Rationale: Signal quantization by the analog to digital converter should not be the driver in the noise budget in order to avoid having discrete jumps in signal level that can lead to digital artifacts (blocky) data.

Page 19 of 50 Printed Friday, August 4, 2023

ID

ACXPORD187

ACXPORD188

ACXPORD189

ACXPORD190

ACXPORD192

ACXPORD193

ACXPORD191

ACXPORD194

ACXPORD195

ACXPORD196

ACXPORD197

ACXPORD198

ACXPORD199

ACXPORD200

ACXPORD201

Object Number

3.2.5.8

3.2.5.9

3.2.5.9.1

3.2.5.9.1.0-1

3.2.6

3.2.6.0-1

3.2.6.0-2

3.2.7

3.2.7.0-1

3.2.7.0-2

3.2.7.1

3.2.7.1.0-1

3.2.7.2

3.2.7.2.0-1

3.2.7.2.0-2

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.2.5.8 Reserved

3.2.5.9 Polarization

3.2.5.9.1 Polarization Control

All channels shall have less than 5% polarization sensitivity to the incoming light at all Earth-viewing angles.

Rationale: Polarization sensitivity should be small to limit signal variations with angle.

3.2.6 System Linearity

The ACX shall have linear radiometric response, before calibration, such that all points within the dynamic range vary from a linear best fit by no more than 1% of Nmax.

Rationale: Detectors may not be perfectly linear, but small deviations can be well corrected.

The ACX measured error over the dynamic range in radiometric response as a function of input radiance shall be less than or equal to 0.5% of the radiometric response.

3.2.7 Data Compression

If needed, the ACX shall perform data compression on all data.

Rationale: Data rates may be excessive for downlink without compression.

The ACX may perform lossy data compression.

Rationale: Constraint on application is not to degrade data beyond performance levels

3.2.7.1 Lossless Data Compression

Lossless data compression shall be in accordance with Applicable Document 1 and Applicable Document 2.

Rationale: Lossless data compression when used will follow these references.

3.2.7.2 Lossy Compression

If performed, lossy compression shall not prevent the ACX from meeting requirements, most notably MTF, SNR, and coherent noise.

Rationale: Calibration data needs to be of a high quality so nominally it should not be compressed as it may impact performance. Reference documents provide additional information on data compression

All calibration data shall be lossless compressed or uncompressed.

Page 20 of 50 Printed Friday, August 4, 2023

ID

ACXPORD204

ACXPORD205

ACXPORD206

ACXPORD207

ACXPORD208

ACXPORD209

ACXPORD210

ACXPORD211

Object Number

3.2.7.3

3.2.7.3.0-1

3.2.7.3.0-2

3.2.7.3.0-3

3.2.7.3.0-4

3.2.7.3.0-5

3.2.7.4

3.2.7.4.0-1

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

3.2.7.3 Vizualization Algorithm

The ACX Visualization Algorithm (VA) shall provide for visualization of radiances at each spectral channel.

The VA may utilize spatial and spectral resampling as needed.

The VA shall create spatially uniform output on the fixed grid of less than or equal to 140 microradians by less than or equal to 140 microradians that also complies with ACXPORD151 (frame-to-frame navigation) and ACXPORD153 (within-frame registration).

The VA shall create spectrally uniform output images of all spectral channels over full-width-half-maximum spectral widths.

For the VA algorithm output, the performance against ACXPORD129 (within-channel spectral response uniformity) shall be less than 2x the derived noise for all channels.

Rationale: The VA enhances Level 1b data to produce images that are spatially and spectrally uniform.

3.2.7.4 Stray Light

ACX stray light shall be less than the derived NEdN over the spectral range for the 110% Albedo radiances provided in the ACX Radiances file.

Page 21 of 50 Printed Friday, August 4, 2023

ID

ACXPORD1000

ACXPORD1001

ACXPORD1002

ACXPORD1003

ACXPORD1004

ACXPORD1005

ACXPORD1006

ACXPORD1007

ACXPORD1008

ACXPORD1009

ACXPORD1010

ACXPORD1011

ACXPORD1012

ACXPORD1013

ACXPORD1015

ACXPORD1016

ACXPORD1017

ACXPORD1018

ACXPORD1019

Object Number

4.1

4.1.0-1

4.1.0-2

4.1.0-3

4.1.0-4

4.1.0-5

4.1.0-6

4.2

4.2.1

4.2.1.0-1

4.2.2

4.2.2.0-1

4.2.3

4.3

4.3.0-1

4.3.0-2

4.3.1

4.3.1.0-1

418-XO-ACXPORD-0121, RM Version, Geostationary eXtended

4 Design Requirements

4.1 Reliability

The ACX shall demonstrate by analysis a Reliability (R) of at least 0.6 after 10 years of on-orbit operations, preceded by ground storage, and up to 5 years of on-orbit storage.

Rationale: The design life of at least 10 years extends from commencement of on-orbit operations until Reliability falls to 0.6.

The ACX shall demonstrate by analysis a Mean Mission Duration (MMD) of at least

8.4 years by integrating under the Reliability curve for 10 years of on-orbit operations, preceded by the storage periods.

No credible single-point failure in ACX flight heater components shall permanently preclude the Instrument from supporting the mission.

No credible single-point failure in ACX flight temperature-sensing components shall permanently preclude the Instrument from supporting the mission.

To satisfy the Reliability and Design Life Requirements, the Instrument may choose selectively redundant approaches beyond those explicitly required in ACXPORD1004 and ACXPORD1005.

The ACX shall…