ENCLOSURE_L.2_-_COMPLIANCE_MATRIX.pdf

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Attached to
Plankton, Aerosol, Cloud, ocean Ecosystem (PACE) Solar Array Panels Federal contract opportunity
Solicitation number
80GSFC19R0003
Issued by
National Aeronautics and Space Administration Goddard Space Center

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Enclosure L.2 - Compliance Matrix

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PACE Solar Array Spec Compliance Matrix

Section Requirement TM Req. Compliant

(C)/Non-

Compliant

(NC)

2.0 Applicable Documents

4.0 Functional Performance

Requirements

4.1.1.1 Flight Panels x

4.1.1.2 Qualification Coupons x

4.1.2 Power at Highest Predicted

Operating Temperature x

4.1.3 Power at Highest Predicted

Temperature

4.1.4 End-of-Life Power x

4.1.5.1 Solar Cell Mechanical x

4.1.5.2a Solar Cell Layout x

4.1.5.3 Solar Cell Power x

4.1.5.4 Limit to Solar Cell Shadowing x

4.1.6.1 Cover Material and Thickness x

4.1.6.2 Cover Orientation x

4.1.6.3 Antireflective/ Indium-Tin-Oxide

Coating (AR/ITO)

4.1.7 Blocking Diodes and Terminal

Boards

4.1.8 Wire and Wire Layout x

4.1.8.1 Coarse Sun Sensor (CSS) Wiring x

4.1.8.2 Hinge Damper Heater Wiring x

4.1.8.3 Monitor Solar Cell x

4.1.9 Connector Wiring and Connector

Type

4.1.10 Platinum Resistor Thermometers

(PRTs)

4.1.11 Insulated Substrate x

4.1.11.1 Substrate Insulation Resistance x

4.1.11.2 Substrate Grounding x

4.1.12 Panel Performance in Thermal

Vacuum Environment

4.1.13 Panel Performance in

Depressurization Environment

4.1.14 Allowable Degradation Due to

Charged Particle Radiation

4.1.15 Allowable Degradation Due to

Humidity

4.2.1 Mass Allocation x

4.3.1 Solar Array Panels Power Wire

Redundancy

4.4.1 Primary Power DC Isolation

4.4.2 Mechanical Contact Resistance

4.4.3 Connector DC Resistance

4.5.2.1 Platinum Resistor Thermometer

(PRT)

4.5.2.2 PRT Performance

5.1 Interface Documentation

5.3 Physical Envelope x

6.0 Environmental Requirements

6.8.1 Operating Pressure Range

6.10 Ground Environments x

6.11.1 Flight Interface Design Temperature

Limits

6.12 Charged Particle Radiation

6.12.2.1 Minimum TID Tolerance for EEE

Parts

6.12.5 Charging Environment x

6.13 Atomic Oxygen Fluence

6.13.1 Atomic Oxygen Analysis

6.13.2 Atomic Oxygen Testing

7.1.1.1 Particulate Contamination x

7.1.1.2 Molecular Contamination x

7.1.2.1 Particulate Generation x

7.1.2.2 Molecular Generation x

7.2.1 Conductive Surface Ground Path x

7.2.2 Conductive Surface Resistivity x

7.2.3 Exposed Harness Specific

7.3 Magnetic Cleanliness x

8.1.1 EEE Parts x

8.1.2 Materials x

8.1.2.1 Material Conductivity x

8.1.2.2 Material Limitations for Debris

Casualty Area

8.2.1 Test Sensors

8.2.2 Interface Requirements x

8.2.3 Mitigation of Internal Charging x

8.3 Safety x

8.5 Identification and Marking

8.6.1 Workmanship Standards

8.6.2 Connectors x

8.7.1 Mission Life x

8.8.1 Ground Support Equipment (GSE)

Design

8.8.7 GSE Cleanliness

8.8.8 GSE Bakeout

8.8.9 Test Harness

9.0 Mechanical Design Requirements

NASA-STD-5020

10.2 Ground Support Equipment x

10.3 Transportation Equipment x

11.0 Verification Requirements x

11.2 Inspection Requirements x

11.4 Test Requirements

11.5 Required Tests x

11.5.10 Thermal Vacuum Bakeout x

11.5.11 Thermal Vacuum Test x

11.5.16 Solar Cell and Bypass Diode

Qualification Tests

11.5.17 Solar Array Panel Qualification Tests x

11.5.18 Flight Solar Array Panel Tests x

11.5.19 Test Condition Power Verification x

11.5.20 Bypass Diode Functionality

Verification

11.5.21 Substrate Insulation Resistance

11.5.22 Solar Cell Mechanical Verification x

11.5.23 Cover Orientation Verification x

11.5.24 Cover Grounding Verification x

11.5.25 Flight Connector Type Verification x

11.5.26 Platinum Resistance Thermometer

Type Verification

11.5.27 PRT Performance Verification

11.5.28 Parts and Assembly Layout

11.5.29 Mission Life Verification

11.5.30 Shelf Life Verification

11.5.31 Substrate Ground Verification

11.5.32 Cleanliness Verification x

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