Exhibit 2 - L10 Spacecraft and Observatory Environmental Testing Matrix Fill-in.pdf

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Attached to
Landsat 10 Spacecraft _ DRAFT RFP
Solicitation number
80GSFC26D0015
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This document is an Engineering Test Matrix (ETM) specification for the L10 spacecraft program, detailing comprehensive testing requirements across multiple hardware categories and subsystems.

The ETM establishes testing protocols organized into four primary categories: Hardware (Structural/Mechanical, EMI/EMC, and Thermal), Mechanisms, Boxes/Components, and Deployable Systems. The matrix specifies test levels using standardized codes including Q (Qualification), PF (Proto-flight), AT (Acceptance), QS (Qualification by Similarity), M (Measured Results), T (Planned Test), LT (Life Test), AN (Analysis), TT (Time and Temperature Bakeout), QCM (Bakeout with QCM), DP (Deployment), HC (Hot/Cold Functional), and PQ (Proto-Qualification). Testing categories encompass structural and mechanical evaluations (mass survey, static load, sine burst, vibration, acoustics, mechanical shock, pressure profile, mechanical function, deployment, torque, life test, and mass properties); electrical assessments (inrush, power quality/profile, RF self-compatibility); and thermal analysis (thermal vacuum cycles, thermal cycles, thermal balance, and bakeout). The specification applies to various hardware tiers including Observatory First Article, SC Bus First Article, Primary Structure First Article, and Modular Propulsion System, with differentiation between First Article and Subsequent configurations. The L10 ETM – Propulsion sheet extends these requirements specifically to propulsion subsystems with detailed test specifications for engines, tanks, filters, valves, regulators, transducers, and related components, color-coded by test category to facilitate identification of requirements across the development and qualification phases.

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Exhibit 6 - L10 Past Performance Questionnaire R.pdf PDF
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Attachment K - L10 Space Environmental Req Document (LSERD).pdf PDF
Attachment L - L10 Analytical Math Model Definitions (LAMMD) Rev.pdf PDF
Attachment M - L10 Spacecraft Government Furnished Equipment Information List (SC GFEGFI).pdf PDF
Attachment N - L10 World Reference System - 3 Definition Rev.pdf PDF
Attachment Q - LandIS Simplified Mechanical Interface Control Drawing (MICD).pdf PDF
Attachment S - L10 Time and Materials Rate Matrices Rev.pdf PDF
Attachment V - L10 C-SCRM Plan.pdf PDF
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Enclosure 4 - L10 Geometric Error Budget (GEB).pdf PDF
Exhibit 1 - L10 Pricing Template.xlsx XLSX spreadsheet
Exhibit 4 - L10 Gate Criteria Fill In R.pdf PDF
Attachment E - L10 Spacecraft to Ground Interface Req Document (SC to GND IRD) Rev.pdf PDF
Attachment G - L10 Spacecraft Simulator Req Document (SC Sim RD).pdf PDF
Attachment H - L10 Spacecraft Deliverable Items List (DIL).pdf PDF
Attachment J - L10 Radiation Environments Description (LRED) Rev.pdf PDF
Attachment R - L10 Spacecraft Contractor Standards.pdf PDF
Attachment U - L10 OCI Plan Rev.pdf PDF
Attachment W - Small Business Subcontracting Plan.pdf PDF
Attachment X - Non-Technical Contract Data Requirements List.pdf PDF
Attachment X DRD 1 - OCI Plan.pdf PDF
Attachment X DRD 2 - Security Requirements for Unclassified IT Resources DRD C-SCRM requirements.pdf PDF
Attachment X DRD 5 - CAIRIA DRD.pdf PDF
Enclosure 2 - L10 Observatory Quality Assurance Surveillance Plan.pdf PDF
Enclosure 3 - L10 Design Reference Case - DRC-18.pdf PDF
Enclosure 3 - L10 Design Reference Case - DRC-18 Definition.pdf PDF
Enclosure 5 - Geometric Budget (GEB) Support Presentation.pdf PDF
Attachment A - L10 Statement of Work (SOW).pdf PDF
Attachment D - L10 Spacecraft Interface Requirements Document (SCIRD).pdf PDF
Attachment F - L10 Observatory Environment Req Document (ObsERD)R.pdf PDF
Attachment O - L10 Lexicon.pdf PDF
Attachment P - L10 Acronym List.pdf PDF
Attachment T - L10 Major Payment Events Payment Schedule and Completion Criteria.pdf PDF
Attachment X DRD 4 - CITAR Report Template.xlsx XLSX spreadsheet
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Attachment B - L10 SC CDRL and DID Rev.pdf PDF
Attachment C - L10 Spacecraft Requirements Document (SC SRD).pdf PDF
Attachment I - L10 Payload to Launch Services Interface Description Doc (LS IDD) Rev.pdf PDF
Attachment X DRD 2 - NASA C-SCRM Plan Questionnaire.xlsx XLSX spreadsheet
Attachment X DRD 4 - CITAR DRD updated.pdf PDF
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Exhibit 3 - L10 Spacecraft Master Equipment List (MEL) Fill In.pdf PDF
Exhibit 5 - L10 Spacecraft Specifications Fill-in.pdf PDF
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L10 Item Unit Type Supplier Mass Modal Survey

Static Load, Sine

Burst

Sine Vibration

Random Vibration Acoustics Mechanical

Shock Pressure Profile

Mechanical Funtction

Deploymen t Torque Life Test Mass

Properties Mechanical Comments CE101 CE102 / CE103 CMBCE Inrush

Power Quality / Profile

RF Self Compatibili ty

CS101 CS114 RE102

(unit)

Agrgregate

RE

(system)

RS103

(unit)

Aggregrate

RS

(system) CE106 CS103 CS104 Electrical Comments

Thermal Vacuum (Cylces)

Thermal Cycle

(Cycles)

Thermal Balance Bakeout Thermal Comments

Observatory First Article

SC Bus First Article

Primary Structure First Article

Modular Prop System* First Article

First Article

Subsequent

First Article

Subsequent

First Article

Subsequent

Legend Description

Q Qualification Test Levels

PF Proto-flight Test Levels

AT

Acceptance Test Levels (or workmanship)

P/A Proto-flight Test Levels or Acceptance based on design

QS Qual by Similarity

M Test with measured results (mass, grounding, etc.)

T Planned test where Q, PF, or AT do not apply

LT Life Test (Life duration) AN Analysis

TT Time and Temp Bakeout

QCM Bakeout with QCM

DP

Deployment, Full deploy / Pop & Catch / First motion, g-negated

HC

Hot / Cold functional tests. Usually @ ambient pressure

PQ Proto-Qualification Test

Mechanisms

Boxes / Components

Deployable Systems (if tested as as such)

ThermalHardware Structural/Mechancial EMI/EMC

L10 ETM - General

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