1g - T3TRK Cost and Software Data Reporting (CSDR) Plan.xls

DD Form 2794, Pg 1 (METADATA)

PLEASE DO NOT RETURN YOUR COMPLETED FORM TO THE ABOVE ORGANIZATION.

DD Form 2794, Pg 2 (REPORTING)

MAINT. &

REPAIR

PARTS

QUANTITY

DD Form 2794, Pg 3 (EVENTS)

DD Form 2794, Pg 4 (REMARKS)

Requirements definition, engineering design & analysis;

Manufacturing tooling, fixtures and procedures;

Development units (breadboard, engineering, qual), including parts and materials;

Handling and test support equipment, simulators;

Development, qualification and life testing;

Development and production test procedures;

Engineering support for development unit fabrication, assembly & tests;

Redesign, rework and retest to correct design flaws;

Maintenance of tooling and unit test equipment until first launch

ii. Recurring Cost:

Hardware production units (proto-flight, flight, spare);

Production unit parts & materials, assembly and testing;

Setup for fabrication, assembly and test;

Engineering support for production unit fabrication, assembly & tests;

Spare parts, materials and subassemblies for production units;

Rework and retest due to workmanship problems;

Maintenance of designs and production procedures;

Maintenance of tooling and unit test equipment after first launch;

Refurbishment (of both qual and proto-flight units)

Development of delivered operational S/W;

Software test procedures;

Software configuration management, quality assurance & documentation;

Support for/conduct of first-time software I&T with hardware and subsequent higher level I&T;

Test, development support and space vehicle production support S/W: develop. and maint. up to 1st launch;

Commercial S/W licenses for development facilities and ground station development support;

Fixing deficiencies and developing enhancements in Ground and flight software from installation up to IOC

ii. Recurring Cost:

Installation and check-out of developed S/W in ground stations;

If first-time S/W I&T is performed at ground station, then it is NRE;

Maintenance of S/C production & test support S/W after first launch;

Acquisition of stand-alone and bundled COTS S/W in operational system;

Maintenance of flight S/W (usually embedded in acquisition contracts)

Requirements definition, allocation and flow-down;

Specifications and ICDs - initial development & maintenance until all TBDs and TBRs are removed;

Top level design trade-offs and system definition;

Analyses and simulations of system performance and effectiveness, mission assurance, reliability,availability, maintainability, survivability, security, safety, EMI/EMC, radiation, survivability, contamination control, human engineering, autonomy and fault management;

Operations concept development;

Technical direction and configuration control during development;

Risk management though CDR;

Mass, power, link margin & reliability budgets -- initial development & maintenance until design complete;

Processing time & memory budgets;

Development, production, verification, risk management, training and security plans;

Parts, materials and processes - establishing procedures, etc.;

Product assurance development tasks;

Requirements verification through design completion, including demonstrations and IV&V;

Technical change management (RFIs, ECPs, etc.) -- NR tasks supporting changes, handling nonrecurring-only changes;

Design Integration -- mechanical, electrical, thermal, facilities;

Functional and physical configuration audit (FCA/PCA) support;

System documentation

ii. Recurring Cost:

Maintenance of specs, ICDs, plans & budgets -- after all TBDs and TBRs are removed;

Performance, S/W maintenance productivity metrics;

Analysis updates;

System configuration control after design completion;

Mass, power, link margin & reliability budgets - supporting production;

Support for production testing, rehearsals and operational test and evaluation;

Product assurance;

Requirements verification after design completion;

Launch readiness reviews, support for product acceptance;

Technical change management (RFIs, ECPs, etc.) -- supporting recurring portions of changes and recurring- only changes

Development, qualification and life testing - all levels and system segments;

Development and acceptance test plans and procedures;

Development, qualification and life test analysis and reports;

I&T for correcting software problems prior to IOC

ii. Recurring Cost:

Space vehicle assembly, integration and acceptance testing;

Acceptance test analysis and reports;

Integration and test of previously-developed software -in GOPCs, GEPs

Management activities applied to/associated with NRE efforts - top level program management, project control and planning, business/financial mgmt, subcontract mgmt, product effectiveness, computer support;

Procedures and infrastructure establishment - Cost accounting, configuration & data management, parts & material acquisition, security, facilities

ii. Recurring Cost:

Management activities applied to/associated with REC efforts

Concept of operations and maintenance development;

Operations & maintenance procedure development;

Development of training materials, simulators and aids;

Initial ILS analysis and data;

Upgrades/changes to above associated with: Major redesigns, capability increments Recapitalization, operating system changes

ii. Recurring Cost:

System operation costs - operations, training, systems engineering & management staff;

Hardware maintenance & recapitalization;

Software maintenance - including COTS license costs;

Software modifications/fixes after IOC;

Reproduction and updating of technical data and manuals;

Procurement/production of hardware spares;

Rehearsals and initialization of space vehicles

These elements contain all the resources related to the pre-operations (Pre-Ops) maintenance (software updates) of Software. This function begins with the acceptance of the Software elements and ends with the start of Operations.

ii. Pre-Operations Mission Support:

These elements include all the resources required for the operation of the Space or Ground system prior to turn-over. Includes, for example:

a. On-orbit testing; routine monitoring of Space or Ground system equipment health and status

b. Fault detection

c. Anomaly investigation and resolution. (The Mission Support period typically begins after installation and a specified time prior to launch and ends when the Space Vehicle achieves initial operational capability.)

DD FORM 2794 (PAGE 4), REMARKS, MAY 2024 PREVIOUS EDITION IS OBSOLETE

DD Form 2794, Pg 5 (SCOPE DEF)

(X if applicable)

DD FORM 2794 (PAGE 5), INTRA-CONTRACT SCOPE, MAY 2024

DD Form 2794, Pg 9a (TECH RQTS)