System and subsystem CDRs Clause Samples
System and subsystem CDRs. The following shall be supplied as applicable:
1. Program Organization and management description update;
2. Program Master Schedule including identification of critical path items, availability of facilities and resources, and any potential problem area;
3. Updated design and test specifications with supporting compliance analysis;
4. Interface control drawings;
5. Summary of functional, performance, interface and environmental requirements and performance compliance matrix;
6. Summary description of S/C system and/or subsystems:
a. Results and summary description of satellite system subsystem or units design analyses,
b. subsystem and units design summaries
c. functional and circuit schematics and logic diagrams;
d. layout and assembly drawings;
e. Mass, power, pointing and fuel budgets;
f. Results of failure mode, effects and criticality analysis (FMECA), where applicable, and updates to single point failure identification;
g. Results of system/subsystem reliability analysis;
h. Updates to design limitations and environmental considerations (thermal, ESD, EMC, EMI, radiation, power handling, multipaction, PIM, etc.);
i. Available measured performance; j. Degradation and wear-out considerations;
7. Analyses data, including:
a. Mathematical model and numerical predictions,
b. All design and analysis numerical predictions compared to contractual requirements, and
c. All design and analysis documents related to the design of the control laws of the Attitude and Control subsystem (ACS and System CDRs only);
8. Identification of critical parts, devices, processes and materials;
9. System and/or subsystem test plan, supporting documentation and compliance with contractual requirements, including launch site tests;
10. Flight and ground support software (as applicable);
11. Preliminary version of the mission sequence of events and contingency plan (system CDR only);
12. Preliminary mission operations plan (system CDR only);
13. System safety and hazard assessment (system CDR only);
14. Launch vehicle interface requirements and compatibility analyses (system CDR only);
15. Telemetry and command date bases (system CDR only);
16. Categorization lists (system CDR only); and
17. Steerable antenna pointing algorithm including the pointing determination, command database and pointing validation test plan.
18. ADTM pointing parameters and algorithm.
19. RVTD (at System CDR only). 20. Custom Devices list (System CDR only).