Bus Performance Data Sample Clauses

Bus Performance Data. The following shall be included: 1. Data lists of the power consumption of all spacecraft units for expected unit temperatures, voltages and RF drive levels (if applicable). The unit power data shall also indicate the power bus which supplies the power to the specific unit. 2. All unit alignment data including principal axis misalignments, actuator and sensor alignments, and as shipped sequenced mass properties. (NOTE: Final sequenced mass properties must be provided from the launch site no later than 7 days before the scheduled launch.) 3. Spacecraft appendage flexible modal frequencies. 4. Earth Sensor torsion bar resonant frequencies (if applicable). 5. Ground tested gyro drift rates (if applicable). 6. Predicted disturbance torques during liquid apogee engine firing. 7. Solar pressure disturbances during in-orbit operations. 8. Spacecraft configuration including serial numbers of all units of that spacecraft. 9. Actual thruster performance data including thrust levels, specific impulses, etc.