Orbital Pegasus - Manual (Page 6)

Release 7.0 Apr 2010 vi
Pegasus User’s Guide
TABLE OF CONTENTS (CONTINUED)
PAGE
8.3.1. Trajectory Analysis .................................................................................................................. 54
8.3.2. Guidance, Navigation, and Control Analyses.......................................................................... 54
8.3.3. Coupled Loads Analysis .......................................................................................................... 55
8.3.4. Payload Separation Analysis................................................................................................... 55
8.3.5. RF Link and Compatibility Analyses........................................................................................ 55
8.3.6. Mass Properties Analysis and Mass Data Maintenance ......................................................... 55
8.3.7. Power System Analysis ........................................................................................................... 55
8.3.8. Fairing Analyses ...................................................................................................................... 55
8.3.9. Mission-Unique Software......................................................................................................... 55
8.3.10. Post-Launch Analysis .............................................................................................................. 56
8.4. Interface Design and Configuration Control ................................................................................. 56
8.5. Mission Planning Schedule .......................................................................................................... 56
8.6. Payload Documentation Support.................................................................................................. 56
9. SHARED LAUNCH ACCOMMODATIONS .......................................................................................... 56
9.1. Load-Bearing Spacecraft.............................................................................................................. 56
9.2. Non-Load-Bearing Spacecraft...................................................................................................... 57
10. NONSTANDARD SERVICES............................................................................................................... 58
10.1. Alternative Integration Sites ......................................................................................................... 58
10.2. Alternative Launch Sites............................................................................................................... 59
10.3. Downrange Telemetry Support .................................................................................................... 59
10.4. Additional Fairing Access Doors .................................................................................................. 59
10.5. Optional Payload/Vehicle Integration Environment...................................................................... 60
10.6. Enhanced Fairing Environment .................................................................................................... 60
10.7. Enhanced Fairing Internal Surface Cleaning ............................................................................... 60
10.8. Hydrocarbon Monitoring ............................................................................................................... 60
10.9. Instrument Purge System............................................................................................................. 60
10.10. Increased Capacity Payload-to-GSE Interface ............................................................................ 61
10.11. Improved Insertion Accuracy Options .......................................................................................... 61
10.12. Load Isolation System .................................................................................................................. 63
10.13. Low Tip-Off Rate with Reduced Clamp Band Tension................................................................. 63
10.14. Enhanced Telemetry Capabilities – Payload Data....................................................................... 63
10.15. State Vector Transmission From Pegasus................................................................................... 63
10.16. Payload Electrical Connector Covers........................................................................................... 64
10.17. Payload Fit Check Support........................................................................................................... 64
10.18. Payload Propellant Loading ......................................................................................................... 64