Orbital Antares User Manual
Page 9
Antares
®
OSP-3
User’s Guide
Table of Contents
Release 1.1
July 2013
ix
Figure 8.6-1. The Orbital Team Has Extensive Experience in a Payload Processing Clean Room
Environment ................................................................................................................................................ 67
Figure 8.7-1. Antares Secure FTS System Block Diagram ....................................................................... 68
Figure 8.8-1. TDRSS 20W LCT2 Transmitter and UB S-Band Antenna ................................................... 69
Figure 8.8-2. TDRSS Notional Telemetry Flow.......................................................................................... 69
Figure 8.9-1. Antares Bi-Propellant Third Stage ........................................................................................ 70
Figure 8.10-1. Omni-Flex Isolators Are Easily Integrated Between the Payload and the Payload
Separation System (Minotaur I Installation Shown) ................................................................................... 70
Figure 8.10-2. Use of Soft Ride Significantly Attenuates Peak LV Dynamic Environments ...................... 71
Figure 8.13-1. Antares LV Enhanced Performance Options ..................................................................... 72
Figure 8.14-1. Antares 120 Enhanced Fairing Dynamic Envelope ............................................................ 73
Figure 8.15-1. Typical Propellant Loading Schematic ............................................................................... 74
Figure 8.19-1. Layout of the Antares Facilities at KLC .............................................................................. 75
LIST OF TABLES
PAGE
Table 2.2-1. Antares Numbering Conventions ............................................................................................. 3
Table 3.6-1. Antares Payload Deployment Pointing and Rate Accuracies ................................................ 19
Table 4.1-1. Design Limited Load Factors ................................................................................................. 21
Table 4.1.1-1. Typical Antares 120 Ground and Flight Acceleration Loads at the Payload Interface ....... 21
Table 4.1.1-2. Phasing of Dynamic Loading Events .................................................................................. 22
Table 4.7-1. Launch Vehicle RF Emitters and Receivers .......................................................................... 31
Table 5.4.2-1. Payload Mass Properties Measurement Tolerance ........................................................... 38
Table 6.3.1-1. Overview of Typical Mission Integration Working Group Flow .......................................... 45
LIST OF APPENDICES
PAGE
APPENDIX A. PAYLOAD QUESTIONNAIRE...........................................................................................A-1