Orbital Antares - Manual (Page 8)

Antares
®
OSP-3
User’s Guide
Table of Contents
Release 1.1 July 2013 viii
Figure 3.3-6. Antares 122 and 132 High Energy Performance from WFF ................................................ 14
Figure 3.4-1. Antares Fleet Launch Capabilities from KLC ....................................................................... 15
Figure 3.4-2. Antares 120 Launch Capabilities from KLC ......................................................................... 16
Figure 3.4-3. Antares 121 Launch Capabilities from KLC ......................................................................... 16
Figure 3.4-4. Antares 130 Launch Capabilities from KLC ......................................................................... 17
Figure 3.4-5. Antares 131 Launch Capabilities from KLC ......................................................................... 17
Figure 3.4-6. Antares 122 and 132 Critically Inclined Elliptical Launch Capabilities ................................. 18
Figure 4.1.2-1. Nominal Payload Acceleration as a Function of Mass (Antares 120) ............................... 23
Figure 4.1.2-2. Nominal Payload Acceleration as a Function of Mass (Antares 121) ............................... 23
Figure 4.1.2-3. Nominal Payload Acceleration as a Function of Mass (Antares 122) ............................... 24
Figure 4.1.2-4. Nominal Payload Acceleration as a Function of Mass (Antares 130) ............................... 24
Figure 4.1.2-5. Nominal Payload Acceleration as a Function of Mass (Antares 131) ............................... 25
Figure 4.2-1. Antares Fairing Internal Maximum Flight Level Payload Acoustic Environment .................. 26
Figure 4.2.2-1. Antares Payload Interface Sine Vibration Levels .............................................................. 27
Figure 4.3-1. Antares Payload Maximum Flight Level Shock at the Base of the Payload ........................ 28
Figure 4.6-1. Antares Fairing Internal Pressure Profile ............................................................................. 30
Figure 5.1.1-1. Antares Fairing Dynamic Payload Envelope with 1575 mm Mechanical Interface ........... 33
Figure 5.1.2-1. Antares Fairing Standard Access Door Location .............................................................. 34
Figure 5.2.1-1. Antares 1575 mm (62 in.) Non-Separating Payload Mechanical Interface ....................... 35
Figure 5.3-1. Antares Electrical Interface Block Diagram .......................................................................... 36
Figure 6.1-1. Mission Integration Team ..................................................................................................... 40
Figure 6.1-2. Antares Program Structure ................................................................................................... 41
Figure 6.1.2-1. Orbital Mission Responsibilities ......................................................................................... 42
Figure 6.2-1. Antares Mission Cycle .......................................................................................................... 44
Figure 7.2-1. Antares HIF at WFF .............................................................................................................. 52
Figure 7.2.1.1-1. Transporter-Erector-Launcher (TEL) .............................................................................. 52
Figure 7.2.1.2-1. Portable Environmental Control System (PECS) .......................................................... 53
Figure 7.2.2.1-1. WFF Launch Pad 0A ...................................................................................................... 54
Figure 7.2.2.2-1. WFF Launch Control Center ........................................................................................... 54
Figure 7.2.2.3-1. WFF Mission/Range Control Center .............................................................................. 55
Figure 7.3-1. Flow of Antares Hardware to the Launch Site ...................................................................... 56
Figure 7.5.3-1. Antares Launch from WFF ................................................................................................ 59
Figure 8.1.1-1. 937S Separation System ................................................................................................... 60
Figure 8.1.1-2. Antares 937S Payload Dynamic Envelope ........................................................................ 61
Figure 8.1.2-1. 1194VS Separation System .............................................................................................. 62
Figure 8.1.3-1. 1666VS Separation System .............................................................................................. 64
Figure 8.1.3-2. Antares 1666VS Payload Dynamic Envelope ................................................................... 65