Orbital Antares User Manual
Page 22
Antares
®
OSP-3
User’s Guide
Section 3.0
– Performance
Release 1.1
July 2013
11
3.3. General Performance from WFF
Antares general performance for circular orbits of various configurations, altitudes, and inclinations is pro-
vided in Figures 3.3-1 through 3.3-5 for launches from WFF.
Figure 3.3-1. Antares Fleet Launch Capabilities from WFF
See also other documents in the category Orbital Equipment:
- GMD Boost Vehicle (2 pages)
- GQM-163A Coyote (2 pages)
- Minotaur I (99 pages)
- Minotaur I (2 pages)
- Minotaur VI (2 pages)
- Minotaur IV (121 pages)
- Minotaur V (2 pages)
- Minotaur IV (2 pages)
- Minotaur-C (2 pages)
- Pegasus (2 pages)
- Pegasus (92 pages)
- Antares (2 pages)
- GEOStar-2 Bus (4 pages)
- GEOStar-3 Bus (2 pages)
- GEOStar Hosted Payloads (2 pages)
- SMF – Virginia (2 pages)
- SMF – Arizona (2 pages)
- LEOStar-3 Bus (4 pages)
- LEOStar-2 Bus (4 pages)
- Iridium NEXT (2 pages)
- Hingelock TEE Deployer Model 358 (2 pages)
- Hingelock TEE Deployer Model 5E9 (2 pages)
- Hingelock TEE Deployer Model 621 (2 pages)
- Hingelock TEE Deployer Model 625 (2 pages)
- Hingelock TEE Deployer Model 9843 (2 pages)
- Hingelock TEE Deployer Model T126 (2 pages)
- Overlap Dual-TEE Model 225 (2 pages)
- Overlap TEE Self-Deployer Model 1/2 OL-SD (2 pages)
- Overlap TEE Deployer Model 214 (2 pages)
- Wire Antenna Deployment Assembly Model 499 (2 pages)
- Wire Antenna Deployment Assembly Model 9842 (2 pages)
- Deep Space 1 (2 pages)
- Dawn (2 pages)
- RHESSI (2 pages)
- SORCE (2 pages)
- IBEX (2 pages)
- Coriolis (2 pages)
- FORMOSAT-3/COSMIC (2 pages)
- AIM (2 pages)
- Glory (2 pages)
- Landsat 8 (2 pages)
- OCO-2 (2 pages)
- ICESat-2 (2 pages)
- ICON (2 pages)