Documentation, Customer-provided documentation, Payload questionnaire – Orbital Minotaur VI User Manual
Page 84: Icd inputs, Payload mass properties, Payload finite element model
This manual is related to the following products:
See also other documents in the category Orbital Equipment:
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- Minotaur I (99 pages)
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- GEOStar-3 Bus (2 pages)
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- 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)