Research Article
Experimental and Computational Modal Analyses for Launch Vehicle Models considering Liquid Propellant and Flange Joints
Table 2
Weights of the components for a test model.
| Oxidizer tank | 2350 g | Center body | 1101 g | Fuel tank | 1763 g | Nuts (48 ea.) | 50.4 g | Washers (96 ea.) | 29.8 g | Bolts (48 ea.) | 221.8 g | Elastic ropes (4 ea.) | 9.2 g | S-shaped rings (8 ea.) | 62.4 g | Total weight | 5600 g |
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