offering the possibility of evenly dispersing vibration dampening control adaptively. [7] Structural system perturbations resulting from thermal expansion of the structural members could pose problems in a structure as expansive as this configuration, which has a maximum blade length of 228 m (748 ft). Other perturbations are solar pressure, drag, gravity gradients, magnetic torque, albedo, Earth radiation, and astronaut motion. These topics will be the issues of continuing research on this design and concept. CONCLUSION As is evident from this paper, the architectural perspective gave rise to different criteria and ordering thereof from those emphasized in engineering designs, and subsequently a different type of design. [1] Typically, manned facilities in LEO have been designed in a 90° orientation to this design. In other words, the rooms are all circular (which has already been determined to be spatially confusing), cutting crosswise down the cylinder rather than lengthwise as is the case in this design. The longitudinal sectional cut allows the personal orientation and vertical to remain consistent throughout the entire component, and SPORE at large. |2] This design introduces pseudogravitational forces, intended to simulate gravitational forces, ranging from 0.1g to 1.0g, Earth normal gravity. It is hoped that within this range there exists a space optimization which maximizes health and productivity while minimizing costs. [3] The structure is no longer a solid, rigid body. Rather space is created only where it is needed; and the flexible SPORE gains its rigidity from its motion. This makes the structure much less dense, and less expensive as every bit of
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