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Open-Source Conceptual Sizing Models for the Hyperloop Passenger PodHyperloop is a new mode of transportation proposed as an alternative to California's high speed rail project, with the intended benefits of higher performance at lower overall costs. It consists of a passenger pod traveling through a tube under a light vacuum and suspended on air bearings. The pod travels up to transonic speeds resulting in a 35 minute travel time between the intended route from Los Angeles and San Francisco. Of the two variants outlined, the smaller system includes a 1.1 meter tall passenger capsule traveling through a 2.2 meter tube at 700 miles per hour. The passenger pod features water-based heat exchangers as well as an on-board compression system that reduces the aerodynamic drag as it moves through the tube. Although the original proposal looks very promising, it assumes that tube and pod dimensions are independently sizable without fully acknowledging the constraints of the compressor system on the pod geometry. This work focuses on the aerodynamic and thermodynamic interactions between the two largest systems; the tube and the pod. Using open-source toolsets, a new sizing method is developed based on one-dimensional thermodynamic relationships that accounts for the strong interactions between these sub-systems. These additional considerations require a tube nearly twice the size originally considered and limit the maximum pod travel speed to about 620 miles per hour. Although the results indicate that Hyperloop will need to be larger and slightly slower than originally intended, the estimated travel time only increases by approximately five minutes, so the overall performance is not dramatically affected. In addition, the proposed on-board heat exchanger is not an ideal solution to achieve reasonable equilibrium air temperatures within the tube. Removal of this subsystem represents a potential reduction in weight, energy requirements and complexity of the pod. In light of these finding, the core concept still remains a compelling possibility, although additional engineering and economic analyses are markedly necessary before a more complete design can be developed.
Document ID
20150000699
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Chin, Jeffrey C.
(NASA Glenn Research Center Cleveland, OH United States)
Gray, Justin S.
(NASA Glenn Research Center Cleveland, OH United States)
Jones, Scott M.
(NASA Glenn Research Center Cleveland, OH United States)
Berton, Jeffrey J.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
January 22, 2015
Publication Date
January 5, 2015
Subject Category
Engineering (General)
Report/Patent Number
GRC-E-DAA-TN14666
Meeting Information
Meeting: SciTech 2015
Location: Kissimmee, FL
Country: United States
Start Date: January 5, 2015
End Date: January 9, 2015
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 794072.02.03.04.08.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
design analysis
multidisciplinary design optimization
systems analysis
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