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Escape Dynamics : ウィキペディア英語版 | Escape Dynamics
Escape Dynamics, Inc. is a Colorado-based technology company focused on bringing to market single-stage-to-orbit reusable electromagnetically powered spaceplanes.〔(【引用サイトリンク】url=http://www.planettechnews.com/interviews/ptn-interviews-escape-dynamics-on-the-future-of-space-technology )〕 The company was founded by Richard F. Schaden and a team of California Institute of Technology scientists headed by Dmitriy Tseliakhovich.〔(Escape Dynamics, Leadership )〕 Laetitia Garriott de Cayeux joined the founding team in 2014.〔(Laetitia Garriott de Cayeux Joins as Company President & COO )〕 Members of the Board of Advisors include Dr. Peter Diamandis of the X Prize Foundation, Mr. Gonzalo Martinez of Autodesk, Professor Harry Atwater of Caltech, Mr. Jonathan Knowles of Autodesk, Mr. Ingvar Petursson of Nintendo of America, Joseph Meyerowitz (co-founder of Escape Dynamics), and Mr. Shaun Maguire (co-founder of Escape Dynamics) of Caltech and Qadium Inc.. == Technology development == The key technology areas Escape Dynamics focuses on are: i) externally powered aerospace vehicles; ii) efficient, reliable and safe wireless energy transfer; and iii) highly efficient high power microwave sources.〔(Escape Dynamics, Technology )〕 Systems the company develops include high power microwave sources (gyrotrons) used to generate microwave energy required to power aerospace vehicles,〔(Turning on 100kW-class Microwave System )〕 high-speed steerable phased array antennas for millimeter-wave long distance wireless energy transfer.,〔(Microwave Power Beaming Milestone )〕 and electromagnetically-powered propulsion systems. In the summer 2015, the company demonstrated operation of a prototype thruster with specific impulse above 500 seconds 〔(Prototype Thruster Milestone )〕 using helium propellant. The demonstration showed an end-to-end sequence of operation of an externally-powered propulsion system. Energy was drawn from the grid, converted into microwaves using EDI's gyrotron, guided through a system of beam shaping mirrors, and beamed from an antenna to a thruster. Conversion of the microwave energy into thrust was performed using a thermal thruster with a highly efficient microwave-absorbing heat exchanger.
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