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Physics / Variable Specific Impulse Magnetoplasma Rocket / Ion thruster / Plasma propulsion engine / Plasma / Hall effect thruster / Helicon / Specific impulse / Krypton / Spacecraft propulsion / Aerospace engineering / Propulsion


Document Date: 2011-09-09 09:54:45

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City

Houston / Wiesbaden / Webster / /

Company

Juan Del Valle12 Ad Astra Rocket Company / Ad Astra Rocket Company / Nautel Ltd. / Sumitomo / /

Country

Germany / United States / Liberia / Costa Rica / /

Currency

pence / /

/

Facility

National Institute of Standards and Technology / University of Houston / The facility / III11 University of Houston / /

IndustryTerm

directed parallel ion kinetic energy / directed ion kinetic energy / stainless steel vacuum chamber / reduced ionization energy / flow kinetic energy / perpendicular ion kinetic energy / argon gas / ionization energy / perpendicular ion energy / ion energy / energy / resolvable 2nd lower energy / kinetic energy / electron energy distribution function / neutral gas flow rate / ambient neutral gas pressure / electrostatic potential energy / energy distribution / parallel ion energy / /

Organization

National Institute of Standards and Technology / University of Houston / /

Person

Mark D / Buena Vista / Franklin R. Chang / Tim W. Glover / Andrew V. Ilin / /

Position

Research Scientist / collector / guard / Director of Technology / Chief Executive Officer / ben.longmier@adastrarocket.com Director of Research / calibrated proportional flow control valve flow controller / Engineer / Staff Engineer / Professor / Physics and ECE / Principal Research Scientist / Staff Scientist / Lead Engineer / representative / Director of Development / /

ProgrammingLanguage

DC / /

ProvinceOrState

Texas / /

Technology

semiconductor / radiation / Probe Array / heat transfer / fiber optic / flow control / ISP / /

SocialTag