PPT-Integrated Linear Thruster

Steve Feketa June 2012 2 Agenda Frequently Asked Questions Applications Accessories and Options Specifications Benefits and Features LDATSeries Integrated Linear Thruster The LDATSeries Integrated Linear Thruster is . This light weight gimbal mechanism is equipped with flexible xenon propellant lines and features numerous thermal control features for all its critical components Unique thermal profiles and operating environments have been the key design drivers fo The gimbals can be con64257gured for wide rotation on both axes limited with the inclusion of range de64257ning hard stops on the thruster axes Moog has quali64257ed and 64258own the widest angular range thruster gimbals Designed and manufactured by e Ax where is vector is a linear function of ie By where is then is a linear function of and By BA so matrix multiplication corresponds to composition of linear functions ie linear functions of linear functions of some variables Linear Equations Breakthrough Space Propulsion Technology for the 21. st. Century. National Aeronautics and . Space Administration. Jet Propulsion Laboratory. California Institute of Technology. Pasadena, California. Yevgeny Raitses. Princeton Plasma Physics Laboratory. Princeton, New Jersey . 16. th. International Conference on Ion Sources, New York City, NY, August 28, 2015. Outline. Hall thruster. Status quo. Propulsion. Perspectives on Achievable Performance. Minimum energy expenditure in taking 1 kg of mass. to Earth Orbit : 9kWh. To Earth Escape : 18kWh. (Is this true? Please check!). Chemical energy depends of mass of propellant used – upper limit on. for libration point missions. Maksim . Shirobokov. Keldysh Institute of Applied Mathematics. Moscow Institute of Physics and . Technology. Sergey . Trofimov. Keldysh Institute of Applied Mathematics. 5 6 7 1 2 3 4 8 9 Contents 2 1 3 4 5 ContentsIntroductionWhy integrated care?Why integrated commissioning?Policy context and evidenceEvidence and experienceUse of joint arrangementsEectiveness of jo Cold Gas System. How the System Creates Propulsion. The system creates propulsion using an inert gas such as Nitrogen or Helium as the fuel.. The gas is stored under high pressure, then sent to the thruster which releases the gas.. the Rocket Equation with Photons. ykbae@ykbcorp.com. 714-838-2881. www.ykbcorp.com. Future In-Space Operation Colloquium. November 9. th. 2016. Credit: NASA. Young K. Bae, Ph.D.. CEO. Y.K. Bae Corp. Sarah E. Cusson. 1. , Marcel P. Georgin. 2. , Ethan T. Dale. 1. , . Vira. Dhaliwal. 1,. and Alec D. Gallimore. 1. 1. Department of Aerospace Engineering, University of Michigan; . 2. Applied Physics Program, University of Michigan . (HCEP). Phase I STTR. Principal Investigator: Christopher Davis, PhD. ElectroDynamic Applications, Inc.. Ann Arbor, Michigan. University Principal Investigator: Professor Michael . Micci. Penn State University. 3ublic reporting burden for this collection of information is estimated to average 1 hour per response including the time for reviewing insti Q - d aintaining thelata needed and completing and reviewi Electric Propulsion Definitions. Electric propulsion (EP) : any propulsion system which uses electrical power . to provide . propellant acceleration, and hence . thrust. .. Excludes . systems which only use power for thermal control, valve actuation, etc..