BEAMED ENERGY PROPULSION
|
|
- Paula Goodwin
- 6 years ago
- Views:
Transcription
1 BEAMED ENERGY PROPULSION Fourth International Symposium on Beamed Energy Propulsion Nara Japan November 2005 EDITORS Kimiya Komurasaki The University of Tokyo Chiba Japan Takashi Yabe Shigeaki Uchida Tokyo Institute of Technology Tokyo, Japan Akihiro Sasoh Tohoku University Sendai, Japan SPONSORING ORGANIZATIONS The Commemorative Organization for the Japan World Exposition (70) Entropia Laser Initiative (Tokyo Institute of Technology) Institute for Laser Technology AIP 75 Years of Service Melville, New York, 2006 AIP CONFERENCE PROCEEDINGS VOLUME 830
2 CONTENTS Preface Committees Award xi xiii xv PLENARY SESSION Performance Characteristics of Laser Propulsion Engine Operating both in CW and in Repetitively-Pulsed Modes 3 Y. A. Rezunkov, A. L. Safronov, A. A. Ageichik, M. S. Egorov, V. V. Stepanov, V. S. Rachuk, V. Y. Guterman, A. V. Ivanov, S. G. Rebrov, and A. N. Golikov New Trends on Solid State Lasers 14 K. Yoshida, T. Yabe, S. Uchida, A. Ikesue, and T. Kamimura An Overview of Entropia Laser Initiative 21 T. Yabe, S. Uchida, K. Yoshida, K. Ikuta, and T. Okamoto FLUID DYNAMICS IN AIR-BREATHIG LASER PROPULSION Effects of Nozzle Structure on Laser Thruster Performance 33 C. Cui, Y. Hong, M. Wen, J. Wang, and G. He Pulsed Laser Propulsion Performance of 11-cm Parabolic 'Bell' Engines: CO2 TEA vs. EDL 38 K. Mori, A. Sasoh, and L. N. Myrabo Experimental Investigations of Laser Propulsion by Using Gas-Dynamic Laser 48 V. S. Rachuk, V. Y. Guterman, A. V. Ivanov, S. G. Rebrov, A. N. Golikov, ' N. B. Ponomarev, and Y. A. Rezunkov \ Analytical Investigation of an Airbreathing, Repetitively Pulsed LSC-Wave Thruster: Part 1 58 L. N. Myrabo, C. A. Borkowski, and D. A. Kaminski Analytical Investigation of an Airbreathing, Repetitively Pulsed LSC-Wave Thruster: Part 2 72 C. A. Borkowski, D. A. Kaminski, and L. N. Myrabo Experimental Investigation for 100-Joule-class TEA CO 2 Laser and Gas Interaction Z. Dou, H. Yao, J. Wang, M. Wen, P. Wang, J. Yang, and C. Li Numerical Simulation for Laser Propulsion of Air Breathing Mode Considering Moving Boundaries and Multi-Pulses 87 P. Gong and Z. Tang Micro Supersonic Air-Breathing Laser-Spike Engine Propulsion 95 Y.-T. Kim, S. Kim, and I.-S. Jeung
3 Experimental Study of the Momentum Coupling Coefficient with the Pulse Frequency and Ambient Pressure for Air-Breathing Laser Propulsion 104 Z. Tang, J. Cai, P. Gong, X. Hu, R. Tan, Z. Zheng, J. Wu, and Y. Lu Experimental Study on Laser Propulsion of Air-breathing Mode 114 R. Tan, Y. Zheng, C. Ke, D. Wang, K. Zhang, G. Zheng, C. Wan, S. Liu, J. Wu, and Y. Yu Thrust Generating Mechanism of Nozzle Powered by Single Laser Pulse 121 Q. Li, Y. Hong, J. She, Z. Cao, and J. Wang LASER SUPPORTED DETONATION AND ENERGY DEPOSITION Energy Conversion Process in Laser Supported Detonation Waves Induced by a Line-Focusing Laser 133 M. Ushio, K. Kawamura, K. Komurasaki, H. Katsurayama, H. Koizumi, and Y. Arakawa Numerical Analysis on Non-Equilibrium Mechanism of Laser-Supported Detonation Wave Using Multiply-Charged Ionization 142 H. Shiraishi Mixing and Reaction Enhancement Characteristics of Laser-Induced Plasmas and Detonations in Laser-Augmented Scramjets 151 J. Negishi, H. Horisawa, and I. Kimura Experimental Analysis of Heat Flux to a Blunt Body in Hypersonic Flow with Upstream Laser Energy Deposition-Preliminary Results Salvador, M. A. S. Minucci, P. G. P. Toro, A. C. Oliveira, J. B. Channes, Jr., L. N. Myrabo, and H. T. Nagamatsu LASER IN-TUBE THRUSTER Physical Processes of the Interaction Between Laser-Generated Plasma and Blast Wave Appearing in Laser-Driven in-tube Accelerator Configuration 175 A. Sasoh, K. Mori, T. Ohtani, N. Ohnishi, Y. Ogino, and K. Sawada Impulse Characteristics of Laser-driven in-tube Accelerator (LITA) 179 T. Ohtani, K. Mori, and A. Sasoh Blast Wave Formation by Laser-Sustained Nonequilibrium Plasma in the Laser-Driven in-tube Accelerator Operation. 183 Y. Ogino, N. Ohnishi, A. Sasoh, and K. Sawada Numerical Simulation of Laser-Driven in-tube Accelerator Operation 191 N. Ohnishi, Y. Ogino, K. Sawada, T. Ohtani, K. Mori, and A. Sasoh VI
4 ABLATIVE PROPULSION AND MICROTHRUSTERS Plasma Diagnostics of a Forward Laser Plasma Accelerated Thruster 201 M. Izumi, H. Horisawa, A. Takeda, and I. Kimura Electromagnetic Acceleration Characteristics of Laser-electric Hybrid Thrusters ;r 213 K. Sasaki, A. Takeda, H. Horisawa, and I. Kimura Performance Test Results for the Laser-powered Microthruster 224 C. R. Phipps, J. R. Luke, W. Helgeson, and R. Johnson A ns-pulse Laser Microthruster 235 C. R. Phipps, J. R. Luke, W. Helgeson, and R. Johnson Laser-Driven Mini-Thrusters 247 E. Sterling, J. Lin, J. Sinko, L. Kodgis, S. Porter, A. V. Pakhomov, C. W. Larson, and F. B. Mead, Jr. An Experimental and Conceptual Investigation of Laser Micro Propulsion 259 J. Cai, X. Hu, and Z. Tang High Velocity Particle Cloud Generation by Pulse Laser Ablation of Ground Glass Surface 268 K. Nagayama, Y. Kotuska, M. Nakahara, and S. Kubota CO 2 Laser Absorption in Ablation Plasmas 272 H.-A. Eckel, J. Tegel, W. O. Schall. Performance Characteristics of Low-Power Laser Ablative Thrusters for Small Satellites 284 H. Maesato, E. Koizumi, and H. Tahara LIQUID PROPELLANT Experimental Study on Continuous Liquid Propellant Supply Mechanisms for Water Cannon Laser Thruster 297 M. Onda and T. Ootani :> Ablation of Liquids for Laser Propulsion with TEA CO 2 Laser 308 J. Sinko, L. Kodgis, S. Porter, E. Sterling, J. Lin, A. V. Pakhomov, C. W. Larson, and F. B. Mead, Jr. Primary Experimental Study on Liquid Ablatant for Laser Propulsion 319 X. Li, Y. Hong, J. Chen, J. Wang, and G. He MICROWAVE AND ION BEAM PROPULSION Single Port Electro-thermal Propulsion Design Factors 329 D. G. Johansen Pressure History Measurement in a Microwave Beaming Thruster 341 Y. Oda, M. Ushio, K. Komurasaki, K. Takahashi, A. Kasugai, and K. Sakamoto vii
5 Performance and Controllability of Pulsed Ion Beam Ablation Propulsion, 349 M. Yazawa, C. Buttapeng, H. Suematsu, W. Jiang, K. Yatsui, and N. Harada A Compact Nuclear Fusion Reactor for Space Flights 359 A. F. Nastoyashchiy Fluxes of Fast Multi-Charged Ions for Producing Jet Propulsion 366 A. F. Nastoyashchiy Hydrodynamic Efficiency of Ablation Propulsion with Pulsed Ion Beam 372 C. Buttapeng, M. Yazawa, N. Harada, H. Suematsu, W. Jiang, and K. Yatsui POWER SOURCES Oscillation Property of Disk-type Nd/Cr:YAG Ceramic Lasers with Quasi-solar Pumping 383 T. Saiki, K. Imasaki, S. Motokoshi, C. Yamanaka, S. Uchida, H. Fujita, M. Nakatsuka, and Y. Izawa A Comparison of Laser and Microwave Approaches to CW Beamed Energy Launch 388 J. T. Kare and K. L. G. Parkin Potential Use of CW High Energy Laser on an Airborne Platform 400 J. R. Cook, S. J. Cusumano, and M. R. Whiteley Metal Matrix Superconductor Composites for SMES-Driven, Ultra High Power BEP Applications: Part D. A. Gross and L. N. Myrabo Metal Matrix Superconductor Composites for SMES-Driven, Ultra High Power BEP Applications: Part D. A. Gross and L. N. Myrabo ENTROPIA LASER INITIATIVE Experimental Study of Solar Pumped Laser for Magnesium-Hydrogen Energy Cycle 439 S. Uchida, T. Yabe, Y. Sato, K. Yoshida, A. Ikesue, T. Ohkubo, A. Mabuchi, Y. Ogata, K. Nakagawa, A. Ohyama, N. Onodera, T. Ohishi, Y. Ohtaka, Y. Yamada, and S. Ito MgO Deoxidization by Focused Laser Pulse for a New Energy Cycle 447 T. Yabe, K. Ikuta, C. Baasandash, R. Katano, S. Uchida, M. Tsuji, Y. Mori, J. Maehara, M. S. Mahmoud, and T. Toya Anti-Refractive and Waterproof Hard Coating for High Power Laser Optical Elements 457 M. Murahara, T. Yabe, S. Uchida, K. Yoshida, and Y. Okamoto viii
6 MEASUREMENT TECHNIQUES AND FACILITIES Development of a New Hypersonic Shock Tunnel Facility to Investigate Electromagnetic Energy Addition for Flow Control and Basic Supersonic Combustion 469 P. G.P. Toro, M. A. S. Minucci, J. B. Chanes, Jr., A. L. Pereira, and H. T. Nagamatsu Development of Surface Junction Thermocouples for High Enthalpy Measurements Salvador, M. A. S. Minucci, P. G. P. Toro, A. C. Oliveira, and J. B. Channes, Jr. A Low-Noise Thrust Stand for Microthrusters with 25nN Resolution 492 C. R. Phipps, J. R. Luke, W. Helgeson, and R. Johnson Time-Resolved Force Measurement Over Laser-Ablated Materials 500 K. Mori, K. Anju, and A. Sasoh Schlieren Visualization Technique Applied to the Study of Laser-Induced Breakdown in Low Density Hypersonic Flow 504 A. C. Oliveira, M. A. S. Minucci, P. G. P. Toro, J. B. Chanes, Jr., 1.1. Salvador, L. N. Myrabo, and H. T. Nagamatsu SYSTEMS AND MISSIONS Lightcraft and Laser Beam Mutual Orientation and Motion Control System using Quaternions 513 Y. M. Baturin Trajectory Simulations, Qualitative Analyses and Parametric Studies of a Laser- Launched Micro-Satellite Using OTIS 522 S. D. Knecht, F. B. Mead, M. M. Micci, and C. W. Larson An Overview of the Experimental 50-cm Laser Ramjet (X-50LR) Program 534 F. B. Mead, Jr., C. W. Larson, and S. D. Knecht Remote Control of Laser-Driven Micro-Vehicles 553 T. Okita, K. Hoshino, and I. Kajiwara Earth-to-Orbit Laser Launch Simulation for the Lightcraft Technology Demonstrator 564 J. C. Richard, C. Morales, W. L. Smith, and L. N. Myrabo Laser Propulsion for ESA Missions: Ground to Orbit Launch Project Overview Part D. P. Resendes, S. Mota, J. T. Mendonc,a, B. Sanders, J. Encarnacio, J. A. Gonzalez del Amo, and L. N. Myrabo NEW CONCEPTS Nuclear Development of Laser Propelled "Semi-Perpetual" Rotary Machine 591 M. M. Gualini, S. A. Khan, and K. Zulfiqar ix
7 Nuclear Waste Disposal in Space: BEP's Best Hope? 600 J. Coopersmith Sending a Probe to Alpha Centauri on a Voyage of Five to Ten Years 605 D. Junker and W. D. Hobbs, Jr. LIGHTCRAFT Comparison of Ablation Performance in Laser Lightcraft and Standardized Mini-Thruster 615 S. D. Knecht, C. W. Larson, and F. B. Mead Experimental and Numerical Investigation of Effects of Laser Pulse Waveform on Lightcraft Performance 628 M. Wen, Y. Hong, Z. Cao, J. Wang, and C. Cui Analysis of Charge Cloud Geometries for Ion Propulsion of Microwave Lightcraft 637 L. Salasoo, J. P. Moder, L. N. Myrabo, and J. K. Nelson Microwave Power Beaming Infrastructure for Manned Lightcraft Operations 651 L. N. Myrabo Author Index 663
Air Breathing Processes in a Repetitively Pulsed Microwave Rocket
46th AIAA Aerospace Sciences Meeting and Exhibit 7 - January 8, Reno, Nevada AIAA 8-85 Air Breathing Processes in a Repetitively Pulsed Microwave Rocket Yuya SHIRAISHI, Yasuhisa ODA, Teppei SHIBATA 3 and
More informationModeling of Laser Supported Detonation Wave Structure Based on Measured Plasma Properties
9th Plasmadynamics and Lasers Conference - 6 June 8, Seattle, Washington AIAA 8-49 Modeling of Laser Supported Detonation Wave Structure Based on Measured Plasma Properties Keigo Hatai *, Akihiro Fukui,
More informationTailoring Laser Propulsion for Future Applications in Space
Tailoring Laser Propulsion for Future Applications in Space Hans-Albert Eckel and Stefan Scharring German Aerospace Center (DLR) Institute of Technical Physics, Pfaffenwaldring 38 40, 70569 Stuttgart,
More informationSupersonic laser propulsion
Supersonic laser propulsion Yurii Rezunkov 1, * and Alexander Schmidt 2 1 Institute of Optoelectronic Instrument Engineering, Sosnovyi Bor, Leningrad oblast 188540, Russia 2 Ioffe Physical Technical Institute,
More informationAnalytical Study on Flight Performance of an Air-Breathing RP Laser Launcher
4th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 11-14 July 24, Fort Lauderdale, Florida AIAA 24-585 Analytical Study on Flight Performance of an Air-Breathing RP Laser Launcher Hiroshi KATSURAYAMA,
More informationLASER PROPULSION A NEW TECHNOLOGY FOR SPACE FLIGHT
LASER PROPULSION A NEW TECHNOLOGY FOR SPACE FLIGHT H.-A. Eckel, S. Karg, S. Scharring German Aerospace Center, Institute of Technical Physics, Pfaffenwaldring 38-40, 70569 Stuttgart Germany Abstract In
More informationChemically-Augmented Pulsed Laser-Ramjet
Chemically-Augmented Pulsed Laser-Ramjet IEPC-27-97 Presented at the 3 th International Electric Propulsion Conference, Florence, Italy Tomoki Kaneko * Hideyuki Horisawa Kazunobu Tamadao Department of
More informationStudy on Energy Law of Similitude for Laser Propulsion in Repetitively-pulsed Mode
Chinese Journal of Aeronautics (9) 583-589 Chinese Journal of Aeronautics www.elsevier.com/locate/cja Study on Energy aw of Similitude for aser Propulsion in Repetitively-pulsed Mode Hong Yanji a, *, Cao
More informationContents. Preface... xvii
Contents Preface... xvii CHAPTER 1 Idealized Flow Machines...1 1.1 Conservation Equations... 1 1.1.1 Conservation of mass... 2 1.1.2 Conservation of momentum... 3 1.1.3 Conservation of energy... 3 1.2
More informationLaser Supported Detonation in Argon Atmosphere
49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 4-7 January 2011, Orlando, Florida AIAA 2011-1139 Laser Supported Detonation in Argon Atmosphere Kohei Shimamura
More informationDevelopment of an Alternating Electric Field Accelerator for Laser-Ablation Plasma Acceleration
Development of an Alternating Electric Field Accelerator for Laser-Ablation Plasma Acceleration IEPC-2015-91125 Presented at Joint Conference of 30th International Symposium on Space Technology and Science
More informationPlasma Behaviours and Magnetic Field Distributions of a Short-Pulse Laser-Assisted Pulsed Plasma Thruster
Plasma Behaviours and Magnetic Field Distributions of a Short-Pulse Laser-Assisted Pulsed Plasma Thruster IEPC-2015-91325 Presented at Joint Conference of 30th International Symposium on Space Technology
More informationNumerical Investigation of LSD Wave Characteristics Using a 1-D Laser-induced Discharge Model
Numerical Investigation of LSD Wave Characteristics Using a 1-D Laser-induced Discharge Model Rei Kawashima 1, Joseph A. Ofosu 2, Kohei Matsui 1, Toru Shimano 2, Kimiya Komurasaki 1, Kohei Shimamura 3,
More informationLaser-Augmented Micro-Pulsejet Thruster
Laser-Augmented Micro-Pulsejet Thruster IEPC-2007-245 Presented at the 30 th International Electric Propulsion Conference, Florence, Italy Sou Eto * and Hideyuki Horisawa Tokai University, Hiratsuka-shi,
More informationAdvanced 14 Aerospace Applications of
Advanced 14 Aerospace Applications of Nano-Second-Laser-Pulse-Induced Pressure Modulation Prof. A. Sosoh Dept. of Aerospace Engineering Nagoya University Laser-Pulse-Induced Pressure Modulation Mixing
More informationIV. Rocket Propulsion Systems. A. Overview
IV. Rocket Propulsion Systems A. Overview by J. M. Seitzman for AE 4451 Jet and Rocket Propulsion Seitzman Rocket Overview-1 Rocket Definition Rocket Device that provides thrust to a vehicle by accelerating
More informationHigh Pulse Repetition Frequency Operation of Low-power short-pulse Plasma Thruster
High Pulse Repetition Frequency Operation of Low-power short-pulse Plasma Thruster IEPC-2015-91035 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International
More informationPropulsion Systems Design MARYLAND. Rocket engine basics Survey of the technologies Propellant feed systems Propulsion systems design
Propulsion Systems Design Rocket engine basics Survey of the technologies Propellant feed systems Propulsion systems design 2008 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu 1 Propulsion
More informationThe Effect of the Discharge Chamber Structure on the Performance of a 5 cm-diameter ECR Ion Thruster
Progress In Electromagnetics Research Letters, Vol. 75, 91 96, 2018 The Effect of the Discharge Chamber Structure on the Performance of a 5 cm-diameter ECR Ion Thruster Yujun Ke, Xinfeng Sun *, Yong Zhao,
More informationREPORT DOCUMENTATION PAGE
REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions,
More informationThisdocumentismadeavailablethroughthedeclassificationeforts andresearchofjohngreenewald,jr.,creatorof: TheBlackVault
Thisdocumentismadeavailablethroughthedeclassificationeforts andresearchofjohngreenewald,jr.,creatorof: TheBlackVault TheBlackVaultisthelargestonlineFreedom ofinformationact(foia) documentclearinghouseintheworld.theresearchefortshereare
More informationFundamental Study of Laser Micro Propulsion Using Powdered-Propellant
Fundamental Study of Laser Micro Propulsion Using Powdered-Propellant IEPC-2007-230 Presented at the 30 th International Electric Propulsion Conference, Florence, Italy S. Yokoyama *, and H. Horisawa Tokai
More information6-DOF Flight Dynamics of Laser-Boosted Vehicle Driven by Blast Wave
6-DOF Flight Dynamics of Laser-Boosted Vehicle Driven by Blast Wave IEPC-213-179 Presented at the 33 rd International Electric Propulsion Conference, The George Washington University, Washington, D.C.,
More informationExtraction of explosive characteristics from stable materials irradiated by low-power laser diodes
Extraction of explosive characteristics from stable materials irradiated by low-power laser diodes IEPC-215-91263 Presented at Joint Conference of 3th International Symposium on Space Technology and Science
More informationCalculation of The Vehicle Drag and Heating Reduction at Hypervelocities with Laser- Induced Air Spike
doi: 8/jatm.v5i.80 Calculation of The Vehicle Drag and Heating Reduction at Hypervelocities with Laser- Induced Air Spike Israel da Silveira Rêgo, Paulo Gilberto de Paula Toro, Marco Antonio Sala Minucci
More informationDevelopment of thrust stand for low impulse measurement from microthrusters
REVIEW OF SCIENTIFIC INSTRUMENTS VOLUME 75, NUMBER 10 OCTOBER 2004 Development of thrust stand for low impulse measurement from microthrusters H. Koizumi Department of Aeronautics and Astronautics, University
More informationHypersonic inlet for a laser powered propulsion system and its interaction with an idealized laser induced detonation wave
Hypersonic inlet for a laser powered propulsion system and its interaction with an idealized laser induced detonation wave Alan Harrland, Dr. Con Doolan and Dr. Vincent Wheatley School of Mechanical Engineering,
More informationNon-Phase-Difference Rogowski Coil for Measuring Pulsed Plasma Thruster Discharge Current
Non-Phase-Difference Rogowski Coil for Measuring Pulsed Plasma Thruster Discharge Current IEPC-2015-49/ISTS-2015-b-49 Presented at Joint Conference of 30th International Symposium on Space Technology and
More informationHypersonic Inlet for a Laser Powered Propulsion System
Hypersonic Inlet for a Laser Powered Propulsion System Alan Harrland, Con Doolan, Vincent Wheatley, and Dave Froning Citation: AIP Conference Proceedings 1402, 145 (2011); doi: 10.1063/1.3657023 View online:
More informationHigh Isp Mechanism of Rectangular Laser-Electromagnetic Hybrid Acceleration Thruster
High Isp Mechanism of Rectangular Laser-Electromagnetic Hybrid Acceleration Thruster IEPC-2011-274 Presented at the 32nd International Electric Propulsion Conference, Wiesbaden Germany Hideyuki Horisawa
More informationAcceleration of a plasma flow in a magnetic Laval nozzle applied to an MPD thruster
Acceleration of a plasma flow in a magnetic Laval nozzle applied to an MPD thruster IEPC-5-68 Presented at Joint Conference of 3th International Symposium on Space Technology and Science 34th International
More informationPreface. 2 Cable space accelerator 39
Contents Abstract Preface xiii xv 1 Space elevator, transport system for space elevator, 1 and tether system 1.1 Brief history 1 1.2 Short description 2 1.3 Transport system for the space elevator 5 1.4
More informationElectric Rocket Engine System R&D
Electric Rocket Engine System R&D In PROITERES, a powered flight by an electric rocket engine is planed; that is, orbital transfer will be carried out with a pulsed plasma thruster (PPT). We introduce
More informationControl of thrust measurement system for cw laser thrusters
Control of thrust measurement system for cw laser thrusters IEPC-2011-322 Presented at the 32nd International Electric Propulsion Conference, Wiesbaden Germany Keiji Hagiwara 1, Hitoshi Yonamine 2, and
More information3. Write a detailed note on the following thrust vector control methods:
Code No: R05322103 Set No. 1 1. Starting from the first principles and with the help of neatly drawn velocity triangles obtain the following relationship: Ψ = 2 Φ (tan β 2 + tan β 3 ) where Ψ is the blade
More informationProgress in LPP EUV Source Development by Japan MEXT Project
Progress in LPP EUV Source Development by Japan MEXT Project Y. Izawa, N. Miyanaga, H. Nishimura, S. Fujioka, T. Aota, K. Nagai, T. Norimatsu,K. Nishihara, M. Murakami, Y. -G. Kang, M. Nakatsuka, H. Fujita,
More informationThrust Measurement of a CW Laser Thruster in Vacuum
Thrust Measurement of a CW Laser Thruster in Vacuum Kazuhiro Toyoda Kyushu Institute of Technology Komurasaki Kimiya and Yoshihiro Arakawa University of Tokyo IEPC-01-207 This paper reports results of
More informationDevelopment of a Two-axis Dual Pendulum Thrust Stand for Thrust Vector Measurement of Hall Thrusters
Development of a Two-axis Dual Pendulum Thrust Stand for Thrust Vector Measurement of Hall Thrusters Naoki Nagao, Shigeru Yokota, Kimiya Komurasaki, and Yoshihiro Arakawa The University of Tokyo, Tokyo,
More informationDISCHARGE CHARACTERISTICS OF A LASER-ASSISTED PLASMA THRUSTER
DISCHARGE CHARACTERISTICS OF A LASER-ASSISTED PLASMA THRUSTER Hideyuki Horisawa *, Masatoshi Kawakami *, Wun-Wei Lin *, Akira Igari *, and Itsuro Kimura # * Department of Aeronautics and Astronautics,
More informationRocket Propulsion Overview
Rocket Propulsion Overview Seitzman Rocket Overview-1 Rocket Definition Rocket Device that provides thrust to a vehicle by accelerating some matter (the propellant) and exhausting it from the rocket Most
More informationA Low-Noise Thrust Stand for Microthrusters with 25nN Resolution
A Low-Noise Thrust Stand for Microthrusters with 25nN Resolution Claude R. Phipps 1, James R. Luke 1,2, Wesley Helgeson 2 and Richard Johnson 2 1 Photonic Associates LLC, 200A Ojo de la Vaca Road, Santa
More informationMARYLAND. Rocket engine basics Survey of the technologies Propellant feed systems Propulsion systems design U N I V E R S I T Y O F
Rocket engine basics Survey of the technologies Propellant feed systems Propulsion systems design 2004 David L. Akin - All rights reserved http://spacecraft.ssl. umd.edu Overview of the Design Process
More informationInternational Symposium of Cavitation and Multiphase Flow (ISCM 2014) Beijing, China October 2014
International Symposium of Cavitation and Multiphase Flow (ISCM 2014) IOP Conference Series: Materials Science and Engineering Volume 72 Beijing, China 18-21 October 2014 ISBN: 978-1-63439-883-1 ISSN:
More informationA 25nN Low-Noise Thrust Stand for Microthrusters
A 25nN Low-Noise Thrust Stand for Microthrusters Claude R. Phipps * and James R. Luke Photonic Associates, LLC, Santa Fe, NM 87508 Wesley D. Helgeson NMT/IERA, Albuquerque, NM 87106 We describe the design,
More informationImproved Target Method for AF-MPDT Thrust Measurement
Improved Target Method for AF-MPDT Thrust Measurement IEPC-2015-172 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric Propulsion
More informationPropulsion Systems Design MARYLAND. Rocket engine basics Survey of the technologies Propellant feed systems Propulsion systems design
Design Rocket engine basics Survey of the technologies Propellant feed systems Propulsion systems design 2005 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu Overview of the Design Process
More informationA Fusion Propulsion System for Interstellar Missions
ICF: A Fusion Propulsion System for Interstellar issions Terry Kammash and Brice N. Cassenti Nuclear Engineering and Radiological Sciences Dept., University of ichigan, Ann Arbor, I 48109 United Technologies
More informationConceptual Design of Manned Space Transportation Vehicle (MSTV) Using Laser Thruster in Combination with H-II Rocket
Conceptual Design of Manned Space Transportation Vehicle (MSTV) Using Laser Thruster in Combination with H-II Rocket Laser Thruster Yoshinari Minami Advanced Sci.-Tech. Rsch. Orgn. (Formerly NEC Space
More informationExperimental Study of a 1-MW-Class Quasi-Steady-State Self-Field Magnetoplasmadynamic Thruster
Experimental Study of a 1-MW-Class Quasi-Steady-State Self-Field Magnetoplasmadynamic Thruster IEPC-2013-234 1 Kenji Miyazaki and 2 Syun Takenaka Tokai University, Hiratsuka, Kanagawa 259-1292, Japan 3
More informationInfluence of Electrode Configuration of a Liquid Propellant PPT on its Performance
Influence of Electrode Configuration of a Liquid Propellant PPT on its Performance IEPC-- /ISTS--b- Presented at Joint Conference of th International Symposium on Space Technology and Science th International
More informationElectric Propulsion System using a Helicon Plasma Thruster (2015-b/IEPC-415)
Electric Propulsion System using a Helicon Plasma Thruster (2015-b/IEPC-415) Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric Propulsion
More informationTAU Extensions for High Enthalpy Flows. Sebastian Karl AS-RF
TAU Extensions for High Enthalpy Flows Sebastian Karl AS-RF Contents Motivation Extensions available in the current release: Numerical schemes for super- and hypersonic flow fields Models for gas mixtures,
More information1. (a) Describe the difference between over-expanded, under-expanded and ideallyexpanded
Code No: R05322106 Set No. 1 1. (a) Describe the difference between over-expanded, under-expanded and ideallyexpanded rocket nozzles. (b) While on its way into orbit a space shuttle with an initial mass
More informationElectrostatic and Electromagnetic Acceleration in a Laser-Electric Hybrid Thruster
Electrostatic and Electromagnetic Acceleration in a Laser-Electric Hybrid Thruster IEPC-25-23 Presented at the 29 th International Electric Propulsion Conference, Princeton University, October 31 November
More informationPHYSICS BASIS FOR THE GASDYNAMIC MIRROR (GDM) FUSION ROCKET. Abstract
PHYSICS BASIS FOR THE GASDYNAMIC MIRROR (GDM) FUSION ROCKET T. Kammash Department of Nuclear Engineering and Radiological Sciences University of Michigan Ann Arbor, MI 48109 (313) 764-0205 W. Emrich Jr.
More informationResearch and Development of High-Power Electrothermal Pulsed Plasma Thruster Systems for Osaka Institute of Technology 2nd PROITERES Nano-Satellite
Research and Development of High-Power Electrothermal Pulsed Plasma Thruster Systems for Osaka Institute of Technology 2nd PROITERES Nano-Satellite IEPC-2015-22 /ISTS-2015-b-22 Presented at Joint Conference
More informationFundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion
Fundamental Mechanisms, Predictive Modeling, and Novel Aerospace Applications of Plasma Assisted Combustion Walter R. Lempert, Igor V. Adamovich, J. William Rich, Jeffrey A. Sutton Department of Mechanical
More informationLimits of Simulating Gas Giant Entry at True Gas Composition and True Flight Velocities in an Expansion Tube
Limits of Simulating Gas Giant Entry at True Gas Composition and True Flight Velocities in an Expansion Tube 8th European Symposium on Aerothermodynamics for Space Vehicles C.M. James, D.E. Gildfind, R.G.
More informationMiniature Vacuum Arc Thruster with Controlled Cathode Feeding
Miniature Vacuum Arc Thruster with Controlled Cathode Feeding Igal Kronhaus and Matteo Laterza Aerospace Plasma Laboratory, Faculty of Aerospace Engineering, Technion - Israel Institute of Technology,
More informationTime-Independent Fully kinetic Particle-in-Cell for plasma magnetic field interactions
Time-Independent Fully kinetic Particle-in-Cell for plasma magnetic field interactions IEPC-2015-478p /ISTS-2015-b-91353 Presented at Joint Conference of 30th International Symposium on Space Technology
More informationA review of plasma thruster work at the Australian National University
A review of plasma thruster work at the Australian National University IEPC-2015-90850 Presented at Joint Conference of 30th International Symposium on Space Technology and Science 34th International Electric
More informationCharacteristics of Side by Side Operation of Hall Thruster
Characteristics of Side by Side Operation of Hall Thruster IEPC-5-7/ISTS-5-b-7 Presented at Joint Conference of th International Symposium on Space Technology and Science 4th International Electric Propulsion
More informationREPORT DOCUMENTATION PAGE
REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instructions,
More informationConcepts in Spin Electronics
Concepts in Spin Electronics Edited by Sadamichi Maekawa Institutefor Materials Research, Tohoku University, Japan OXFORD UNIVERSITY PRESS Contents List of Contributors xiii 1 Optical phenomena in magnetic
More information11.1 Survey of Spacecraft Propulsion Systems
11.1 Survey of Spacecraft Propulsion Systems 11.1 Survey of Spacecraft Propulsion Systems In the progressing Space Age, spacecrafts such as satellites and space probes are the key to space exploration,
More informationHelicon Plasma Thruster Persepective and At University of Padua
Helicon Plasma Thruster Persepective and Development status and future development At University of Padua D.Pavarin, M.Manente, F.Trezzolani, A.Selmo, M.Magarotto, E.Toson Outline Helicon Thruster overview
More informationEXTERNAL-JET (FLUID) PROPULSION ANALOGY FOR PHOTONIC (LASER) PROPULSION By John R. Cipolla, Copyright February 21, 2017
EXTERNAL-JET (FLUID) PROPULSION ANALOGY FOR PHOTONIC (LASER) PROPULSION By John R. Cipolla, Copyright February 21, 2017 ABSTRACT External-jet propulsion uses a narrow jet of high velocity water or conceptually
More information(b) Analyzed magnetic lines Figure 1. Steady state water-cooled MPD thruster.
A. MPD thruster In this study, as one of the In-Space Propulsion projects by JAXA (Japan Aerospace exploration Agency), a practical MPD propulsion system was investigated. We planned to develop MPD thrusters
More informationTo the space by laser light (II)
Vol.4, No.9, 713-718 (2012) http://dx.doi.org/10.423/ns.2012.49094 Natural Science To the space by laser light (II) Victor V. Apollonov A. M. Prokhorov General Physics Institute, Moscow, Russia; vapollo@kapella.gpi.ru
More informationLaser Ablation of Metal Doped Polymers with CO 2 Laser
Laser Ablation of Metal Doped Polymers with CO 2 Laser EOARD Grant FA8655-3-1-361 Properties of Laser Ablation Products of Delrin with CO 2 Laser Wolfgang O. Schall H.-A. Eckel, J. Tegel, F. Waiblinger,
More informationElectric Field Measurements in Atmospheric Pressure Electric Discharges
70 th Gaseous Electronics Conference Pittsburgh, PA, November 6-10, 2017 Electric Field Measurements in Atmospheric Pressure Electric Discharges M. Simeni Simeni, B.M. Goldberg, E. Baratte, C. Zhang, K.
More informationSimultaneous Measurement of Impulse Bits and Mass Shots of Electrothermal Pulsed Plasma Thruster
Simultaneous Measurement of Impulse Bits and Mass Shots of Electrothermal Pulsed Plasma Thruster IEPC-2017-456 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology
More informationThermal Radiation Studies for an Electron-Positron Annihilation Propulsion System
Thermal Radiation Studies for an Electron-Positron Annihilation Propulsion System Jonathan A. Webb Embry Riddle Aeronautical University Prescott, AZ 8631 Recent studies have shown the potential of antimatter
More informationIEPC Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta, Georgia USA
Research and Development of Electrothermal Pulsed Plasma Thruster Systems for Powered Flight onboard the Osaka Institute of Technology 2nd PROITERES Nano-Satellite IEPC-2017-89 Presented at the 35th International
More informationDynamic Pressure Characterization of a Dual-Mode Scramjet
26 th ICDERS July 30 th August 4 th, 2017 Boston, MA, USA Dynamic Pressure Characterization of a Dual-Mode Scramjet Camilo Aguilera, Amardip Ghosh, Kyung-Hoon Shin, Kenneth H. Yu Department of Aerospace
More informationDirect Conversion for Space Solar Power
Direct Conversion for Space Solar Power Nicholas Boechler gtg218s@mail.gatech.edu Research Advisor: Prof. Komerath Direct Conversion Concept Given broad/narrow band EM radiation source Sun Man made EM
More informationGeneration and Acceleration of High-Density Helicon Plasma Using Permanent Magnets for the Completely Electrodeless Propulsion System )
Generation and Acceleration of High-Density Helicon Plasma Using Permanent Magnets for the Completely Electrodeless Propulsion System ) Shuhei OTSUKA, Toshiki NAKAGAWA, Hiroki ISHII, Naoto TESHIGAHARA,
More informationNumerical Simulation of Microwave Plasma Thruster Flow
Numerical Simulation of Microwave Plasma Thruster Flow IEPC-2007-211 Presented at the 30 th International Electric Propulsion Conference, Florence, Italy September 17-20, 2007 Mao-lin Chen *, Mao Gen-wang,
More informationNumber Density Measurement of Neutral Particles in a Miniature Microwave Discharge Ion Thruster
Trans. JSASS Aerospace Tech. Japan Vol. 12, No. ists29, pp. Tb_31-Tb_35, 2014 Topics Number Density Measurement of Neutral Particles in a Miniature Microwave Discharge Ion Thruster By Yuto SUGITA 1), Hiroyuki
More informationImaging of Plasma Flow around Magnetoplasma Sail in Laboratory Experiment
J. Plasma Fusion Res. SERIES, Vol. 8 (2009) Imaging of Plasma Flow around Magnetoplasma Sail in Laboratory Experiment Kazuma UENO, Tomohiro AYABE 1), Ikkoh FUNAKI 2), Hideyuki HORISAWA 1) and Hiroshi YAMAKAWA
More informationYUsend-1 Solid Propellant Microthruster Design, Fabrication and Testing
YUsend-1 Solid Propellant Microthruster Design, Fabrication and Testing 24 th AIAA/USU Conference on Small Satellites Authors: Kartheephan Sathiyanathan, Regina Lee, Hugh Chesser (York University) Charles
More informationAntimatter Driven Sail for Deep Space Exploration
Antimatter Driven Sail for Deep Space Exploration Dr. Steven D. Howe Dr. Gerald P. Jackson Hbar Technologies, LLC Any technology being presented to you at this workshop will need at least one miracle in
More informationCONTENTS Real chemistry e ects Scramjet operating envelope Problems
Contents 1 Propulsion Thermodynamics 1-1 1.1 Introduction.................................... 1-1 1.2 Thermodynamic cycles.............................. 1-8 1.2.1 The Carnot cycle.............................
More informationEffect of Fuel-to-Oxidiser Ratio on Thrust Generation of a Hybrid Al + NaOH + H 2 O Propulsion System for CubeSat Applications
Effect of Fuel-to-Oxidiser Ratio on Thrust Generation of a Hybrid Al + NaOH + H 2 O Propulsion System for CubeSat Applications Ahmed, O. D. and Knoll, A. K. Surrey Space Centre, University of Surrey, GU2
More informationFlight Demonstration of Electrostatic Thruster Under Micro-Gravity
Flight Demonstration of Electrostatic Thruster Under Micro-Gravity Shin SATORI*, Hiroyuki MAE**, Hiroyuki OKAMOTO**, Ted Mitsuteru SUGIKI**, Yoshinori AOKI # and Atsushi NAGATA # * Hokkaido Institute of
More informationAir Force Research Laboratory
Air Force Research Laboratory Air Force Research Laboratory Plasma Excited Oxygen Effects on Combustion and Perspectives on Applications to High-Speed Propulsion Date: 10 November 2011 Integrity Service
More informationChapter 7 Rocket Propulsion Physics
Chapter 7 Rocket Propulsion Physics To move any spacecraft off the Earth, or indeed forward at all, there must be a system of propulsion. All rocket propulsion relies on Newton s Third Law of Motion: in
More informationarxiv: v1 [physics.plasm-ph] 16 May 2018
Two-dimensional Modeling of the Hall Thruster Discharge with Non-uniform Propellant Supply in Azimuth Rei Kawashima a,, Junhwi Bak a, Kimiya Komurasaki a, Hiroyuki Koizumi b a Department of Aeronautics
More informationSOLAR ROCKET PROPULSION Ground and Space Technology Demonstration. Dr. Michael Holmes, AFRL/PRSS
SOLAR ROCKET PROPULSION Ground and Space Technology Demonstration Dr. Michael Holmes, AFRL/PRSS Solar Thermal Propulsion Concept Parabolic Mirror Sun Create thrust by collecting and focusing sunlight to
More informationEnergy-spread measurement of triple-pulse electron beams. based on the magnetic dispersion principle
nergy-spread measurement of triple-pulse electron beams based on the magnetic dispersion principle Yi Wang, Qin Li, Zhiyong Yang, Huang Zhang, Hengsong Ding, Anmin Yang, Minhong Wang Key Laboratory of
More informationPROPULSIONE SPAZIALE. Chemical Rocket Propellant Performance Analysis
Chemical Rocket Propellant Performance Analysis Sapienza Activity in ISP-1 Program 15/01/10 Pagina 1 REAL NOZZLES Compared to an ideal nozzle, the real nozzle has energy losses and energy that is unavailable
More informationFigure 1, Schematic Illustrating the Physics of Operation of a Single-Stage Hall 4
A Proposal to Develop a Double-Stage Hall Thruster for Increased Efficiencies at Low Specific-Impulses Peter Y. Peterson Plasmadynamics and Electric Propulsion Laboratory (PEPL) Aerospace Engineering The
More informationdetailed contents Unit One Describing Failing Objects and Projectile Physics, the Fundamental Science 1 The Newtonian Revolution 17
r detailed contents L Preface x Acknowledgments xvi Secrets to Success in Studying Physics xvii Failing Objects and Projectile 3.1 Acceleration Due to Gravity 39 3.2 Tracking a Falling Object 42 Motion
More information16855 North Chase Drive, Houston Texas (682) Ping Lu
16855 North Chase Drive, Houston Texas 77060 (682) 234-8150 pilu@eagle.org Researcher & Engineer II, Corporate Offshore Technology, American Bureau of Shipping Research Interests & Expertise Numerical
More informationSmall-Sized Laser Thruster for Attitude Control and Trajectory Control of Satellite
IOSR Journal of Polymer and Textile Engineering (IOSR-JPTE) e-issn: 2348-019X, p-issn: 2348-0181, Volume 4, Issue 5 (Sep. - Oct. 2017), PP 44-56 www.iosrjournals.org Small-Sized Laser Thruster for Attitude
More informationPropulsion Systems Design
Propulsion Systems Design Rocket engine basics Survey of the technologies Propellant feed systems Propulsion systems design 1 2011 David L. Akin - All rights reserved http://spacecraft.ssl.umd.edu Propulsion
More informationPROGRESS ON THE DEVELOPMENT OF A PULSED PLASMA THRUSTER FOR THE ASTER MISSION
PROGRESS ON THE DEVELOPMENT OF A PULSED PLASMA THRUSTER FOR THE ASTER MISSION IEPC-2013-318 Presented at the 33rd International Electric Propulsion Conference, The George Washington University Washington,
More informationResearch and Development of High-Power, High-Specific-Impulse Magnetic-Layer-Type Hall Thrusters for Manned Mars Exploration
Research and Development of High-Power, High-Specific-Impulse Magnetic-Layer-Type Hall Thrusters for Manned Mars Exploration IEPC-2015-151 /ISTS-2015-b-151 Presented at Joint Conference of 30th International
More informationPole-piece Interactions with the Plasma in a Magnetic-layertype Hall Thruster
Pole-piece Interactions with the Plasma in a Magnetic-layertype Hall Thruster IEPC-2017-426 Presented at the 35th International Electric Propulsion Conference Georgia Institute of Technology Atlanta, Georgia
More informationNumerical Simulation of Tail Flow Field of Four - Nozzle Solid Rocket Engine
Journal of Physics: Conference Series PAPER OPEN ACCESS Numerical Simulation of Tail Flow Field of Four - Nozzle Solid Rocket Engine To cite this article: Bailin Zha et al 2018 J. Phys.: Conf. Ser. 1064
More information