This 5 day executive program is about how to build innovation culture within an organization. It gives you a unique opportunity to immerse into the startup ecosystem. Sample Unveiling Program' title='Sample Unveiling Program' />Final Program. Organized Sessiono 1 1 Interorbital and Interplanetary Transportation with EP 1. Session Date. June 6 Tue 9 2. Issuu is a digital publishing platform that makes it simple to publish magazines, catalogs, newspapers, books, and more online. Easily share your publications and get. Room. Pearl Room BChairpersons. Masayuki Takahashi Tohoku University, JapanHitoshi Kuninaka JAXA, Japan2. Nuclear Electric Propulsion to EUROPA and MARSFrank Jansen. Tim Brandt. 1, Volker Maiwaldt. Frdric Masson. 2, Stephane Oriol. Jean Claude Worm. Emmanouil Detsis. Francois Lassoudierre. Richard Granjon. 5, Maria Cristina Tosi. Simona Ferraris. 6, Anatoly S. Koroteev. 7, Alexander V. Semenkin. 7, Alexander Solodukhin. Tim Tinsley. 8, James Ap. Findlay. 8, Zara Hodgson. Lamartine Nogueira Frutuoso Guimares. DLR Institute of Space Systems, Bremen, Germany, 2. CNES, Paris, France, 3. European Science Foundation, Strasbourg, France, 4. Airbus Safran Launchers, Vernon, France, 5. Auto B V3 Crack. Sagem Dfense Scurit, Valence, France, 6. Thales Alenia Space, Torino, Italy, 7. Keldych Research Centre, Moscow, Russia, 8. National Nuclear Laboratory, Sellafield, United Kingdom, 9. Instituto de Estudos Avanados, So Jos dos Campos, Brazil. Return Trajectory of Martian Moons e. Xplorer by Way of Chemical Electric Hybrid Propulsion. Makoto Horikawa. 1, Kazutoshi Takemura. Takanao Saiki. 3, Yasuhiro Kawakatsu. Hiroaki Yoshimura. Department of Applied Mechanics, Waseda University, Tokyo, Japan, 2. Department of Applied Mechanics and Aerospace Engineering, Waseda University, Tokyo, Japan, 3. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan. Highlights of Electric Sail Propulsion Efforts at NASAs Marshall Space Flight Center. Bruce M Wiegmann. Andy Heaton. 1, Michal Bangham. Robert Hoyt. 21. Marshall Space Flight Center, NASA, USA, 2. Tethers Unlimited, Inc., 3. Bangham Engineering, Inc. Dynamics of Single Charged Wire for Solar Wind Electric Sail. Fei Liu, Quan Hu, Jingrui Zhang, Keying Yang, Yanyan Li. School of Aerospace Engineering, Beijing Institute of Technology, Chinao 1 2 Interorbital and Interplanetary Transportation with EP 2. Session Date. June 6 Tue 1. Room. Pearl Room BChairpersons. Frank Jansen DLR, GermanyHiroyuki Koizumi The University of Tokyo, Japan2. Investigation of Scaling Laws for Electrical Thrusters by Use of Particle in Cell Simulations. Tim Brandt. 1,3,4, Ralf Schneider. Julia Duras. 2,6, Daniel Kahnfeld. Franz Georg Hey. 5, Holger Kersten. Frank Jansen. 1, Nils Haverland. Jonas Pawlik. 7, Claus Braxmaier. DLR, Institute of Space Systems, Bremen, Germany, 2. Institute of Physics, Ernst Moritz Arndt University Greifswald, Greifswald, Germany, 3. Center of Applied Space Technology an Microgravity, University of Bremen, Bremen, Germany, 4. Institute of Experimental and Applied Physics, University of Kiel, Kiel, Germany, 5. Airbus Defence and Space, Claude Dornierstrae 1, Immenstaad, Germany, 6. Department of Applied Mathematics, Physics and Humanities, Nuremberg Institute of Technology, Nuremberg, Germany, 7. University of Bremen, Germany. Development of a Numerical Tool for Hall Thruster Plume and Spacecraft Interaction Analysis. Takanobu Muranaka. Yasutaka Inanaga. School of Engineering, Chukyo University, Nagoya, Japan, 2. Where Is Oppo Serial Number/ Download. Advanced Technology R D Center, MELCO, Amagasaki, Japan. Two Head Operations of Hall Thruster. Tomohiro Kita, Takeshi Miyasaka, Masahiro Sakoda, Yoshimi Miyake, Kazuya Oishi, Ryo Kawamura, Yuki Mamiya, Kohei Kurita, Hiroki Kanie, Makoto Asahara. Gifu University, Japano 2 1 Launch Vehicle for Small Spacecrafts 1Session Date. June 6 Tue 9 0. Room. Meeting Room 7. Chairpersons. Kenji Fujii JAXA, JapanShigeru Aso Kyushu University, Japan2. Compact and High Performance Rocket Design of Epsilon and Future Prospect of Solid Propellant Launch Vehicles. Yasuhiro Morita. Japan Aerospace Exploration Agency JAXA, SagamiharaTsukuba, Japan. Epsilon Launch Vehicle Second Flight and its Evolutions. Tatsuya Kanechika. Yasunobu Segawa. 1, Kazuhiro Yagi. Takayuki Imoto. 21. IHI AEROSPACE Co. Ltd. IA, Japan, 2. Institute of Space and Astronautical Science, JAXA, Japan. Development and Flight Results of Solid Propulsion System for Enhanced Epsilon Launch Vehicle. Koki Kitagawa. 1, Shinichiro Tokudome. Keiichi Hori. 1, Haruhito Tanno. Nobuyuki Nakano. 21. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2. Solid Propulsion Office, Rocket Systems Department., IHI Aerospace, Tomioka, Japan. Development and Flight Results of Structure Subsystem for Enhanced Epsilon Launch Vehicle. Hiroshi Ikaida. 1, Kyoichi Ui. Ryoma Yamashiro. 1, Takayuki Imoto. Yasuhiro Morita. 21. Tsukuba Space Center, JAXA, Tsukuba, Japan, 2. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japano 2 2 Launch Vehicle for Small Spacecrafts 2Session Date. June 6 Tue 1. 1 0. Room. Meeting Room 7. Chairpersons. Atsushi Murakami IHI AEROSPACE Co., Ltd., JapanKazuhide Mizobata Muroran Institute of Technology, Japan2. Conceptual Study of Japans Future Solid Rocket System. Ryoma Yamashiro. 1, Shinichiro Tokudome. Yasuhiro Saitoh. 1, Takayuki Yamamoto. Yoshitaka Mochihara. Hiroki Ikaida. 11. Tsukuba Space Center, JAXA, Tsukuba, Japan, 2. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan. Initial Guess Generation Strategies for Spaceplane Trajectory Optimisation. How To Get A Medical Marijuana Growing License In Canada. Federico Toso, Christie Maddock. Aerospace Centre of Excellence, University of Strathclyde, Glasgow, United Kingdom. The Low Cost Rocket with Low Melting Temperature Thermoplastic Propellant. Hikaru Isochi. 1, Hikaru Otabe. Tsutomu Uematsu. 1, Nobuji Kato. Keiichi Hori. 3, Yasuhiro Morita. Ryojiro Akiba. 41. Uematsu Electric Co. Ltd., Akabira, Japan, 2. Katazen Corporation, Aichi, Japan, 3. The Institute of Space and Astronautical Science, Sagamihara, Japan, 4. Hokkaido Aerospace Science and Technology Incubation Center, Sapporo, Japano 3 1 Future Space Transportation System 1Session Date. June 6 Tue 1. 4 0. Room. Meeting Room 7. Chairpersons. Wataru Sarae JAXA, JapanTakahiro Fujikawa Kyushu Institute of Technology, Japan2. Technical and Flight Demonstrations for Reusable Launch Vehicle. Satoshi Nonaka, Takashi Ito, Yoshifumi Inatani. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan. Trajectory Optimization for a Reusable Sounding Rocket. Shunsuke Sato. 1, Takayuki Yamamoto. Takahiro Nakamura. Satoshi Nonaka. 21. Research Unit 1, Research and development Directorate, JAXA, Sagamihara, Japan, 2. Department of Space Flight Systems, Institute of Space and Astronautical Science ISAS, JAXA, Sagamihara, Japan. Numerical Analysis on Reusable Rocket Aerodynamics with Reduced Yaw Force Configurations. Ayano Inatomi. 1, Keiichi Kitamura. Satoshi Nonaka. 21. Yokohama National University, Yokohama, Japan, 2. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan. Computational Study on Finned Reusable Rocket during Turnover. Takuya Aogaki. 1, Keiichi Kitamura. Satoshi Nonaka. 21. Graduate School of Engineering, Yokohama National University, Kanagawa, Japan, 2. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan. Anomaly Detection Configured as a Combination of State Observer and Mahalanobis Taguchi Method for a Rocket Engine. Yusuke Maru. 1, Hatsuo Mori. Takashi Ogai. 2, Noriyoshi Mizukoshi. Shinsuke Takeuchi. Takayuki Yamamoto. Tsuyoshi Yagishita. Satoshi Nonaka. 11. Institute of Space and Astronautical Science, JAXA, Sagamihara, Japan, 2. IHI Corporation, Tokyo, Japano 3 2 Future Space Transportation System 2Session Date. June 6 Tue 1. 6 0. Room. Meeting Room 7.