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IAF Space Propulsion Symposium 2019 IAF Space Propulsion Symposium 2019 Held at the 70th International Astronautical Congress (IAC 2019) Washington, DC, USA 21 -25 October 2019 Volume 1 of 2 ISBN: 978-1-7138-1491-7 Printed from e-media with permission by: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 Some format issues inherent in the e-media version may also appear in this print version. Copyright© (2019) by International Astronautical Federation All rights reserved. Printed with permission by Curran Associates, Inc. (2020) For permission requests, please contact International Astronautical Federation at the address below. International Astronautical Federation 100 Avenue de Suffren 75015 Paris France Phone: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 www.iafastro.org Additional copies of this publication are available from: Curran Associates, Inc. 57 Morehouse Lane Red Hook, NY 12571 USA Phone: 845-758-0400 Fax: 845-758-2633 Email: [email protected] Web: www.proceedings.com TABLE OF CONTENTS VOLUME 1 PROPULSION SYSTEM (1) BLUE WHALE 1: A NEW DESIGN APPROACH FOR TURBOPUMPS AND FEED SYSTEM ELEMENTS ON SOUTH KOREAN MICRO LAUNCHERS ............................................................................ 1 Dongyoon Shin KEYNOTE: PROMETHEUS: PRECURSOR OF LOW-COST ROCKET ENGINE ......................................... 2 Jérôme Breteau ASSESSMENT OF MON-25/MMH PROPELLANT SYSTEM FOR DEEP-SPACE ENGINES ...................... 3 Huu Trinh 60 YEARS DLR LAMPOLDSHAUSEN – THE EUROPEAN RESEARCH AND TEST SITE FOR CHEMICAL SPACE PROPULSION SYSTEMS ....................................................................................... 9 Anja Frank, Marius Wilhelm, Stefan Schlechtriem FIRING TESTS OF LE-9 DEVELOPMENT ENGINE FOR H3 LAUNCH VEHICLE ................................... 24 Takenori Maeda, Takashi Tamura, Tadaoki Onga, Teiu Kobayashi, Koichi Okita DEVELOPMENT STATUS OF BOOSTER STAGE LIQUID ROCKET ENGINE OF KSLV-II PROGRAM ........................................................................................................................................................ 30 Soon-Young Park, Yoonwan Moon, Hwan-Seok Choi, Chang Ho Choi, Sangyeop Han, Yeoung-Min Han, Jinhan Kim DEVELOPMENT TESTS OF RD815 ENGINE PREBURNER DEMONSTRATOR ...................................... 44 Alexandr Prokopchuk, Volodymyr Shulga, Andrew Kukhta, Yevgen Strelchenko ANOMALY DETECTION OF LIQUID PROPELLANT ROCKET ENGINE USING SYSTEM INVARIANT ANALYSIS TECHNOLOGY ..................................................................................................... 49 Masaki Sato, Tomoyuki Hashimoto, Masanori Shiga, Tomoya Soma, Toshiya Kimura, Shinichi Moriya VINCI UPPER STAGE ENGINE QUALIFICATION FOR ARIANE 6 .......................................................... 59 Erwam Humbert, Patrick Danous MAIN RESULTS FROM ORION EUROPEAN SERVICE MODULE PROPULSION SUBSYSTEM QUALIFICATION TESTING ................................................................................................... 66 Markus Jäger WATER PROPULSION - THE ULTIMATE GREEN TECHNOLOGY .......................................................... 73 Ulrich Gotzig, Malte Wurdak, Nicholas Harmansa, Zachary Lynn NUMERICAL STUDY ON PERFORMANCES OF AN ELECTRIC PUMP-FED CYCLE ROCKET ENGINE ............................................................................................................................................ 80 Toshiya Kimura, Mitsuru Shimagaki, Hitoshi Naito, Tomoyuki Hashimoto, Masaki Sato, Naoki Nagao PRELIMINARY STUDY ON EXPANDER CYCLE METHANE ENGINE FOR POST-KSLV 2 PROGRAM ........................................................................................................................................................ 89 Cheulwoong Kim, Hayoung Lim, Gyusik Cho, Woongrae Roh QUALIFYING AN ADDITIVELY MANUFACTURED LIQUID ROCKET ENGINE FOR HOT- FIRE READINESS ............................................................................................................................................ 95 Nihar Patel, Venkata Devalaraju, Sean Standbridge, Paul Prochnicki, Suyash Ghirnikar, Andrew Antony PROPULSION SYSTEM (2) HYBRID PROPULSION: INNOVATIVE FORMULATIONS BASED ON PARAFFIN / ETHANOL INTERACTION ........................................................................................................................... 109 Rene Gonçalves, Cristiane Martins, Leonardo Gouvêa, Paulo Gabriel Cunha Martins, Koshun Iha, Jose Rocco IMPACT ASSESSMENT OF PROPELLANT ENTRAPMENT IN LOOSE FLAP CAVITY ON BALLISTIC PERFORMANCE AND VALIDATION THROUGH HOT TEST OF SOLID ROCKET BOOSTER ....................................................................................................................................... 110 Arun Raj, A Shaji, V Mahesh, Levin G, Eswaran V KEYNOTE: OMEGA LAUNCH VEHICLE ................................................................................................... 111 Kent Rominger ARIANE 6 AND VEGA-C PROGRAMS: THE P120C SRM NOZZLE QUALIFICATION ........................ 112 Eric Gautronneau PERFORMANCE EVALUATION OF 4D CARBON-CARBON THROAT INSERT THROUGH HOT TEST OF SOLID MOTOR ..................................................................................................................... 125 Shubham Maurya, Shaji A, Arun Raj, V Mahesh, Jhon Paul, Krishnadasan C K, Levin G, Siva Kumar Ganesan DESIGN AND DEVELOPMENTAL CHALLENGES OF SLOW BURNING SOLID BOOSTER FOR SUB-ORBITAL HYPER SONIC RE-ENTRY EXPERIMENT ............................................................. 130 Achutananda Parhi, Mahesh V, Levin G, Eswaran V PERFORMANCE AND ENVIRONMENTAL IMPACT PREDICTION OF SRMS. ROAD MAP FOR RELIABLE DATASET OF PARTICLES IN PLUME ........................................................................... 131 Stefania Carlotti, Filippo Maggi, Luciano Galfetti ANALYSIS OF SOLID PROPELLANT COMBUSTION USING IMAGE PROCESSING TECHNIQUES ................................................................................................................................................. 138 Sonali Sinha Roy, Selvakumaran T MARS ASCENT VEHICLE (MAV) PRELIMINARY ARCHITECTURE ASSESSMENT OVERVIEW ..................................................................................................................................................... 149 Angie Jackman A STUDY ON NEW HYBRID ROCKET ENGINE WITH MULTI-SECTION SWIRL INJECTION AND AFT COUNTER-SWIRL INJECTION METHOD ........................................................... 160 Shigeru Aso REAL-TIME REGRESSION RATE MEASUREMENT OF AN ADDITIVE-MANUFACTURED FUNCTIONAL HYBRID ROCKET FUEL .................................................................................................... 169 Kohei Ozawa, Han-Wei Wang, Takuro Yoshino, Nobuyuki Tsuboi COST-EFFECTIVE HYBRID ROCKET LAUNCH VEHICLE OF TAIWAN .............................................. 179 Yen-Sen Chen GREEN FUELS FOR ROCKET PROPULSION: CURRENT STATUS AND FUTURE PERSPECTIVES OF PARAFFIN-BASED FORMULATIONS ..................................................................... 186 Riccardo Bisin, Sebastiano Alberti, Alberto Verga, Christian Paravan, Luciano Galfetti DYNAMIC RESPONSE OF THRUST MODULATION IN HYBRID ROCKET FOR VTVL PROPULSION SYSTEM ................................................................................................................................. 198 Heesang Chae, Donghoon Chae, Changjin Lee PERFORMANCE ANALYSIS OF N2O/CO2 OXIDIZER MIXTURE WITH PARAFFIN BASED MICRO-ALUMINUM FUEL FOR MARS ASCENT VEHICLES ................................................................. 205 Ozan Kara, Arif Karabeyoglu, Büsra Kahraman, Busra Nimet Eren, Hakki Karakas PROPULSION TECHNOLOGY (1) NUMERICAL INVESTIGATION OF ROTATING STALL IN HIGH PRESSURE FUEL PUMP OF SEMICRYOGENIC ENGINE ................................................................................................................... 220 Khalid Rashid, Deepak K. Agarwal, John T Tharakan, Sunil Kumar S. KEYNOTE: PROPULSION TECHNOLOGY DEVELOPMENT ACTIVITIES AT NASA ......................... 221 George Schmidt FEASIBILITY STUDY ON ELECTRIC PUMPS FEEDING PROPELLANTS TO A ROCKET ENGINE ........................................................................................................................................................... 222 Mitsuru Shimagaki, Toshiya Kimura, Tomoyuki Hashimoto, Satoshi Takada, Hayato Ikeda, Shuiciro Honda, Kozo Matake HOT-FIRE TEST OF THE ETID SANDWICH NOZZLE EXTENSION FOR FUTURE UPPER STAGE ENGINE APPLICATIONS ................................................................................................................ 230 Klas Lindblad, Eva Stenström, Darri Kristmundsson, Jan Östlund, Alexandre Capitao Patrao CHANNEL WALL NOZZLE MANUFACTURING TECHNOLOGY ADVANCEMENTS FOR LIQUID ROCKET ENGINES ......................................................................................................................... 235 Paul Gradl, Christoper Protz PROGRESS IN ADDITIVELY MANUFACTURED COPPER-ALLOY GRCOP-84, GRCOP-42, AND BIMETALLIC COMBUSTION CHAMBERS FOR LIQUID ROCKET ENGINES ............................ 251 Paul Gradl, Christoper Protz, David Ellis, Sandy Greene THE DEVELOPMENT PROCESS FOR A SINGLE-PART ADDITIVELY MANUFACTURED LIQUID ROCKET ENGINE INJECTOR WITH AS-PRINTED ORIFICES .................................................. 265 John Targonski, Michael Moruzzi LASER METAL DEPOSITION TECHNOLOGY FOR LE-9 ENGINE......................................................... 266 Akira Ogawara, Masaki Adachi, Koichi Okita, Hideto Kawashima FLAME INITIATION INSIDE THE GAS TORCH
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