Chairpersons Luigi De Luca (Politecnico di Milano) Paul Kuentzmann (ONERA) Anatolij Koroteev (Keldysh Research Center) Alexander S. Rudakov (CIAM) Session 5.13 - Diagnostic Techniques Monday Afternoon/ 4 July 2005  Chaired by W. Zinner, EADS-ST and V. Kim, MAI Pushkin hall 5.13.01 14h00    Methods of Functional Diagnostic of LPRE on the Basis of Mathematical Models    V. Chvanov, D. Martirosov, NPO Energ., Khimky, RU         5.13.02 14h25   Vulcain 2 Flight Load Simulation Device (LSD)   A. Haberzettl, D. Gundel, H. Zimmermann, DLR, Hardthausen, DE E Poulin, J.-F. Delange, Y. Prevot, SNECMA, Vernon, FR M. Kesteman, CNES, Evry, FR         5.13.04 14h50   The Nanobalance Test-Stand for Micro-Thrust Measurements : Digital Control and Data Processing   L. Massotti, E. Canuto, Politecnico di Torino, IT         5.13.05 15h15   P4.1 Test Facility for Altitude Simulation of VINCI Engine, Bench Development   K. Schafer, C. Bohm, H. Krommuller, R. Stark, H. Zimmermann, DLR, Hardthausen, DE         5.13.06 15h40   Measurement Techniques for Investigation of Heat Transfer Processes at European Research and Technology Test Facility P8   D. Suslov, A. Woschnak, D. Greuel, M. Oschwald, DLR, Hardthausen, DE         5.13.07 16h05   Test Platform of LOx/Ethanol Rocket Steam Generators at DLR Lampoldshausen   G. Kruehsel, K. Schafer, DLR, Hardthausen, DE Session 5.1 - SRM: Motors or Components Tuesday Morning/ 5 July 2005  Chaired by G. Mastrangelo, Europropulsion and V. Mironov, Keldysh Research Center Pushkin hall 5.01.01 9h00   Performance Comparison Between Two Different Injector Configurations in a Hybrid Rocket   A. Russo Sorge, C. Carmicino, Univ. di Napoli, IT         5.01.02 9h25   Effect of Induced Swirl Flow on Regression Rate of Hybrid Rocket Fuel by Helical Grain Configuration   C. Lee, J. Lee, Y. Byun, University of Konkuk, Seoul, KR S. Lee, Hanwha Corp., KR         5.01.03 9h50   Hybrid Rocket Engines: the Benefits and Prospects   A.M. Gubertov, R.Gollender, V. Mironov, N. Volkov, N. Davydenko, KeRC, Moscow, RU         5.01.04 10h15   A New Concept to Reduce SRM Pressure Oscillations: the 3D Frontal Thermal Protection   M. Telara, Avio, Roma, IT T. Pevergne, L. Jacques, Ph. Le Helley, D. Ribereau, SNECMA, Le Haillan, FR B. Gondouin, N. Cesco, CNES, FR         5.01.05 10h40    Numerical Simulation of Pressure Oscillations in Solid Rocket Motors    F. Stella, F. Paglia, M. Giangi, Univ. di Roma "La Sapienza", IT M. Telara, Avio Spa, Colleferro, IT         5.01.06 11h05   Pressuring Gas Effects on Pressure Oscillations during the Ignition Transient of SRM   B. Favini, M. Di Giacinto, Universita di Roma "La Sapienza", IT F. Serraglia, ESA-ESRIN, IT A. Neri, AVIO, IT         5.01.07 11h30   Frontal Thermal Protection Evolution by Means of a Fluid Structure Interaction Approach : Coupled Numerical Simulation   M. Telara, Avio Spa, Colleferro, Roma, IT F. Stella, F. Paglia, M. Giangi, Aero. Univ. di Roma "La Sapienza", IT         5.01.08 11h55   P80 FW SRM Low Torque Flex-Seal Development - A Cost Effective Approach from Design to Manufacturing   C. Descamps, M. Daurat, G. Rousseau, E. Gautronneau, SNECMA, Le Haillan, FR         5.01.09 12h20   Gas Dynamics and Heat Exchange in Rocket Engines   D. Borisov, L. Volkova, A. Gubertov, V. Mironov, KeRC, Moscow, RU Session 5.4 - LRE: Cryogenic Combustion Tuesday Morning/ 5 July 2005  Chaired by O. Haidn, DLR and A. Rudakov, CIAM Checkov Hall 5.04.01 9h00    An Eulerian Model for LOx/GH2 Shear-Coaxial Jet Atomization and Combustion    N. Meyers, F. Dupoirieux, M. Habiballah, ONERA, Palaiseau, FR         5.04.02 9h25   Experiments and Simulations of LOx/CH4 Combustion at High Pressures   S. Candel, G.Singla, P. Scouflaire, C. Rolon, ECP, Chatenay-Malabry, FR S. Zurbach, J.-L. Thomas, SNECMA Moteurs, Vernon, FR         5.04.03 9h50   Steady-State High Pressure LOx/H2 Rocket Engine Combustion   J. Smith, M. Bechle, D. Suslov, M. Oschwald, O. Haidn, DLR, Hardthausen, DE G. Schneider, Univ. of Adelaide, AU         5.04.06 10h40   CARS Spectroscopy of CH4 for Temperature Measurements in a Cryogenic Combustion Chamber   E. Bertseva, F. Grisch, M. Habiballah, ONERA, Palaiseau, FR H. Berger, F. Chaussard, T. Gabard, E. Jourdanneau, R. Saint-Loup, L.P.U.B., Dijon, FR         5.04.07 11h05   PLIF of OH in High Pressure Cryogenic LOx/GH2 Jet Flames   G. Singla, P. Scouflaire, C. Rolon, S. Candel, CNRS, Chatenay-Malabry, FR         5.04.08 11h30   Characterization of Cryogenic Propellants Ignition on the MASCOTTE Test Rig; Preliminary Results   L. Vingert, P. Gicquel, M. Barat, ONERA, Palaiseau, FR J. Sender, DLR, Lampoldshausen, DE Session 5.2 - SRM: Novel Ingredients Tuesday Afternoon/ 5 July 2005  Chaired by Y. Fabignon, ONERA and V. Zarko, Institute of Chemical Kinetics & Combustion Pushkin hall 5.02.1 14h00    Universal Concept of the Spatial Periodic Micro Structures Excitation at the Energetic Materials Transient Combustion as a Way for Improvement of the Solid Propulsion Technologies    A. Lukin, Institute of Applied Mechanics, Izhevsk, RU         5.02.02 14h25   Energetic Materials Laboratory Tests Related to Motor Slow Cook-off Behaviour   B. D'Andrea, F. Lillo, G. Marcelli, A. Dell'Orco, AVIO Propulsione Aerospaziale, Rome, IT         5.02.03 14h50   New Generation of Cheap and Ecologically Safe Solid Propellants for Space Applications   V. Babuk, Baltic State Technical University, St Petersburg, RU A. Glebov, I. Dolotkazin, A. Dosychev, L.-T. Deluca, Politecnico di Milano, IT B. D'Andrea, Avio, Colleferro, IT A. Vorozhtsov, Tomsk State Univ. RU G. Klyakin, South Russia State Techn, Univ., Novocherkassk, RU         5.02.04 15h15   Some Aspects of Combustion Modeling for Solid Energetic Materials   Y. Fabignon, A. Bizot, V. Borie, V. Giovangigli, N. Meynet, J.-F. Trubert, ONERA, Palaiseau, FR         5.02.05 15h40   HNF Flame - Alternative Mechanism of Gas Phase Reactions   N.-E. Ermolin, Instit. of Theorical and Applied Mech., Novosibirsk, RU V. Zarko, ITAM, Novosibirsk, RU H. Keizers, TNO Prins Maurits Lab., Rijswijk, NL         5.02.06 16h05   Combustion Characterisation of Hydrazinium Nitrate/Energetic Binder/Alex Based Model Propellants   V. Zarko, V. Simonenko, Inst. of Chemical Kinetics and Combustion, Novosibirsk, RU G. Anisiforov, A. Aparin, Boreskov Inst. of Catalysis, RU         5.02.07 16h30   Physical and Ballistic Characterisation of AlH3 Based Space Propellants   L.-T. DeLuca, L. Galfetti, F. Severini, L. Rossettini, Politecnico di Milano, Milano, IT L. Meda, G. Marra, Inst. G. Donegani, Novara, IT B.D'Andrea, Avio, Colleferro, IT V. Weiser, ICT, Pfinztal, DE M. Calabro, The Inner Arch., Villennes, FR A.-B. Vorozhtsov, A.-A. Glazunov, G.-J. Pavlovets, Tomsk State Univ., RU Session 5.5 - LRE: Particular Technologies Tuesday Afternoon/ 5 July 2005  Chaired by D. Haeseler , EADS-ST and A. Rudakov, CIAM Checkov Hall 5.05.01 14h00    Hypergolic Ignition of Catalytically Promoted Fuels with Rocket Hydrogen Peroxide    T. Pourpoint, W. Anderson, Purdue Univ., West Lafayette, US         5.05.02 14h25   Combined RANS/PDF Computation of Auto-Ignition and Soot-Formation in Diesel Like Spray   M. Gorokhovski, N. Baricault, CNRS, St-Etienne de Rouvray, FR         5.05.03 14h50   Numerical Simulation of a Quarter Wave Resonator Operation   A. Nicole, M. Habiballah, ONERA, Châtillon, FR         5.05.04 15h15   Temperature Dependence of Material Properties and Its Influence on the Thermal Distribution in Regeneratively Cooled Combustion Chamber Walls   M. Oschwald, D. Suslov, A. Woschnak, DLR, Hardthausen, DE         5.05.05 15h40   Spray and Combustion Characteristics of Aluminized Gelled Fuels with an Impinging Jet Injector   H. Ciezki, J. Von Kampen, H. Ciezki, DLR, Hardthausen, DE F. Alberio, Politecnico di Milano, IT Session 5.3 - SRM: Metallized Formulations Wednesday Morning/ 6 July 2005  Chaired by B. D'Andrea, Avio and V. Babuk, Baltic State Technical University Pushkin hall 5.03.1 9h00    The Ballistic Characteristics of SP Containing Nanoaluminium and Dual Oxidizer (AP and stabilized AN)    A. Vorozhtsov, V. Arkhipov, S. Bondarchuk, N. Popok, IPCET, RU G. Klyakin, STU, Novocherkassk, RU V. Babuk, BSTU, St Petersburg, RU V. Kuznetsov, L. Revyagin, S. Volkov, TSU, Tomsk, RU L.-T. DeLuca, L. Galfetti, Politecnico di Milano, IT         5.03.02 9h25   Direct Numerical Simulation of Aluminium Agglomeration in Composite Solid Propellant Combustion   S.-A. Rashkovsky, Institute for Problems in Mechanics, Moscow, RU A. Iannetti, L.-T. Deluca, Politecnico di Milano, IT         5.03.04 10h15   HTPB/AP/AL Solid Propellants with Nanometric Aluminium   O. Orlandi, J.-F. Guéry, G. Lacroix, S. Chevalier, N. Desgardin, SME, FR         5.03.05 10h40   Complex Research of Al Nanopowders Produced by the Exploding Wire Method   V. Sedoi, L. Chemezova, Yu. Ivanov, M. Osmonaliev, Inst. of High Current Elctr., Tomsk, RU V. Ivanov, I. Sobolev, Inst.of Petrol. Chemistry RAS, Tomsk, RU         5.03.06 11h05   Pre and Post-Burning Analysis of Nano-Aluminized Solid Rocket Propellants   L. Galfetti, L.-T. DeLuca, F. Severini, G. Colombo, Politec.di Milano, IT L. Meda, G. Marra, Inst. G. Donegani, Novara, IT         5.03.07 11h30   Studies on the Burning of Complex Aluminum Particles   P. Escot, Ch. Chauveau, I. Gökalp, Labo. de Combustion et Syst. Réactifs, Orléans, FR E. Shafirovich, Purdue University, School of Chemical Engineering, USA Session 5.6 - LRE: Motors or Components Wednesday Morning/ 6 July 2005  Chaired by M. Pouliquen, SNECMA and A. Rudakov, CIAM Checkov Hall 5.06.01 9h00    HM7B Engine Transient Simulator with CARINS Tool    V. Leudière, J. Hebrard, G. Albano, CNES, Evry, FR         5.06.03 9h25   ARIANE 5 Launcher - Finite Element Modelling of a VULCAIN 1 Engine   V. Touchet, L. Appolloni, CNAM-CNES, FR         5.06.04 9h50   Numerical Simulation of the Working Process in Gas Generator on Propellant Components LOx + Gaseous Methane   G. Kalmykov, A. Larionov, D. Sidlerov, L. Yanchilin, Keldysh Research Center, Moscow, RU         5.06.05 10h15   Selection of Scheme and Parameters of Reusable LOx-Methane LPRE   I. Klepikov, NPO Energomash, Khimky, RU         5.06.06 10h40   Recent Investigations on Hydrocarbon Based Fuels for Future Propulsion Systems   C. Maeding, D. Preclik, D. Haesler, EADS-ST., Munich, DE         5.06.08 11h05   Simulation of Non-Stationary Thermal and Hydro-Gasdynamic Processes in LRE of Expander Cycle   L. Volkova, N. Volkov, I. Gurina, M. Filimonov, V. Mironov, KeRC, Moscow, RU Session 5.7 - Aero Engines: Ramjets and Scramjets Wednesday Afternoon/ 6 July 2005  Chaired by F. Falempin, MBDA and A. Rudakov, CIAM Pushkin hall 5.07.1 14h00   Three Mode Ramjet   V. Aleksandrov, D. Zhirnov, Yu. Mnatsakanyan, D. Moseev, A. Prohorov, CIAM, Moscow, RU         5.07.02 14h25   Combustion Experiments of Liquid Kerosene and Hydrogen/Methane Mixing in a Dual Mode Ramjet   O. Dessornes, ONERA, Palaiseau, FR M. Bouchez,Bourges, MBDA, FR         5.07.03 14h50   Air Breathing Propulsion for Space Launchers. A Minimum R&T Program Proposed for Europe   F. Falempin, M. Bouchez, MBDA, Châtillon, FR L. Serre, ONERA, Palaiseau, FR C. Bruno, Univ. of Roma " La Sapienza", IT P. Hendrick, Univ. Libre de Bruxelles, BE         5.07.04 15h15   Fuel Reforming for Scramjet Thermal Management and Combustion Optimization   E. Daniau, M. Bouchez, MBDA, Bourges, FR O. Herbinet, P.-M. Marquaire, CNRS-INPL, Nancy, FR N. Gascoin, P. Gillard, Labo.EES, Bourges, FR         5.07.05 15h40    Experimental and Numerical Investigation of Supersonic Reacting Hydrogen/Methane Jets in Hot Air Co-Flows    V. Quintilla, Ph. Magre, D. Scherrer, ONERA, FR P.-E. Destors, E. Dufour, MBDA, FR         5.07.06 16h05   LEA Flight Test Program - Status in 2005   F. Falempin, MBDA, Châtillon, FR L. Serre, ONERA, Palaiseau, FR         5.07.07 16h30   Numerical Simulation of Supersonic Combustion with CH4-H2 Fuel   D. Davidenko, I. Gokalp, CNRS, Orléans, FR E. Dufour, MBDA, Châtillon, FR P. Magre, ONERA, Palaiseau, FR         5.07.08 16h55   Modeling Studies of the Supersonic Combustion of the Primary Hydrocarbons and the Products of its Thermal Destruction with Air. Application to Hypersonic Vehicles   L. Bezgin, V. Kopchenov, A. Starik, N. Titova, CIAM, Moscow, RU         5.07.09 17h20   Some Gas Dynamic Aspects of Combustion in Supersonic Flow   O. Gouskov, M. Danilov, V. Kopchenov, CIAM, Moscow, RU Session 5.9 - Pulse Detonation Engines and Solar Power Wednesday Afternoon/ 6 July 2005  Chaired by C. Buongiorno, La Sapienza and by V. Kopchenov, CIAM Checkov Hall 5.09.01 14h00    Liquid Fueled Air Breathing PDE Demonstrator    S. Frolov, V. Aksenov, V. Basevich, Semenov Instit. of Chem. Physics , Moscow, RU         5.09.02 14h25   Numerical Modeling of Electrochemical Pulse Detonation Engine   I. Semenov, V. Markov, Inst. for Computer Aided Design, Moscow, RU S. Wojcicki, WSU, Pullman, US         5.09.03 14h50   Investigation of Pulse Detonation Engine Operation   V. Levin, Instit. for Auto. and Cont. Processes, Vladivostok, RU I. Semenov, V. Markov, RAS, Moscow, RU A. Khmelevski, MSU, Moscow, RU T. Zhuravskaya, S. Osinkin, Moscow Sta. Univ., RU         5.09.04 15h15   Pulsed and Rotating Detonation Propulsion Systems First Steps Towards Operational Engines   E. Daniau, MBDA, Bourges, FR F. Falempin, MBDA, Châtillon, FR F. Bykovskii, S. Zhdan, LIH, Novosibirsk, RU         5.09.06 16h05   Deflagration to Detonation Control by Non-Equilibrium Gas Discharges and Its Applications for Pulsed Detonation Engine   A. Starikovskii, V. Zhukov, Moscow Instit. of Physics and Tech., RU         5.09.07 16h30   Solar Power Propulsion System. Adaptation to ARIANE 5 and Preliminary Development Plan   D. Fiot, D. Iranzo-Greus, O. Gogdet, EADS-ST, Les Mureaux, FR A. Koroteev, Yu. Kochetkov, V. Akimov, N. Arkhangelsky, S. Popov Keldysh Research Center, Moscow, RU Session 5.8 -Aero Engines: Turbojets Thursday Morning/ 7 July 2005  Chaired by I. Gokalp, CNRS and A. Rudakov, CIAM Pushkin hall 5.08.01 9h00    Influences of Rotating Inlet Distortion on Compressor Stability Margin in the Light of Nonlinear Oscillation and Control Theories    J. Pismenny, Y. Levy, Technion, Haifa, IL         5.08.02 9h25   Application of 3D CFD Methods to the Analysis of Large Particles Ingestion to the Engine Inlet Located Near to the Aerodrome Surface   S. Krasheninnikov, D. Pudovikov, CIAM, Moscow, RU         5.08.04 10h15   NOx Emissions from Axially Staged Sector Combustor at Major Operating Conditions of the Next-Generation SST Engine in ESPR Project   S. Hayashi, H. Yamada, K. Shimodaira, M. Kobayashi, Japan Aero. Exploration Agency, Tokyo, JP T. Oda, H. Nimomiya, Kawasaki Heavy Ind. Ltd, Akashi, Hyogo, JP         5.08.05 10h40   Specific Problems of Micro Turbine for Micro Drones Application   C. Dumand, J. Guidez, M. Orain, V. Sabel'nikov, ONERA, Palaiseau, FR         5.08.06 11h05   The Use of Coanda's Motor Jet in Aircraft Propulsion   V. Stanciu, C. Pavel, University Politechnica of Bucharest, RO         5.08.07 11h30   CFD in the Design of an Ultra Micro Gas Turbine Combustion Chamber   J. Trilla, D. Verstraete, N. De Bruyn, Royal Military Academy of Belgium, BE P. Hendrick, ULB, Bruxelles, BE Session 5.10 - In-Space: Electric Propulsion Thursday Morning/ 7 July 2005  Chaired by E. Chesta, CNES and O. Gorshkov, Keldysh Research Center Checkov Hall 5.10.01 9h00   Problems of the High Specific Impulse Stationary Plasma Thruster Development   V. Kim, V. Kozlov, G. Popov, A. Skrylnikov, MAI, Moscow, RU         5.10.02 9h25   Electric Propulsion Systems of the Spacecraft: the State of the Art in Development and Outlooks for Progress   O. Gorshkov, A. Vasin, V. Muravlev, A. Shagayda, Keldysh Research Center, Moscow, RU         5.10.03 9h50   Experimental Setup of a Pulsed MPD Thruster at IRS   A. Nawaz, M. Auweter-Kurtz, G. Herdrich, H. Kurtz, Univ. of Stuttgart, DE         5.10.04 10h15   Small Electric Propulsions Developed by RIAME MAI   G. Popov, N. Antropov, V. Kim, V. Kozlov, A. Skrylnikov, MAI, Moscow, RU         5.10.05 10h40    Initial Design of a 1N Multipropellant Resistojet DUR-1   K.-J.-A. Rycek, B.-T.-C. Zandbergen, Delft Univ. of Tech., NL         5.10.06 11h05   Innovative Hybrid Micro-Arcjet   M. Pessana, Alenia Spazio, IT F. Turco, Politecnico di Torino, IT         5.10.07 11h30   Pulsed Plasma Thruster Option for Myriade Deorbiting   N. Pillet, B. Pouilloux, P. Pelipenko, J. Folliard, F. Darnon, E. Chesta, P. Bousquet, F. Alby, CNES, Toulouse, FR N. Antropov, G. Diakonov, V. Jakovlev, M. Orlov, P. Trubnikov, V. Tyutin, RIAME, Moscow, RU         5.10.08 11h55   Double Stage Hall Effect Thruster Development Activities at SNECMA    M. Prioul, SNECMA Moteurs, Moissy-Cramayel, FR A. Bugrova, V. Kharchevnikov, A. Desyatskov, MIREA, Moscow, RU J.-P. Bœuf, C. Boniface, CNRS-CPAT, Univ. P. Sabatier, Toulouse, FR         5.10.09 12h20   Development Status of the SNECMA PPS® Hall-Effect Thruster   O. Duchemin, N. Cornu, SNECMA Moteurs, Moissy-Cramayel, FR F. Darnon, CNES, Toulouse, FR D. Estublier, ESA ESTEC, Noordwijk, NL Session 5.12 - Fundamentals and Plasma Thursday Afternoon/ 7 July 2005  Chaired by J.-C. Rolón, Ecole Centrale de Paris and R. Rizakhanov, Keldysh Research Center Pushkin hall 5.12.01 14h00   Theoretical Predictions of Hydrogen Recombination on Zirconia   F. Finamore, C. Bruno, Universita di Roma "La Sapienza", IT         5.12.02 14h25   Automatic Generation of Skeletal Kinetics for HC Fuels in LRE   M. Valorani, F. Creta, Universita di Roma "La Sapienza", IT D.-A. Goussis, GR H.-N. Najm, SNL, Livermore, US         5.12.05 14h50    Propane-Air Mixture Ignition by a Sequence of Nanosecond Pulses   S. Pancheshnyi, D.-A. Lacoste,A. Bourdon, C.-O. Laux, Ecole Centrale Paris, Chatenay-Malabry, FR         5.12.06 15h15   Stabilization of a Turbulent Premixed Flame Using a Nanosecond Repetitively Pulsed Plasma   D. Galley, G. Pilla, D.-A. Lacoste, S. Ducruix, F. Lacas, D. Veynante, C.-O. Laux, Lab. EM2C, CNRS, Chatenay-Malabry, FR         5.12.07 15h40   Modeling of PAH and Soot Formation in Primary Reference Fuel Combustion   N. Slavinskaya, M. Aigner, Inst.of Comb.Tech., Lampoldshausen, DE F. Donato, O. Haidn, DLR, Lampoldshausen - DE         5.12.08 16h05   Evaluation of Al/CO2 propellant performance for future Mars atmospheric missions   V. Golovichev, Chalmers University of Technology, Gothenburg, SE C. Bruno, Dip. di Mecc. e Aeron., Roma, IT         5.12.09 16h30   Universalities and LES Approach in the Modeling of Dispersion of Light Particles in Highly Intermittent High-Reynolds Number Turbulent Flow    M. Gorokhovski, A. Chtab, CNRS, St-Etienne, FR Session 5.11 - In-Space: Chemical and Nuclear Propulsion Thursday Afternoon/ 7 July 2005  Chaired by G. Bellaiche, CNES and O.Gorshkov, Keldysh Research Center Checkov Hall 5.11.01 14h00    1-D, Homogeneous Liquefied Gas Self-Pressurization Model    V. Zakirov, L. Li, Tsinghua University, Beijing, CN         5.11.02 14h25   Year of 2004 - Small Satellite Propulsion Challenges   V. Zakirov, L. Li, Tsinghua University, Beijing, CN         5.11.03 14h50   Propulsion Related Orbital Debris   M. Oswald, S. Stabroth, C. Wiedemann,P. Vorsmann, Technical University of Braunschweig, DE P. Vorsmann, P. Wegener, Wegener Aerospace Consult, Braunschweig, DE         5.11.04 15h15   Hybrid Propulsion Technology Applied to Aerospace Platforms   M. Mamou, P.-G. Amand, P. Chevreux, PyroAlliance SME , Les Mureaux, FR         5.11.05 15h40   Mini Motors Using Solid Propellants   L. Vignaroli, O. Orlandi, V. Bodart, SME Research Center, Vert le Petit, FR         5.11.06 16h05   The Half Century Progress in the Feasibility Assessment of the Fusion Detonation Powered Flying Machine Design   V. Belokogne, Samara State Aerospace University, RU         5.11.07 16h30   Problems of Space Power Engineering and Role of Space Nuclear Power Systems for their Solution   P. Andreev, V. Vasilkovsky, G. Zaritsky, N. Ponomarjov-Stepnoy, G. Kompaniets, V. Usov, FSUE "Krasnaya Zvezda", Moscow, RU         5.11.08 16h55   The Problems in Development and Prospects for Application of Space Nuclear Power Propulsion Systems   V. Akimov, A. Gafarov, Keldysh Research Center, Moscow, RU Inter-Symposium 2-5: >> Flight physics for aircraft and launch vehicles including reentry bodies-Propulsion Physics