Space for our future proceedings of the 13th International Conference of Pacific-Basin Societies (ISCOPS) held May 15-18, 2012, Kyoto, Japan
Development of carbon/carbon-silicon carbide composite for space mirrors (AAS 12-561) -- A vision of future space transportation systems (AAS 12-562) -- Research development and flight test of subscale reusable winged rockets (AAS 12-563) -- Combustion characteristics of hybrid rocket motor using GA...
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| Format: | UnknownFormat |
| Sprache: | eng |
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San Diego, California
Publ. for the American Astronautical Society by Univelt
2013
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| Schriftenreihe: | Advances in the astronautical sciences
146,CD-ROM |
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Tag hinzufügen | Zusammenfassung: | Development of carbon/carbon-silicon carbide composite for space mirrors (AAS 12-561) -- A vision of future space transportation systems (AAS 12-562) -- Research development and flight test of subscale reusable winged rockets (AAS 12-563) -- Combustion characteristics of hybrid rocket motor using GAP-based solid fuel (AAS 12-565) -- Combustion mechanism and thruster application of HAN-based green propellant (AAS 12-566) -- Study on application of DBD plasma actuator for side force control of high-angle-of-attack slender body (AAS 12-567) -- Technical findings of HTV propulsion system associated with its dynamic characteristics (AAS 12-568) -- The development of HTV exposed pallet multi-purpose (AAS 12-569) -- Development of a hypersonic shock tube for planetary entry aerothermodynamics (AAS 12-570) -- Influence of elastic deformation on unsteady multi-body separation (AAS 12-571) -- Application of the scaling technology in numerical study on the aerodynamic characteristics of launch vehicle (AAS 12-572) -- The development status of the Epsilon Launch Vehicle (AAS 12-573) -- Research and develoment progress of Space Transportation Propulsion R & D Center in JAXA (AAS 12-574) -- Overview of LE-X research and development program (AAS 12-575) -- Critical performance of trubopump mechanical elements for rocket engine (AAS 12-576) -- Development and test of the LOX/LNG regenerative cooled rocket engine (AAS 12-577) -- Pressure and geometry scaling of flowfield and combustion characteristics of gaseous hydrogen and gaseous oxygen shear-coaxial injectors (AAS 12-578) -- Post-flight analysis of Hayabusa; asteroid sample return capsule (AAS 12-579) -- Technical demonstrations for reusable sounding rocket system (AAS 12-580) -- Electrostatic levitation furnace for the International Space Station (AAS 12-581) -- The study on structure of large reflector for space solar power systems (SSPS) (AAS 12-582) -- Exploring innovative ways of cooperation and technology transfer between Japan and Columbia (AAS 12-583) -- Destiny Mission overview: a small satellite mission for deep space exploration technology demonstration (AAS 12-585) -- Formation flying around libration points of circular restricted three body problem with small [mu] (AAS 12-586) -- Japanese Moon Lander SELENE-2 and its technology development (AAS 12-587) -- Launching low Mars Orbiter by using aerobraking (AAS 12-588) -- Error analysis and mid-course maneuver of Earth-Mars transfer orbit (AAS 12-589) -- On orbit design around a micro gravity asteroid (AAS 12-590) -- Appendices -- Indices. |
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| Beschreibung: | Includes bibliographical references and indexes |
| Beschreibung: | 1 CD-ROM (color ; 12 cm) illustrations 25 cm |
| ISBN: | 087703592X 0-87703-592-X 9780877035923 978-0-87703-592-3 |