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> Uchu Kozo, Zairyo Shinpojiumu. Heisei 14 Nendo. Dai18kai
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Uchu Kozo, Zairyo Shinpojiumu. Heisei 14 Nendo. Dai18kai
Development situation of large deployable reflector for ETS-VIII installation.
Compressive strength of C/C composite.
Influence of interface on tensile fracture mechanism of C/C composites.
Nonlinear dynamic behavior of carbon fiber/carbon composite material.
Failure mechanism from rocket motor case hoop wound layer made of FWCFRP.
Attempt of numerical analysis of ultrahigh-speed collision destruction and performance evaluation of debris shield protection of composite material laminate.
Effect of rubber modification on fracture property of glass-microballoon-filled epoxy resin.
Very low temperature strength property of titanium alloy small forging steel for FTP. Aiming at reliability improvement of FTP 2.
Effect of grain size on low temperature fatigue property of ELI alloy of Ti-5%Al-2.5%Sn.
Effects of surface roughness and notch on very-low-temperature fatigue property of titanium alloy.
High cycle fatigue property of alloy 718 superalloy for rocket engine.
Fatigue crack progress property and fractography of Alloy 718.
"Ultrasonic wave automatic flaw detection method of a graphite nozzle throat by pulse reflection, omniazimuth perpendicular flaw detection and full immersion testing" standard.
Array-type ultrasonic testing system of graphite for solid propellant rocket motor nozzle throat.
Ultrasonic propagation property evaluation of graphite nozzle throat material.
Evaluation of ultrasonic reflection source of graphite nozzle throat material.
Microscopic destruction and mechanical properties of graphite material.
Measurement of tension property of film surface considering application to solar sail.
Folding of thin circular film with easy deployability.
Analysis of development behavior of spin-type solar sail.
Consideration on Deployable Membrane Structures in Organisms.
Film surface shape control characteristics by piezoelectric film stuck in fold region.
Effect of fold on vibration of unidimensionally deployed film surface.
Vibration measurement of film using image analysis.
Resonant frequency detecting method of microstructure.
Deploying experiment of integrated inflatable structure.
Vibration control of inflatable structure using piezoelectric element.
Shape analysis of inflatable film structure (for realization of parabola shape).
Specular shape control of mesh reflecting mirror based on radiation characteristics analysis.
Dynamics Analysis of A Solar Power Satellite.
Stability Analysis of Gravitational Stabilized Space Solar Power System.
Effect of Aerodynamic Loads on the Dynamic Stability of Slender Launch Vehicle Subjected to an End Rocket Thrust.
Damping Design for Controlling Flutter Bound of Free-Free Beams Subjected to Rocket Thrust.
Improvement considering coupling of propellant to bending vibration model of solid propellant rocket motor.
Impact load determination of laminate using embedded piezoelectric sensor.
Mode displacement measurement by optimum arrangement of strain sensor.
Construction of a structure health monitoring technique by smart structure using piezoelectrics.
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