hypersonic flight experiment, HYFLEX, elctronical component, bus system evaluation, guidance control system, onboard electrical equipment, reflect meter, communication and tracking system, actuator system, antenna pattern, post flight analysis, electrical component development
その他のタイトル(英)
Development of electrical components and evaluation of bus system
The electrical equipment installed in the HYFLEX (Hypersonic Flight Experiment) vehicle has been developed in a short period by applying well established technology and by utilizing and modifying developed equipment. This paper presents the function, performance and an outline of the developed equipment. Post flight evaluation and analysis results for bus system (electric system) are also presented.