• Title/Summary/Keyword: 공중발사 로켓

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Investigation on the shock-induced rocket separation from the mother plane (충격파에 의한 비정상 모선분리 현상 연구)

  • Kim Y. S.;Ji Y. M.;Lee J.-W.;Park J. S.
    • 한국전산유체공학회:학술대회논문집
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    • 2004.10a
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    • pp.155-160
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    • 2004
  • This paper describes a supersonic separation of air-launching rocket from the mother plane. Three dimensional Euler equations were numerically solved to analyze steady/unsteady state fluid flows. To solve the Euler equations, named CFD-FASTRAN that is commercial computation code. The results of simulation clearly demonstrate effect of shock-expansion wave interaction between the rocket and the mother plane. Moreover, important influential factors at separating stage of the rocket were extracted with a comprehensive analysis. Finally, from the consideration of supersonic-separation, a guideline to safety-separation is given to the design of supersonic air-launching rocket.

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Development of CanSat System With 3D Rendering and Real-time Object Detection Functions (3D 렌더링 및 실시간 물체 검출 기능 탑재 캔위성 시스템 개발)

  • Kim, Youngjun;Park, Junsoo;Nam, Jaeyoung;Yoo, Seunghoon;Kim, Songhyon;Lee, Sanghyun;Lee, Younggun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.49 no.8
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    • pp.671-680
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    • 2021
  • This paper deals with the contents of designing and producing reconnaissance hardware and software, and verifying the functions after being installed on the CanSat platform and ground stations. The main reconnaissance mission is largely composed of two things: terrain search that renders the surrounding terrain in 3D using radar, GPS, and IMU sensors, and real-time detection of major objects through optical camera image analysis. In addition, data analysis efficiency was improved through GUI software to enhance the completeness of the CanSat system. Specifically, software that can check terrain information and object detection information in real time at the ground station was produced, and mission failure was prevented through abnormal packet exception processing and system initialization functions. Communication through LTE and AWS server was used as the main channel, and ZigBee was used as the auxiliary channel. The completed CanSat was tested for air fall using a rocket launch method and a drone mount method. In experimental results, the terrain search and object detection performance was excellent, and all the results were processed in real-time and then successfully displayed on the ground station software.