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| 1 |
A Study on the Nylon Wire Holding and Release Mechanism for Cube Satellites by Applying Constant Holding
Koo, KeonWoo;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.1-6,
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| 2 |
The Methodology and Case of Scientific System Engineering Management Process in Defense Space Program
Park, Heonjun;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.7-10,
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| 3 |
Estimation of Hovering Flight Time of Battery-Powered Multicopters
Cho, Mun jin;Han, Cheolheui;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.11-20,
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| 4 |
Comparative Analysis of the PWM of an Inverter for an Electric Aircraft Thrust Motor
Koo, Bon-soo;Jo, Seong-hyeon;Choi, In-ho;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.21-29,
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| 5 |
Structural Analysis for VVIP Cabin Compartment Modification STC of Commercial Airplane
Lee, Sang Hoon;Bang, Dae Han;Choi, Sang Min;Choi, Hang Suk;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.30-39,
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| 6 |
Development of an Efficient Notching Toolkit for Response Limiting Method
Shin, Jo Mun;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.40-46,
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| 7 |
A study on optimizing the electrical load analysis for modifying the avionics equipment in an aged aircraft
Yoon, Inbok;An, Kyeongsoo;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.47-56,
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| 8 |
A Study on the Satellite Launch Vehicle Separation Detection Interface to Improve the Reliability of the Launch and Early Operation Phase
Lee, Nayoung;Kwon, Dong-young;Jeon, Hyeon-Jin;Jeon, Moon-Jin;Cheon, Yee-Jin;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.57-63,
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| 9 |
Operational Risk Assessment for Airworthiness Certification of Military Unmanned Aircraft Systems using the SORA Method
Namgung, Pyeong;Eom, Jeongho;Kwon, Taehwa;Jeon, Seungmok;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.64-74,
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| 10 |
Development of ROS-based Flight and Mission State Communication Node for X-Plane 11-based Flight Simulation Environment
Cho, Sungwook;
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The Society for Aerospace System Engineering
, v.15, no.4, pp.75-84,
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