• Title/Summary/Keyword: 돛

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Development and Performance Test of Solar Sail System for CNUSAIL-1 Cube Satellite (CNUSAIL-1 큐브위성의 태양돛 개발 및 성능시험)

  • Song, Su-A;Kim, Seungkeun;Suk, Jinyoung;Roh, Jin-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.3
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    • pp.228-239
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    • 2016
  • CNUSAIL-1 is a 3U-sized cube satellite with $4m^2$ small solar sail which is currently being developed at the Chungnam National University. The primary purpose of the CNUSAIL-1 is successful sail deployment in LEO and its operation for investigating its effect on satellite orbit and attitude as well as performing de-orbiting using the sail membranes as drag sail at the final phase. The system design and mechanism of solar sail deployment is introduced, and optical and tensile tests are carried out for the material of membranes and booms for its safety and performance verification. The ground test is carried out to verify its performance for sail deployment and satellite through comparison between folding methods by determining its folding patterns, thickness of spiral spring and angular velocity measurement in a low-friction environment.

Status of the Solar Sail Technologies (태양돛 기술 동향)

  • Cho, Hyeong-Sun;Kim, Hak-In;Lee, Soo-Yong;Roh, Jin-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.6
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    • pp.495-504
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    • 2014
  • Solar sail spacecrafts can gain propulsion using the momentum change through reflecting the photon packets of energy from the Sun. The sail slowly but continuously accelerates to accomplish a wide-range of potential missions. To develop the potential mission of the solar sail, the configuration, the film characteristics and the deployment devices should be carefully considered. In this paper, recent development and activities of the solar sail are introduced and design technology of the sail subsystem is investigated.

Wrinkle Reduction Design Method of Triangular Solar Sail (삼각형 태양돛의 주름저감 설계방안)

  • Bae, Hongsu;Woo, Kyeongsik
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.12
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    • pp.940-949
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    • 2013
  • In this paper, wrinkle reduction design was studied for triangular sail. Wrinkles in the solar sail membrane can change the load path and surface topology which may have an adverse effect on propulsion performance and controllability. In this study, wrinkle reduction strategies of adjusting cable angle, catenary and catenary-wire schemes were considered and the design parameters for wrinkle reduction were systematically investigated.

Mission and Conceptual System Design of Solar Sail Testing Cube Satellite CNUSAIL-1 (태양돛 시험용 큐브위성 CNUSAIL-1의 임무 및 시스템 개념설계)

  • Koo, Soyeon;Kim, Gyeonghun;Yoo, Yeona;Song, Sua;Kim, Sungkeun;Oh, Bockyoung;Woo, Beomki;Han, Chang-Gu;Kim, Seungkeun;Suk, Jinyoung;Han, Sanghyuck;Choi, Gi-Hyuk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.7
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    • pp.586-593
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    • 2014
  • The CNUSAIL-1 project aims to develop and operate a 3U-sized cube satellite with solar sail mechanism. The primary mission is to successfully deploy the solar sail in a low earth orbit, and the secondary mission is to collect the scientific data for the effect of the solar sail deployment and operation on orbit maneuver and attitude change of the cube satellite. For this, the bus system will collect and transmit the dynamic data of the satellite and the visual images of the solar sail operation. This paper describes solar sail mission and conceptual design of CNUSAIL-1. The actuation/operation of the solar sail and the bus system are preliminarily designed in terms of attitude control system, communication system, electrical power system, command and data handling system, structure and thermal control system is designed.

A Study on Orbit Transfer Methods for Solar Sail Spacecraft (태양돛 우주선의 궤도천이 기법 연구)

  • Kim, Min-Gyu;Kim, Jeongrae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.10
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    • pp.770-778
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    • 2013
  • Solar sail propulsion uses solar radiation pressure to propel spacecraft without propellant, and it is useful for deep-space missions and continuos orbit maneuver missions. After a brief introduction of solar sail dynamics, locally optimal trajectories in Sun-centered and Earth-centered orbits are analyzed. Numerical simulations for the optimal trajectories are performed. Trajectory for the rendezvous with Halley comet is generated, and different planet escape methods are compared.

새치류의 부리와 미사일의 Spike형상의 유동특성 연구

  • Gil, Ha-Jong;An, Yeong-Min;Bae, Jin-Gyu
    • Proceeding of EDISON Challenge
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    • 2016.11a
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    • pp.44-48
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    • 2016
  • 물 속에서 고속으로 유영하는 상당수의 어류는 긴 부리 모양의 주둥이를 가진다. 대표적으로 지구상 가장 빠른 물고기인 돛새치가 있다. 이러한 사실은 이 독특한 형상과 고속운동의 상관관계에 대해 학구적 호기심을 자아냈고 그에 따라 본 연구를 수행하였다. 본 연구에서는 돛새치, 청새치들의 2차원 형상을 가지고 부리의 존재 유무가 항력에 미치는 영향을 분석하고 더 나아가 미사일의 spike가 항력에 미치는 영향을 분석하였다. 또한 부리가 방향전환 시 기동성 증진에도 기여하는지를 알아보았다. 해석을 위해 Kflow Edison_13와 2D_Comp_P 해석자를 활용하여 동일 유동조건에서 항력계수를 비교하였다. 그리고 돛새치가 방향 전환할 때 발생하는 모멘트계수를 얻기 위해 2D_Incomp_P 해석자를 활용하였다.

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A study on the performance evaluation and technical development of an eco-environmental photovoltaic solar leisure boat with applied sail control device (접이식 풍력 Sail 돛 제어장치를 적용한 친환경 태양광 레져보트의 성능평가)

  • Moon, Byung-Young;Lee, Sung-Bum;Lee, Ki-Yeol
    • Journal of Advanced Marine Engineering and Technology
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    • v.40 no.3
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    • pp.240-248
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    • 2016
  • As a new technical approach, the achievement of an eco-environmental leisure boat with a photovoltaic system is attempted by simultaneously actuating nine photovoltaic solar panels, in association with an applied sail control system by use of wind. In this approach, the photovoltaic system consists of a solar module, an inverter, a battery, and relevant components, while the sail control device is equipped with a sail up/down and mast-turning instrument. Furthermore, this research conducts a performance evaluation of the manufactured prototype and acquires the purposed quantity value and the development purpose items. The significant items-sail up/down speed (seconds) and mast turning angle (degrees)-are evaluated during the performance test. In the process of the performance evaluation, a wind direction sensitivity of 90% and a maximum instant charging power of 900 W were also obtained. In addition, the maximum sail time is evaluated in order to acquire the optimum quantity.

Feeding Habits of Moon Dragonet Repomucenus lunatus in the Coastal Waters off Gori, Korea (동해 남부 고리 주변해역에 출현하는 돛양태(Repomucenus lunatus)의 식성)

  • Huh, Sung Hoi;Kim, Jin Min;Park, Joo Myun;Baeck, Gun Wook
    • Korean Journal of Ichthyology
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    • v.25 no.1
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    • pp.17-24
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    • 2013
  • The feeding habits of Repomucenus lunatus were studied using 232 specimens collected from January to December 2006 in the coastal waters off Gori, Korea. The size of R. lunatus ranged from 4.7 to 14.0 cm in standard length (SL). R. lunatus was a bottom-feeding carnivore which consumed mainly amphipods and polychaetes. Its diet also included small quantities of shrimps, cumaceans, bivalvies, gastropods, crabs, copepods, euphausia, mysids, stomatopods, ostracods and sipunculides. Amphipods were eaten predominantly for the smallest size class. The proportions of polychaetes increased gradually with increasing fish size and large size class of R. lunatus mainly consumed polychaetes. The feeding strategy graphical method revealed that R. lunatus is a specialized feeder. The mean number and weight of preys per stomach of larger size classes were higher than those of smaller size classes. The mean weight of preys per stomach ontogenetically changed with size classes.

농민의 자리에서 본다-필요성이 곧 가능성도 아니고,가능성이 곧 현실성도 아니다

  • No, Yeong-Han
    • The Korea Swine Journal
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    • v.17 no.11 s.195
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    • pp.56-57
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    • 1995
  • 이번 불황을 맞아"우리나라 양돈산업이 올바로 가고 있나?'에 대해서 점검할 필요가 있다. 당뇨병 환자의 갈증을 해결하려면 물을 마시는 것보다는 당뇨병을 치료해야 하기 때문이다 돛단배는 바람이 방향이 같은데도 불구하고 돛의 방향에 따라 가는 길이 다르듯이,단지를 만들고 축사시설을 다시 해서 구조개선을 한다 해도 각기 가는 방향은 다를 수 있기 때문이다. 항상 목적지를 향해 바로 가고 있는가를 점검할 필요가 있다.

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