• Title/Summary/Keyword: High altitude

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On the Management of Nutrition for High Altitude Training (고지(高地) 훈련시(訓練時) 영양관리(營養管理)에 관(關)하여)

  • Sung, N.E.;Lee, C.H.
    • Journal of Nutrition and Health
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    • v.1 no.1
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    • pp.27-31
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    • 1968
  • The author investigated the effects of dietary composition upon the work efficiency of Splague Dowley rat at high altitude, and obtained the following results: 1. At high altitude a carbohydrate-rich diets worked more favorably upon work efficiency of the animal then a protein and or fat-rich diets did. 2. It may be recommended that fibrous components be excluded from the diets. 3. Ingestion of large amounts of sugars prior to the onset of work load is highly recommended.

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A New Methodology for Estimating the Impact of Co-Channel Interference from High-Altitude Platforms to Terrestrial Systems

  • Milas Vasilis F.;Constantinou Philip
    • Journal of Communications and Networks
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    • v.8 no.2
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    • pp.175-181
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    • 2006
  • This paper addresses an in-depth analysis of the stratosphere-to-Earth co-channel interference produced by high-altitude platforms (HAPs) and proposes a new methodology for the evaluation of its impact to terrestrial systems in terms of fractional degradation in performance, taking into account parameters such as HAP's mobility, realistic distribution of azimuth and elevation angles of the terrestrial microwave links (TMLs), and gradual high-altitude platform network (HAPN) loading. Simulations performed for different HAPN configurations, prove that the implementation of the methodology proposed, may lead to a more efficient use of the spectrum shared between the two services.

Conceptual Design of High Altitude Test Facility for Testing Liquid Rocket Engine (액체로켓엔진 고공모사시험설비의 개념설계)

  • Kim, Cheul-Woong;Nam, Chang-Ho;Kim, Seung-Han;Seol, Woo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.383-387
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    • 2008
  • To design a high altitude test facility for testing liquid rocket engine optimal technical solutions with general understanding about characteristics of engines and test stands, mission of a rocket and the financial aspects of tests are required. In this paper conditions and requirements needed at the stage of conceptual design of high altitude engine test facility were suggested, and preliminary calculations of the sizes of a supersonic diffuser and volume of cooling water were carried out.

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Analysis of Importance of Search Altitude Control for Rapid Target Detection of Drones

  • Ha, Il-Kyu
    • Journal of information and communication convergence engineering
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    • v.16 no.2
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    • pp.78-83
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    • 2018
  • Rapidity and accuracy are important considerations when a drone is employed in a wide surveillance area to detect a target. They are more important when the scope of application is a search and rescue operation or the monitoring of natural disasters, which may require prompt warnings and response. During the actual operation of a drone, rapidity and accuracy are associated with the change in the altitude of the drone. The aim of this study is to analyze the characteristics of drones at varying altitudes and prove that altitude is a relevant factor in the performance of drones. Herein, the characteristics of the drone at varying altitudes were analyzed through several search simulations. The results suggest that a high-altitude drone is relatively advantageous compared to a low-altitude drone in a probability-based target search, and that the search altitude is also a very important and fundamental factor in target search by drones.

Observation of Long and Short Wave Radiation During Summer Season in Daegu Area (대구지역의 하절기 장.단파복사 관측)

  • Oh, Ho-Yeop;Choi, Dong-Ho;Lee, Bu-Yong
    • 한국태양에너지학회:학술대회논문집
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    • 2012.03a
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    • pp.134-139
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    • 2012
  • This study observed downward long and short-wave radiant environment with selecting 4 areas which have different height in downtown and 1 suburban area to figure out the characteristic of radiant environment in each altitude. The purpose of this study is to collect the preliminary data for interpreting urban thermal environment in summer season by analyzing thermal characteristic of atmosphere in the upper of downtown. The results of this study are as follows. 1) The higher altitude has the lower temperature, and temperature difference was more huge in day time than night time. 2) The short wave radiation according to altitude was higher as altitude was high. 3) Generally, the higher altitude has the lower air temperature, and also the higher altitude has the lower downward long wave radiation by the atmospheric radiation. 4) The ratio short wave radiation of long wave radiation was lower as altitude was high. And the urbanization effect was higher as the ratio was low.

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Construction of a High-Altitude Ignition Test Facility for a Small Gas-turbine Combustor (소형 가스터빈 연소기 고공환경 점화 시험 설비 구축 및 검증 실험)

  • Kim, Tae-Woan;Lee, Yang-Suk;Kim, Ki-Woo;Kim, Bo-Yean;Ko, Young-Sung;Kim, Sun-Jin;Kim, Hyung-Mo;Jung, Yong-Wun
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.3
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    • pp.61-68
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    • 2010
  • A small high altitude test facility has been developed to investigate ignition performance of a small gas-turbine combustor under high altitude conditions. Supersonic diffusers and a heat exchanger were used to perform a low pressure and a low temperature condition, respectively. Experimental results showed that the low pressure environment could be controlled by upstream pressure of primary nozzle flow and low temperature environment by mixture ratio of cooled air and ambient air. Ignition performance tests were performed to verify the performance of the facility under simulated high altitude conditions. Conclusively, it was proven that the test facility could be used for ignition performance test of a small gas-turbine combustor under high altitude condition of approximately 6,100m.

Performance of UAV(Unmanned Aerial Vehicle) Communication System Using Civil Wireless Mobile Networks

  • Lee, Byung-Seub
    • Journal of Satellite, Information and Communications
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    • v.12 no.1
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    • pp.43-48
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    • 2017
  • Recently, demands on civilian UAV (Unmanned Aerial Vehicle) has been increasing and appropriate communication system is required for the UAV. In this paper, the performance of the UAV communication system using commercial wireless mobile network is discussed. The main service area of the wireless mobile network is ground level however the flying range of the UAV is normally in high altitude. Because of this mismatch of service area the performance of the UAV communication system is degraded in high altitude. To compensate performance degradation of the UAV communications system in high altitude, adaptive array antenna is introduced which is able to overcome altitude limitation of the UAV communication system.

Development and Performance Test of Vacuum Facility at the CNU for High Altitude Space Environment Test (충남대학교 고고도 우주환경모사 진공설비의 구축 및 성능설험)

  • Jung, Sung-Chul;Kim, Youn-Ho;Shin, Kang-Chang;Huh, Hwan-Il
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.45-48
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    • 2007
  • Vacuum facility is required for high altitude space environment test to develop small thruster. We, at Chungnam National University, developed vacuum test facility up to $10^{-5}$ torr to simulate 100${\sim}$120 km altitude environment. In this paper, we present some preliminary performance test results.

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The Cooling System for Head up Display (Head up Display용 냉각시스템)

  • Ji, Youg-Seok;Kim, Young-Seop;An, Byeong-Man;Lim, Sang-Min
    • Journal of the Semiconductor & Display Technology
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    • v.9 no.1
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    • pp.67-71
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    • 2010
  • Head up display’s cooling system is auto-diagnosed resulting from the external environment. The quantity of heat depending on this Head up display’s cooling system layout determines the speed of FAN for system cooling. In other words, a system’s heat quantity is planned through the air density depending on altitude, the amount of wind in air depending on FAN control condition, and the algorithm that is proportional to delta temperature. To detect the altitude, we use the criteria of delta T, which is determined by the subtracted value of LED junction temperature, and atmospheric temperature that is recorded on the Head up display system. Depending on the classification of delta T value, the altitude section is determined. While we can use GPS as the tool to detect the altitude, we should predict the change of the air density as the altitude alters, and should not just measure the altitude. And the value of delta T is used as the criterion of detecting the altitude for increasing the cooling efficiency of the car’s inner Head up display system with reflecting the speed of the FAN dependent upon the air density. In our theory, altitude is depending on the value of delta T and stabilizing or maintaining the system’s temperature by changing FAN’s rpm depending on determined value of altitude.

Selection of Transformer for the Augmentation of an Existing AIS EHV Substation in Hilly Terrain at 3000m+ Altitude

  • Kim, Kwang-Soo;Kang, Byoung-Wook;Kim, Jae-Chul
    • Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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    • v.26 no.12
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    • pp.28-36
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    • 2012
  • Augmentation of existing EHV substations located in hilly terrain and at high altitude require many different considerations as compared to substations located in plain areas and at lower altitude. Owing to high altitude and steep terrain, meticulous engineering and preparations are required, considering the actual available space at the existing substation. Historical fault events too must be considered to enhance reliability and performance of the substation equipment. This paper proposes ways to augment the existing 2 banks of 20MVA, 220/66kV power transformers ($3{\times}6.67MVA$, single-phase) to $2{\times}50$/63MVA, 220/66kV power transformers to meet continuously increasing demand of the capital city over the next 20 years. Upgrading and augmentation of existing substations, especially the main transformers and associated equipment, require replacement with minimum or no disturbance to the existing power supply system. Considerations should also be made during engineering and design, the operational flexibilities, maintenance aspects, future expandability and value addition, in terms of reliability and space usage of the existing substation.