• Title/Summary/Keyword: 미연방 항공우주국

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Performance of Constructed Facilities: Pavement Structural Evaluation of William P Hobby Airport in Houston, Texas

  • Kim, Sung-Hee;Jeong, Jin-Hoon;Kim, Nak-Seok
    • Journal of the Korean Society of Hazard Mitigation
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    • v.9 no.1
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    • pp.21-25
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    • 2009
  • The results of a recent case study for material characterizations and structural evaluation to design asphalt overlay thickness of William P Hobby airport in Houston, Texas are presented herein. The existing runway 12R-30L of Hobby airport consisted of thick asphalt overlay over Portland Cement Concrete (PCC) and the localized surface shoving as evident in the closure of surface groove has been observed recently. Using the field cored asphalt concrete mixtures, measurements of percent air voids, asphalt content and aggregate gradation were conducted to find out the causations of surface shoving and groove closure. The FAA layered elastic program, LEDFAA was utilized to evaluate pavement structural conditions for new asphalt overlay. Two different composition assumptions for existing pavement were made to evaluate the pavement as followings: 1) APC, Asphalt Concrete Overlay over PCC pavement and 2) AC, Asphalt Concrete pavement. Based on laboratory testing results, a ratio of percent passing #200 to asphalt content ranged 1.1 to 2.2, which is considered a high ratio and a tendency of tender mix design was observed. Thus, the localized surface shoving and groove closure of the runway 12R-30L could be attributed to the use of excessive fine contents and tender mix design. Based on the structural evaluation results, it was ascertained that the analysis assuming the pavement structure as AC pavement gives more realistic structural life when the asphalt overlay is thicker enough compared to PCC layer because the existing PCC pavement under asphalt overlay acts more like a high quality base material.

Japanese Aircraft Certification System and Status of Bilateral Aviation Safety Agreement (일본의 항공기인증제도 및 항공안전협정(BASA) 체결 동향)

  • Park, Guen-Young;Jin, Young-Kwon;Lee, Jong-Hee
    • Current Industrial and Technological Trends in Aerospace
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    • v.8 no.2
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    • pp.124-135
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    • 2010
  • The Japanese and U.S. governments has signed a Bilateral Aviation Safety Agrement and associated implementation procedures for airworthiness on April 27, 2009 to mutually accept the airworthiness approvals for aircraft and parts that the other country issue. This bilateral agreements do not relieve the Civil Aviation Authority(CAA) of its statutory responsibilities for certification. However, they provide an alternative means for the CAA to make its findings, recognizing the competency of another authority to conduct certification functions in a manner comparable to, and on behalf of, the CAA. In this way, the bilateral agreements contribute to ensuring aviation safety as well as reducing the burden imposed on the aviation industries without compromising safety. This paper is to discuss recent status of Bilateral Aviation Safety Agreement and associated Japanese Aircraft Certification System.

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A Study of the C-band Ground-based Radio Navigation System for UAM Cooperative Navigation (UAM 복합 항법을 위한 C 밴드 지상기반 전파 항법 시스템 연구)

  • Kyung-Soon Lee;Yong-Un Cho;Min-Jung Kim;Kyung Heon, Koo
    • Journal of Advanced Navigation Technology
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    • v.27 no.4
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    • pp.374-381
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    • 2023
  • This study focuses on the implementation of C-band radio navigation in the 5.03 ~ 5.15 GHz terrestrial band to cooperate with GNSS navigation mainly used in existing UAMs. This is one of the navigation technologies that can fully satisfy the requirements of Title 14 of CFR-135.165. According to the FAA, the use of two or more independent navigation sources for aircraft is proposed for aircraft. This study proceeded with the link budget derivation through radio wave propagation path loss analysis, and antenna shape design for miniaturized Doppler VOR, and DME design with enhanced positional distance resolution compared to conventional aircraft. The ground navigation system which is the result of this study, consists of a VOR/DME ground station and a terminal that can be mounted on UAM. Significant performance was confirmed through the production and testing of each prototype.

Evaluation of Friction and Hydroplaning Characteristic in Aifield Using Dry Grooving Method (건식그루빙을 사용한 공항 활주로의 마찰 및 수막현상 특성평가)

  • Park, Tae-Soon
    • International Journal of Highway Engineering
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    • v.3 no.3 s.9
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    • pp.111-118
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    • 2001
  • Since the advent of turbojet aircraft with their greater weight and high landing speed breaking performance on runway surface has become un critical. Under certain weather conditions(wet weather, winter) hydroplaning or unacceptable loss of traction can occur, resulting in poor braking performance and possible loss of directional control. To address this concern a number of research project me conducted by NASA, FAA, USAF. The various method which was reported the advantage of the increasing the friction and decreasing the hydroplaning effect. A-2 section of inchon international airport was grooved using drying grooving method. In order to evaluate the effectiveness of the dry grooving method the surface was spray with water and measured the fiction factor and the depth of the water using Mu meter and water depth measuring device. The field test results shooed that the fiction factor nos increased and the depth of the water decreased. The dry grooving method illustrated the reduction of hydroplaning and also, no distress on the runway.

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