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FAA William J. Hughes Technical Center for Advanced Aerospace

rosaP Repository & Open Science Access Portal

Technical reports, Tech Notes, and articles that document the FAA’s applied research, engineering, testing and evaluation, and resulting scientific solutions addressing current and future air transportation challenges in collaboration with industry, academia, and other government partners. For more content, visit the FAA Technical Library https://www.faa.gov/about/office_org/headquarters_offices/ang/library/. Bookmark this collection:https://rosap.ntl.bts.gov/collection_faa_tl or https://doi.org/10.21949/1530830.

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Showing 761 - 780 of 802 results
  • Test and Evaluation of the Discrete Address Beacon System DABS Moving Target Detector MTD Radar Data Acquisition Subsystem RDAS
    Test and Evaluation of the Discrete Address Beacon System (DABS) / Moving Target Detector (MTD) / Radar Data Acquisition Subsystem (RDAS)
    Mancus, Edward
    1981-05-01 | PDF
    The primary objectives of testing the Moving Target Detector (MTD) and the Radar Data Acquisition Subsystem (RDAS) as an integral part of the Discrete Address Beacon System (DABS) are to characterize their combined performance in:a. Providing radar/beacon correlation of DABS and Air Traffic Control Radar Beacon System (ATCRJSS) targets with radar t ...
  • Index of NAFEC Technical Reports 1972 1977
    Index of NAFEC Technical Reports, 1972 -1977
    Farrell, Ruth J. ;
    Boylan, Nancy G.
    1981-05-01 | PDF
    This report 1S an index of all technical reports which were assigned NA numbers and published by NAFEC during the period 1972 through 1977. Entries are arranged by NA number and include titles, authors and full abstracts. Separate sections contain indexes by subject, author, and RD number.
  • A Compendium of Aircraft Cockpit Vision Surveys 1950 Through 1980 Volume I
    A Compendium of Aircraft Cockpit Vision Surveys 1950 Through 1980 – Volume I
    Barile, Anthony J.
    1981-05-01 | PDF
    This publication contains a history of cockpit visibility surveys which were conducted to measure and record aircraft (General Aviation, Transport, Helicopter, Military) cockpit visibility. Many of the aircraft were involved in midair collisions, accident investigations, research and development, and the design up through production implementation. ...
  • Application of General Technology Applications Incorporated GTA Blending Process to Antimisting Fuel Additives
    Application of General Technology Applications, Incorporated (GTA) Blending Process to Antimisting Fuel Additives
    Trippe, J. C. ;
    Waters, P. F.
    1981-05-01 | PDF
    This program examines the applicability of a proprietary blending process to blending antimisting additives in JET A aviation fuel. The first phase of the program covers Use of the process with a high molecular weight polyisobutylene. The second phase covers the use of the process with Imperial Chemical Industries, Ltd.'s proprietary polymer, FM-9. ...
  • Active Beacon Collision Avoidance Logic Evaluation Volume 1 Mode C Equipped ATCRBS Threat Phase
    Active Beacon Collision Avoidance Logic Evaluation: Volume 1, Mode C Equipped (ATCRBS) Threat Phase
    Adkins, A. ;
    Billmann, B.
    1981-05-01 | PDF
    The purpose of this project was to evaluate and refine the April 1979 version of the Beacon Collision Avoidance System (BCAS) logic prior to Active BCAS prototype flight testing. The April 1979 version of the BCAS logic added changes to support multiple aircraft resolution, conflict indicator register interfacing, and new surveillance function inte ...
  • Radar Detection of Birds Hazardous to Aircraft Phase II
    Radar Detection of Birds Hazardous to Aircraft (Phase II)
    Lee, Tai Y.
    1981-04-01 | PDF
    A portable photographic radar recording system developed by the Technical Center Photographic Laboratory was evaluated to determine its capability to monitor and record bird movements as detected by an airport surveillance radar. This system was developed for use by U.S. Fish and Wildlife Service (USFWS) biologists for study of bird hazards problem ...
  • Math Model Study of Glide Slope Sites for Runway 19L San Francisco International Airport San Francisco California
    Math Model Study of Glide Slope Sites for Runway 19L, San Francisco International Airport, San Francisco, California
    Walls, John
    1981-04-01 | PDF
    Results of a math model study for the runway 191 Instrument Landing System (ILS) glide slope at the San Francisco International Airport, San Francisco, California, are presented. This study was performed at the request of the Western Region to determine the effects on glide slope performance resulting from proposed relocation of the glide slope and ...
  • First Quarterly Data Report for the Reliability and Maintainability Evaluation of the Basic Wide Microwave Landing System at Wallops Island Virginia
    First Quarterly Data Report for the Reliability and Maintainability Evaluation of the Basic Wide Microwave Landing System at Wallops Island, Virginia
    Plotka, Marvin S.
    1981-04-01 | PDF
    This is the first quarterly data report on the reliability and maintainability evaluation of the Basic Wide Microwave Landing System located at Wallops Island, Virginia. Chargeable and nonchargeable failures are defined. Chargeable failures are listed, and calculated reliability values are presented.
  • Remote System Monitor Type FA98521
    Remote System Monitor Type FA-9852/1
    Brown, Harry L.
    1981-04-01 | PDF
    Data were collected on the performance of the Remote System Monitor (RSM), type FA-9852/1, at the Federal Aviation Administration (FAA) Technical Center. The RSM supports the Radar Beacon Performance Monitor (RBPM) program. The performance was monitored in a real-world environment as a subtask of 9550-AAF-501-78-002. The parameters observed were az ...
  • Analytical Investigation of Time Correction in AlphaBeta Tracking Filters with Application to En Route Tracking
    Analytical Investigation of Time Correction in Alpha-Beta Tracking Filters with Application to En Route Tracking
    Lefferts, Robert E.
    1981-04-01 | PDF
    In the analysis of the a-a tracking filter, it 1s normally assumed that the tracking filter and data source operate in synchronism at a constant data rate. An analytical solution is obtained for the case in which the tracking filter and data source operate asynchronously, thus violating the standard assumptions. To compensate for the asynchronous o ...
  • Terminal Helicopter Instrument Procedures TERPS
    Terminal Helicopter Instrument Procedures (TERPS)
    Pursel, Robert H.
    1981-04-01 | PDF
    The Federal Aviation Administration (FAA) Technical Center Helicopter Project is designed to provide actual flight test data to the FAA Office of Flight Operations (AFO) to aid in the updating and streamlining of helicopter terminal area procedures and criteria. The data gathered here will be used toward the revision of chapter 11 of the Terminal I ...
  • Evaluation of the Navigation Satellite Timing and Ranging Global Positioning System Navstar GPS as a Rotary Wing Aircraft Navigation Aid Using the Magnayox Z Set
    Evaluation of the Navigation Satellite Timing and Ranging Global Positioning System [Navstar GPS] as a Rotary Wing Aircraft Navigation Aid Using the Magnayox “Z” Set
    Till, Roger D.
    1981-04-01 | PDF
    This project plan is designed as a series of task designated tests as scheduled in section 9 to be conducted with the primary objective to evaluate the suitability and accuracy of low-cost Navigation Satellite Timing and Ranging Global Positioning System (NAVSTAR GPS) receivers for helicopter area navigation operations. The results will be compared ...
  • Flight Tests of the American Electronic Laboratories Inc AELNarco Low Cost General Aviation Microwave Landing System MLS Receiver
    Flight Tests of the American Electronic Laboratories, Inc. [AEL]/Narco Low Cost General Aviation Microwave Landing System [MLS] Receiver
    Warren, John
    1981-04-01 | PDF
    The objective is to evaluate performance characteristics of a low-cost Microwave Landing System (MLS) receiver (American Electronic Laboratories, Inc. (AEL) / NARCO Avionics) through comparative flight tests with a standard Bendix receiver. The analog outputs and system flags to the pilot's course deviation indicator (CDI) from both units will be c ...
  • Full Digital Automated Radar Terminal System ARTS Display
    Full Digital Automated Radar Terminal System (ARTS) Display
    Clark, Robert A. ;
    Aschenbach, John W.
    1981-03-01 | PDF
    The objective of this project is to determine the suitability of the Full Digital Automated Radar Terminal System (ARTS) Display for operational use in automated terminal air traffic control facilities. The results of this evaluation will be presented in a final report which will serve as the basis for a future production specification.
  • Effect of Thermal Radiation on the Integrity of Pressurized Aircraft Evacuation Slides and Slide Materials
    Effect of Thermal Radiation on the Integrity of Pressurized Aircraft Evacuation Slides and Slide Materials
    Brown, Louis J. ;
    Nicholas, Eldon B.
    1981-03-01 | PDF
    Seventeen full-scale fire tests were conducted to examine the effect of thermal radiation from a large fuel fire on the integrity of pressurized aircraft evacuation slides. Urethane nylon, aluminized urethane nylon, neoprene nylon, aluminized neoprene nylon, and aluminized neoprene Kevlar slides were tested at various distances from a 30-by-30-foot ...
  • Type 1106 Flasher Modification for Remote Operation
    Type 1106 Flasher Modification for Remote Operation
    Jones, Paul H.
    1981-03-01 | PDF
    The Federal Aviation Administration (FAA) 1S presently planning to install an approach lighting system with sequenced flashing lights for category II (ALSF-2) on runway 22R at the McGhee-Tyson Airport, Knoxville, Tennessee. This project was performed in response to an Airway Facilities Services request to determine the feasibility of modifying a fl ...
  • Considerations on Collision Risk Analysis for Decision Making in the NAT Region
    Considerations on Collision Risk Analysis for Decision Making in the NAT Region
    United States. Department of Transportation. Federal Aviation Administration. Technical Center
    1981-03-01 | PDF
    This working paper presents the views of the United States relative to a proposed change 1n the North Atlantic System Planning Group's decision-making procedure. This view is that the decision making process is composed of a number of interrelated parts--a target level of safety, a collision risk analysis, a minimum navigation performance specifica ...
  • Program Validation of Lincoln Laboratory Microwave Landing System Math Model
    Program Validation of Lincoln Laboratory Microwave Landing System Math Model
    Jones, Jesse D.
    1981-03-01 | PDF
    The Microwave Landing System (MLS) mathematical model computer program developed by the Lincoln Laboratory of the Massachusetts Institute of Technology will be converted by Federal Aviation Administration (FAA) Technical Center personnel to operate on their Honeywell 66/60 computer. The program will be exercised at the Technical Center and at Linco ...
  • Summary of Transponder Data May 1979 Through November 1979
    Summary of Transponder Data May 1979 Through November 1979
    Greenberg, Max
    1981-02-01 | PDF
    The purpose of this effort was to determine the performance characteristics of air traffic control radar beacon transponders in an operational environment in general aviation aircraft. A transponder performance analyzer (TPA) was developed at the Federal Aviation Administration Technical Center to measure performance parameters of transponders inst ...
  • Wing Spillage Tests Using Antimisting Fuel
    Wing Spillage Tests Using Antimisting Fuel
    Salmon, Robert F.
    1981-02-01 | PDF
    Fuel spillage tests were conducted to evaluate the performance of an antimisting fuel (FM-9 with glycol/amine carrier fluid) in a simulated crash environment. The results of the tests are: (1) FM-9 when compared with neat Jet A afforded flammability protection even under test conditions which resulted in a "fail" for the FM-9; (2) 0.3% 80"F FM-9 pr ...
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