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Development of High Temperature Seal-Lubricant Deposit Evaluation Techniques
Report Number: AFAPL TR 65-3
Author(s): Pfoutz, Billy D.; Knox, William G.; Gannon, Frank
Corporate Author: Koppers Co Inc Monroeville PA
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/3/1965
Pages: 23
Features: + Graph(s) + Table(s)
Contract: AF 33(615)-1112
Project: 3044
Task: 304401
AD Number: AD0617072
Photo Enhancement: Not Needed
Abstract Text:
Testing techniques for evaluating experimental gas turbine lubricants in face-riding main shaft jet engine seals at temperatures representative of high mach aircraft have been under development. Using the ASD Seal Rig, repeatable evaluation techniques were developed for MIL-L-9236 type lubricants that were indicative of performance in engines. The present phase of the program is directed towards refining evaluation equipment and preparing the rig for more advanced research work. During the period covered, internal seal head air heating to 1160F, preliminary evaluation studies using 0-60-19 and 0-60-18 lubricants, and engineering features of a new seal head design were investigated. An adaptor to permit the use of the seal head with Erdco test equipment is being designed.
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Storage Stability Of High Temperature Fuels
Report Number: AFAPL TR 65-13 Part 3
Author(s): Whisman, M. L.; Ward, C. C.
Corporate Author: Bureau Of Mines Bartlesville Okla Petroleum Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 2/1/1967
Pages: 95
Features: + Diagram(s) + Graph(s) + Table(s)
Contract: DO(33-615)-64-1009
Project: 3048
Task: 304801
AD Number: AD0647787
Photo Enhancement: Not Needed
Abstract Text:
The report covers an investigation of the influence of fuel constituents during storage on thermal stability of JP-6 and other high temperature fuels. The major objectives of the program were satisfied by the successful development and evaluation of several methods utilizing radiotracers to determine the causes of thermal instability as well as predicting thermal stability quality of high temperature fuels during storage. Ninety-four test blends of 12 fuels and 9 radioactive fuel compounds were prepared and tested in the evaluation of a microscale thermal stability procedure developed for the purpose of determining the contribution of selected fuel components to thermally induced deposits. Eight-eight of these test blends were retested after 26 weeks storage at 130F to determine the effect of storage upon deposit-forming tendencies. Analysis of the data obtained in this study resulted in a further study of thermal decomposition of a fuel antioxidant additive. An investigation of several variables associated with an in situ hydrogenation method using tritium as the index of reactivity was completed as an effort to develop a sensitive and accurate analytical technique for very low concentrations of olefins in hydrocarbon fuels. In addition, initial steps were taken toward obtaining or synthesizing radioactive materials and reference standards essential to a continuation of this program along a similar line of approach.
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Rotor-Bearing Dynamics Design Technology. Part VII: The Three Lobe Bearing And Floating Ring Bearing
Report Number: AFAPL TR 65-45 Part 7
Author(s): Lund, J. W.
Corporate Author: Mechanical Technology Inc Latham NY
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 2/1/1968
Pages: 292
Contract: AF 33(615)-3238
Project: 3048
Task: 304806
AD Number: AD0829895
Photo Enhancement: Not Needed
Abstract Text:
The volume treats three special bearing types selected for study because of their favorable stability characteristics and, hence, their potential for use in high speed rotating machinery applications. The three bearing types are: (a) The Three Lobe Journal Bearing; (b) The Floating Sleeve Bearing with an Incompressible Lubricant; (c) The Floating Sleeve Bearing with a Compressible Lubricant. In the floating sleeve bearings, the ring is prevented from rotating but is otherwise free to move. The ring is floated by pressurizing the outer film of the bearing. In the case of a compressible lubricant, the inner film is pressurized as well. The volume gives extensive design data in form of charts and tables from which the bearing dimensions can be obtained for a given application. Data are given for bearing flow, friction power loss and the speed at which hydrodynamic instability sets in. In addition, two computer programs accompany the volume, and instructions and listings of the programs are included. The programs may be used to obtain data for cases not covered by the presented design data.
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Investigation of RF Radiation as a Secondary Phenomenon for Use in Checkout
Report Number: AFAPL TR 65-46
Author(s): James W. Ballard; Eugene F. Horn
Corporate Author: Systems Research Laboratories, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 6/1/1965
Pages: 105
Features: + Diagram(s) + Foldout(s) + Graph(s) + Photo(s) + Table(s)
Contract: AF 33(615)-1489
Project: 8119
Task: 811925
AD Number: AD0619899
Photo Enhancement: Complete
Abstract Text:
The emission of radio-frequency (rf) radiation was studied over a range of frequencies from .15 to 400 megacycles per second (Mc/sec) for small gaps of .5 to 10 mils. The electrodes were .050-inch in diameter with polished plane ends which formed the gap. Most of the work reported was done in air at atmospheric pressure with nickel electrodes although argon gas and gold, aluminum, and copper electrodes were employed. Considerable attention was given to shielding, and the effect of receiver and generator circuitry. The effect of antennas and cables were also studied in relation to rf radiation emission and reception. Radiation from malfunctioning systems is attributed to a brush type discharge across very small discontinuities within the electrical parts. These discontinutities in a number of cases were found to be essentially contact, i.e. less than a few thousand angstroms. The mechanism causing breakdown was found to be the avalanche type with the involvement of secondary electronic emission.
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Aerospace Expandable Stuctures. Conference Transactions
Report Number: AFAPL TR 65-108
Author(s):
Corporate Author: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 803
Project: 0
Task: 0
AD Number: AD0631406
Photo Enhancement: Complete
Abstract Text:
The report is based upon the discussions at the Conference held at the Lafayette Club, Minnetonka Beach, Minnesota. The subject matter has been arranged in six sessions in the order of presentation at the conference, followed by six papers which were not given at the conference.
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Introduction and Table of Contents
Report Number: AFAPL TR 65-108 p. i-xiii
Author(s):
Corporate Author:
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 13
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Expandable Structures Design Concepts for Astronaut Transfer
Report Number: AFAPL TR 65-108 p. 1-18
Author(s): Jurich, L., Forbes, F. W., Schofield, J. Hribar, V. F.
Corporate Author: Aero Propulsion Laboratory; Aero Medical Laboratory; Aerospace Corporation; Goodyear Aerospace Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 18
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Development and Optimization of a Resin System for Rigidization
Report Number: AFAPL TR 65-108 p. 19-49
Author(s): McKillip, W, J., Leitheiser, R. H., Clemens, L. M., Impola, C. N., Lee, J.
Corporate Author: Archer Daniels Midland Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 31
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Application of Expandable Honeycomb to Fabrication of Space Structures
Report Number: AFAPL TR 65-108 p. 50-73
Author(s): Russell, I. W., Koons, C.
Corporate Author: GCA Corporation; Experimental Fabrication Division, WPAFB
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 24
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Lightweight, Expandable Support Shelter Systems
Report Number: AFAPL TR 65-108 p. 75-103
Author(s): Alexander, J. M.
Corporate Author: University of Cincinnati
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 29
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Bare Base Development Concepts
Report Number: AFAPL TR 65-108 p. 104-139
Author(s): Merkel, K. H., Alexander, J. M., Born, G. C.
Corporate Author: University of Cincinnati
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 36
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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'Ratio' Automated Assembly Technique for Space Structures
Report Number: AFAPL TR 65-108 p. 141-163
Author(s): Slysh, P.
Corporate Author: General Dynamics/Convair
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 23
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Chemical Rigidization of Preformed Flexible Foams
Report Number: AFAPL TR 65-108 p. 165-178
Author(s): Hanny, J. F.
Corporate Author: National Cash Register Company
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 24
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Maintenance Technology for Space Systems
Report Number: AFAPL TR 65-108 p. 179-197
Author(s): May, C. B.
Corporate Author: Air Force Aero Propulsion Laboratory
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 19
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Structural Considerations for an Expandable Lenticular Satellite
Report Number: AFAPL TR 65-108 p. 199-213
Author(s): Humble, J. L.
Corporate Author: NASA Langley Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 14
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Application of Inflatable Structures to Station Keeping of Passive Communications Satellites
Report Number: AFAPL TR 65-108 p. 215-233
Author(s): Cooper, J. E.
Corporate Author: NASA Langley Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 19
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Development of Manufacturing Techniques for a Metal Fabric Reinforced Re-entry Paraglider
Report Number: AFAPL TR 65-108 p. 235-247
Author(s): Keville, J. F.
Corporate Author: Space-General Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 13
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Bending of Unfurlable Tubular Structures in Space
Report Number: AFAPL TR 65-108 p. 249-263
Author(s): Herzl, G. G.
Corporate Author: Philco Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 15
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Development and Evaluation of a Rigidized Inflatable Microwave Reflector
Report Number: AFAPL TR 65-108 p. 265-287
Author(s): Gibson, K. F., Peace, G. M.
Corporate Author: Computing Devices of Canada, Ltd.; Bendix Corporation Research Laboratories
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 23
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Sodium Silicate as a Versatile Structural Material
Report Number: AFAPL TR 65-108 p. 289-303
Author(s): Hoffman, H. I.
Corporate Author: Southwest Research Institute
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 15
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Inflatable Thermal Radiation Shield for Space Application
Report Number: AFAPL TR 65-108 p. 305-338
Author(s): Marshall, J. E.
Corporate Author: General Dynamics/Fort Worth
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 34
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Predistributed Foam for Rigidizing Membrane Structures in Space
Report Number: AFAPL TR 65-108 p. 339-361
Author(s): Jouriles, N.
Corporate Author: Goodyear Aerospace Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 23
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Semi-rigid Structures for Space Applications: Expandable Space Structure
Report Number: AFAPL TR 65-108 p. 362-295
Author(s): Knox, P. M., Omer Moses, R.
Corporate Author: Martin Company
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 34
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Buildings in Barrels, Part III
Report Number: AFAPL TR 65-108 p. 397-428
Author(s): Swensen, S.B.
Corporate Author: U.S. Army Engineer Research and Development Laboratories
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 32
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Metal Fabrics for Aerospace Expandable Structures
Report Number: AFAPL TR 65-108 p. 429-446
Author(s): Freeston Jr., W. D.
Corporate Author: Fabric Research Laboratories, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 18
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Simulation of Meteoroid Impact Effects on Expandable Structures
Report Number: AFAPL TR 65-108 p. 447-466
Author(s): Holten, A. J.
Corporate Author: None Given
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 20
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Development of an Expandable Airlock Utilizing the Elastic Recovery Principle
Report Number: AFAPL TR 65-108 p. 467-496
Author(s): Williams, J., Brink, N. O.
Corporate Author: NASA Langley Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 30
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Potential Applications for Expandable and Inflatable Structures for Re-entry Vehicles
Report Number: AFAPL TR 65-108 p. 497-518
Author(s): Wykes, R. P.
Corporate Author: North American Aviation, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 22
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Compression Tests of Wire-Film Cylinders
Report Number: AFAPL TR 65-108 p. 519-535
Author(s): Rottmayer, E.
Corporate Author: Goodyear Aerospace Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 17
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Design Criteria for Inflated, Expandable Beams Used as Structural Members in an Advanced Concept Paraglider
Report Number: AFAPL TR 65-108 p. 537-554
Author(s): Toni, R. A., McNulty, J. F.
Corporate Author: NASA Langley Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 18
Contract: None Given
Project: None Given
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AD Number: See AD0631406
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Development of Space Expanded and Rigidized Solar Energy Collectors
Report Number: AFAPL TR 65-108 p. 555-571
Author(s): Schwartz, S.
Corporate Author: Hughes Aircraft Company
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 17
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Aluminum Foil Expandable Structures
Report Number: AFAPL TR 65-108 p. 572-602
Author(s): Motta, S.
Corporate Author: Avco Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 31
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Fabrication and Pressurization Technology for Improvement of Surface Accuracy of Passive Communications Satellites
Report Number: AFAPL TR 65-108 p. 603-616
Author(s): Grana, D. C.
Corporate Author: NASA Langley Research Center
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 14
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Membrane Analysis of Pressurized Thin Spheroid Shells Composed of Flat Gores and Its Application to Echo II
Report Number: AFAPL TR 65-108 p. 617-631
Author(s): Bahiman, H., Thole, J. M.
Corporate Author: None Given
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 15
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Astronaut Maneuvering Unit Technology
Report Number: AFAPL TR 65-108 p. 633-648
Author(s): Van Schaik, P. N.
Corporate Author: Air Force Aero Propulsion Laboratory
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 16
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Deployment System for the Pegasus Meteoroid Technology Satellite
Report Number: AFAPL TR 65-108 p. 649-657
Author(s): Ganssle, E. R.
Corporate Author: Fairchild Hiller Corp.
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 9
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Structural Behavior of Tapered Inflated Fabric Cylinders Under Various Loading Conditions
Report Number: AFAPL TR 65-108 p. 659-685
Author(s): Kovalesvsky, L., Rish, F. L.
Corporate Author: North American Aviation, Inc.
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 27
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Satellite Applications for Expandable Space Structures
Report Number: AFAPL TR 65-108 p. 687-707
Author(s): Zahn, H. S.
Corporate Author: Martin Company
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 21
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Recent Applications of Inflated Structures to Aerospace Vehicles
Report Number: AFAPL TR 65-108 p. 709-739
Author(s): Ross, R. S.
Corporate Author: Good Year Space Corp.
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 31
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Correlation of Analytical and Experimental Results of Cylindrical Shells Under Newtonian Pressure Distribution
Report Number: AFAPL TR 65-108 p. 740-767
Author(s): Lycurgus, N. C., Midgley, W. R.
Corporate Author: None Given
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 28
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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High-Temperature Protective Re-entry Coatings for Expandable Structures
Report Number: AFAPL TR 65-108 p. 769-783
Author(s): Conger, M. T., Chalmers, T. W.
Corporate Author: None Given
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 15
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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Dual Wall Inflatable Structures for Space Oriented Applications
Report Number: AFAPL TR 65-108 p. 785-802
Author(s): Bair, H. Q., Fischer, W. H.
Corporate Author: Air Inflatable Products Corporation
Laboratory: Air Force Aero Propulsion Laboratory
Publication Date: 5/27/1965
Pages: 18
Contract: None Given
Project: None Given
Task: None Given
AD Number: See AD0631406
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