1–20 of 643 hits
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    F/A-18E/F Program Update

    Clark, C. / Glaser, B. / Society of Flight Test Engineers | British Library Conference Proceedings | 1996

    Nickel Alloy, Brazing Filler Metal 73Ni - 0.75C - 4.5Si - 14Cr - 3.1B - 4.5Fe 1790 °F (977 °C) Solidus to 1970 °F (1077 °C) Liquidus

    SAE Technical Papers | 2018
    suitable binder. AMS4775K incorporates industry standard requirements of AWS A5.8, revises Title, Burn-off of Binder (3.3.1.1, 3.3.2.2) Powder ...

    Nickel Alloy, Brazing Filler Metal 82Ni - 4.5Si - 7.0Cr - 3.1B - 3.0Fe 1780 °F (971 °C) Solidus to 1830 °F (999 °C) Liquidus Range

    SAE Technical Papers | 2018
    suitable binder. AMS4777J incorporates industry standard requirements of AWS A5.8, revises Title, Burn-off of Binder (3.3.1.1, 3.3.2.2), Powder ...

    Nickel Alloy, Brazing Filler Metal 73Ni - 4.5Si - 14Cr - 3.1B - 4.5Fe (Low Carbon) 1790 °F (977 °C) Solidus to 1970 °F (1077 °C) Liquidus Range

    SAE Technical Papers | 2018
    suitable binder. AMS4776J incorporates industry standard requirements of AWS A5.8, revises Title, Burn-off of Binder (3.3.1.1, 3.3.2.1) Powder ...

    F/A-18 E/F Flight Test Program Overview

    Morgan, K. / Society of Flight Test Engineers | British Library Conference Proceedings | 1999

    F-22 Presentation

    Society of Flight Test Engineers | British Library Conference Proceedings | 1996

    Using Advanced F/T Technologies on a Radar F/T Program

    Maderer, Z. / Society of Flight Test Engineers | British Library Conference Proceedings | 1996

    F-22 Program Update

    Pieper, J. / Martin, L. / Society of Flight Test Engineers | British Library Conference Proceedings | 1999

    The space shuttle title: A new electronic substrate and radome material

    Gregorwich, W.S. | Tema Archive | 1983
    liquid nitrogen at -295 F and the reentry temperature of +2300 F. The excellent thermal performance of the TPS can be attributed to an extremely ...

    High Angle of Attack Control Law Development and Testing for the F/A-18E/F Super Hornet

    Heller, M. / Niewoehner, R. / Lawson, K. et al. | British Library Conference Proceedings | 1999

    Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 5080 psi (35000 kPa), 275 °F (135 °C), Aircraft Hydraulic Systems

    SAE Technical Papers | 2017
    in 275 °F (135 °C), 5080 psi (35000 kPa) aircraft hydraulic systems. Changed layline requirement, added hose assembly part standards from ...

    SEAL, PLAIN, RUBBER (HOT AIR RESISTANT 400 °F) MOLD IN GROOVE

    SAE Technical Papers | 2008
    OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ...

    Seek Eagle F-15E Mixed Loads Certification

    Baird, J. C. / Koper, E. / Smith, D. et al. | British Library Conference Proceedings | 1996

    Insert - Screw Thread, Thin Wall, Self-Locking, UNS N07718, Silver Plated, Class: 185 ksi/1025 °F, Procurement Specification

    SAE Technical Papers | 2019
    corrects an error in the paragraph title for the ‘as-received’ self-locking torque test, Section 4 (Quality Assurance Provisions) has been ...

    Data Analysis System for the F-16

    Atkinson, G. F. / Austin, S. C. / IEEE et al. | British Library Conference Proceedings | 1997

    Aluminum Alloy, Sheet and Plate 4.4Cu - 1.5Mg - 0.60Mn (2024-O) Annealed; or when specified, “As Fabricated” (2024-F)

    SAE Technical Papers | 2017
    the annealed (O temper) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper. AMS4035M revises ...

    SEAL, PLAIN, RUBBER (-65 TO +350 °F FUEL RESISTANT) MOLD IN GROOVE

    SAE Technical Papers | 2008
    OF THE DOCUMENT TITLE INDICATES A COMPLETE REVISION OF THE DOCUMENT, INCLUDING TECHNICAL REVISIONS. CHANGE BARS AND (R) ARE NOT USED IN ...

    HOSE ASSEMBLY, POLYTETRAFLUOROETHYLENE, PARA ARAMID REINFORCED, 275 °F, 4000 MAX PSI, FLARELESS, TITANIUM FITTINGS, STRAIGHT TO STRAIGHT

    SAE Technical Papers | 2011
    REVISE TITLE FOR 4000 PSI MAX USAGE, REMOVED /21/ FROM FIG. 1, AND CORRECTED USAGE CHARACTERISTICS, MARKING, AND PROOF PRESSURE ...

    F-22 Avionic Test and Evaluation Standard File Format

    Barnum, J. / Society of Flight Text Engineers | British Library Conference Proceedings | 1997

    Aluminum Alloy, Sheet and Plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-O) Annealed or when specified, “As Fabricated” (2219-F)

    SAE Technical Papers | 2017
    thickness, supplied in the annealed (O) condition (see 8.4). When specified, product shall be supplied in the “as fabricated” (F) temper. AMS4031J ...