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3.1 This specification provides designers and manufacturers of electric propulsion for light sport aircraft design references and criteria to use in designing and manufacturing EPUs. 3.2 Declaration of compliance is based on testing and documentation during the design, ground testing and flight...
1.1 The digital reference images provided in the adjunct to this standard illustrate various types and degrees of discontinuities occurring in thin-wall steel investment castings.2 Use of this standard for the specification or grading of castings requires procurement of the adjunct digital...
1.1 The digital reference images provided in the adjuncts to this standard illustrate various types and degrees of discontinuities occurring in titanium castings.2 Use of this standard for the specification or grading of castings requires procurement of the appropriate adjunct digital reference...
This document specifies the requirements relating to: Heat resisting alloy X6NiCrTiMoV26-15 (1.4980) Softened and cold worked Wires for forged fasteners D ≤ 15 mm 900 MPa ≤ Rm ≤ 1 100 MPa for aerospace applications. W.nr: 1.4980. ASD-STAN designation: FE-PA2601.
1.1 This practice covers methods for instrumenting low-conductivity specimens for testing in an environment subject to rapid thermal changes such as produced by rocket motors, atmospheric re-entry, electric-arc plasma heaters, and so forth. Specifically, practices for bare-wire thermocouple...
The scope of this Recommended Standard is the specification of the binding in terms of technology mapping to TCP/IP of: a) MAL message; b) MAL Transport Interface. The MAL Blue Book (reference [1]) specifies the MAL protocol in an abstract way, i.e., without defining the concrete Protocol Data...
The scope of this Recommended Standard is the specification of the binding in terms of technology mapping to the HTTP and XML of: a) MAL message; b) MAL Transport Interface. The MAL Blue Book (reference [1]) specifies the MAL protocol in an abstract way, i.e., without defining the concrete protocol...
This document specifies the characteristics of thrust wire nuts for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa. Temperature range: −55 °C to 135 °C.
This document specifies the requirements relating to: Heat resisting nickel base alloy (NI-P100HT) Cold worked and softened Bar and wire for continuous forging or extrusion for fasteners 3 mm ≤ D ≤ 30 mm
This document specifies the requirements relating to: Heat resisting nickel base alloy Ni-P96-HT Cold drawn and precipitation treated Wire D ≤ 10 mm for aerospace applications.
This European Standard specifies the requirements relating to: Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1)
This Standard specifies: • Requirements for the following crimping wire connections intended for high reliability electrical connections for use on spacecraft and associated equipment operating under high vacuum, thermal cycling and launch vibration: - removable contacts, single wire...
