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  2. Aircraft design process - Wikipedia

    en.wikipedia.org/wiki/Aircraft_design_process

    Aircraft design process. The aircraft design process is a loosely defined method used to balance many competing and demanding requirements to produce an aircraft that is strong, lightweight, economical and can carry an adequate payload while being sufficiently reliable to safely fly for the design life of the aircraft.

  3. Lofting - Wikipedia

    en.wikipedia.org/wiki/Lofting

    Lofting is a drafting technique to generate curved lines. It is used in plans for streamlined objects such as aircraft and boats. The lines may be drawn on wood and the wood then cut for advanced woodworking. The technique can be as simple as bending a flexible object, such as a long strip of thin wood or thin plastic so that it passes over ...

  4. DO-178B - Wikipedia

    en.wikipedia.org/wiki/DO-178B

    DO-178B, Software Considerations in Airborne Systems and Equipment Certification is a guideline dealing with the safety of safety-critical software used in certain airborne systems. It was jointly developed by the safety-critical working group RTCA SC-167 of the Radio Technical Commission for Aeronautics (RTCA) and WG-12 of the European ...

  5. CADAM - Wikipedia

    en.wikipedia.org/wiki/CADAM

    Website. www.cadam.com. CADAM (computer-augmented design and manufacturing) is CAD -related software that was developed by Lockheed. [1] CADAM was originally written for IBM mainframes and later ported to UNIX workstations, including the IBM RT PC. A variant of CADAM called Micro CADAM was also developed for PCs under DOS.

  6. ARINC 653 - Wikipedia

    en.wikipedia.org/wiki/ARINC_653

    ARINC 653. ARINC 653 (Avionics Application Software Standard Interface) is a software specification for space and time partitioning in safety-critical avionics real-time operating systems (RTOS). It allows the hosting of multiple applications of different software levels on the same hardware in the context of an Integrated Modular Avionics ...

  7. DO-178C - Wikipedia

    en.wikipedia.org/wiki/DO-178C

    DO-178C. DO-178C, Software Considerations in Airborne Systems and Equipment Certification is the primary document by which the certification authorities such as FAA, EASA and Transport Canada approve all commercial software-based aerospace systems. The document is published by RTCA, Incorporated, in a joint effort with EUROC and replaces DO-178B.

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