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  2. Launch vehicle system tests - Wikipedia

    en.wikipedia.org/wiki/Launch_vehicle_system_tests

    Furthermore, due to extensive fire, the SLC-40 launch pad was heavily damaged and had to be rebuilt. [10] [11] Static fire test failures have resulted in the unintentional launch of the test vehicle. On June 6th, 1952, Viking 8 broke loose of its moorings during a static fire test. After 55 seconds of flight, a command was sent to cut ...

  3. Category:Aerospace system testing - Wikipedia

    en.wikipedia.org/wiki/Category:Aerospace_system...

    Pages in category "Aerospace system testing" The following 6 pages are in this category, out of 6 total. ... Static fire; T. Tethered flight test; W. Wet dress rehearsal

  4. ARP4761 - Wikipedia

    en.wikipedia.org/wiki/ARP4761

    ARP4761, Guidelines for Conducting the Safety Assessment Process on Civil Aircraft, Systems, and Equipment is an Aerospace Recommended Practice from SAE International. [1]

  5. Verification (spaceflight) - Wikipedia

    en.wikipedia.org/wiki/Verification_(spaceflight)

    Large aerospace corporations may also developed their own internal standards. These standards exist in order to specify requirements for the verification of a space system product, such as: [1] the fundamental concepts of the verification process; the criteria for defining the verification strategy and

  6. Range safety - Wikipedia

    en.wikipedia.org/wiki/Range_safety

    A separate 'fire' command detonates explosives, typically linear shaped charges, to disable the rocket. [3] Reliability is a high priority in range safety systems, with extensive emphasis on redundancy and pre-launch testing. Range safety transmitters operate continuously at very high power levels to ensure a substantial link margin. The signal ...

  7. AC 25.1309-1 - Wikipedia

    en.wikipedia.org/wiki/AC_25.1309-1

    ARP4761, Guidelines for Conducting the Safety Assessment Process on Civil Aircraft, Systems, and Equipment describes recommended processes for assessing safety for new aircraft and equipment design as well as significant changes to existing designs for compliance with the safety requirements of FAR 25.1309 and FAR 23.1309. [4]