• Thumbnail for Ascent Abort-2
    Ascent Abort-2 (AA-2) was a test of the launch escape system (LAS) of NASA's Orion spacecraft. The test followed Orion's Pad Abort-1 test in 2010, and...
    5 KB (409 words) - 10:51, 1 November 2023
  • Thumbnail for Cape Canaveral Space Launch Complex 46
    2017. On July 2, 2019, NASA launched a repurposed Peacekeeper missile from SLC-46, carrying the Orion spacecraft for the Ascent Abort-2 mission. The mission's...
    10 KB (874 words) - 22:01, 15 July 2024
  • Thumbnail for Space Shuttle abort modes
    liftoff. An abort during ascent that would result in the orbiter returning to a runway or to an orbit lower than planned was called an "intact abort", while...
    43 KB (5,202 words) - 18:20, 24 September 2024
  • Thumbnail for Orion (spacecraft)
    Pad Abort 1 An Orion boilerplate was used for the Pad Abort 1 flight test, the LAS was fully functional, the boilerplate was recovered. Ascent Abort-2 An...
    109 KB (8,697 words) - 07:36, 26 September 2024
  • Thumbnail for Crew Dragon In-Flight Abort Test
    II Mercury-Atlas 3 Crew Dragon Pad Abort Test Orion Pad Abort 1 and Ascent Abort 2 Boeing Pad Abort Test Soyuz abort modes TV-D1 Wikimedia Commons has...
    18 KB (1,642 words) - 19:39, 26 September 2024
  • AA2 (redirect from AA-2 (disambiguation))
    credit rating given by Moody's Investors Service Ascent Abort-2, a 2019 flight test of the launch abort system of NASA's Orion spacecraft This disambiguation...
    921 bytes (156 words) - 06:52, 6 May 2022
  • Thumbnail for Artemis program
    at 32,000 km/h (20,000 mph). The Ascent Abort-2 test on 2 July 2019 tested the final iteration of the launch abort system on a 10,000 kg (22,000 lb)...
    188 KB (17,812 words) - 17:02, 26 September 2024
  • less violent phases of the ascent, the EDS was turned off and an abort would have to be initiated manually. Of the five abort modes, the modes up to three...
    9 KB (1,339 words) - 10:32, 30 August 2024
  • Thumbnail for Apollo Abort Guidance System
    Module's primary guidance system (Apollo PGNCS) during descent, ascent or rendezvous. As an abort system, it did not support guidance for a lunar landing. The...
    13 KB (1,761 words) - 16:06, 7 July 2024
  • Thumbnail for Launch escape system
    ascent. The engines, which use hypergolic propellants and generate 40,000 pounds-force of thrust each, are provided by Aerojet Rocketdyne. The abort system...
    17 KB (1,835 words) - 11:38, 17 September 2024