English
A summary of the overpressure environment from the 5% Ares I Scale Model Acoustic Test (ASMAT) and the implications to the full-scale Ares I are presented in this Technical Memorandum. These include the scaled environment that would be used for assessing the full-scale Ares I configuration, observations, and team recommendations. The ignition transient is first characterized and described, the overpressure suppression system configuration is then examined, and the final environment characteristics are detailed. The recommendation for Ares I is to keep the space shuttle heritage ignition overpressure (IOP) suppression system (below-deck IOP water in the launch mount and mobile launcher and also the crest water on the main flame deflector) and the water bags.
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Ebook · NASA Technical Reports Server (NTRS) 20120001328: Ares I Scale Model Acoustic Test Overpressure Results · NASA Technical Reports Server (NTRS) · Internet Archive
NASA Technical Reports Server (NTRS) · OVERPRESSURE · SCALE MODELS · ARES 1 LAUNCH VEHICLE · SPACE TRANSPORTATION SYSTEM · COMPUTATIONAL FLUID DYNAMICS · IGNITION · ACOUSTICS · BAGS · PRESSURE CHAMBERS