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Flight Motor Set 360t004 Sts 30r Volume 1 System Overview
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Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781723080319 Total Pages :170 pages Book Rating :4.0/5 (83 download)
Book Synopsis Flight Motor Set 360t004 (Sts-30r). Volume 1 by : National Aeronautics and Space Administration (NASA)
Download or read book Flight Motor Set 360t004 (Sts-30r). Volume 1 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 170 pages. Available in PDF, EPUB and Kindle. Book excerpt: The fourth NASA space shuttle flight incorporating redesigned solid rocket motors began on 4 May 1989. The flight motors were designated 360Q004A (left-hand) and 360H004B (right-hand); the mission was designated STS-30R. Overall engine performance was excellent. The low sample rate data that was available showed exceptional propulsion performance. All ballistic and mass property parameters closely matched the predicted values and were well within the required contract end item specification levels that could be assessed. No strain, vibration, or aft skirt heating environments could be addressed due to developmental flight instrumentation deletion. Infrared readings from the shuttle thermal imager were considered very good when compared with ground environment instrumentation readings taken during both the aborted and the actual countdowns. However, hand-held infrared gun reading/ground environment instrumentation comparisons were considered poor during both countdowns, with the exception of the T - 3 hour timeframe during the actual launch. Postflight inspection again verified superior performance of the insulation, phenolics, metal parts, and seals. All combustion gas was contained by the insulation in the field and case-to-nozzle joints. Inadequate parachute performance on the left-hand booster caused high splashdown loads, which resulted in a displaced nozzle and factory joint weatherseal unbond anomalies. Recommendations were made concerning improved thermal modeling and instruments. The rationale for these recommendations, the dispositions of all anomalies, and complete result details are given. Ricks, Glenn A. Unspecified Center COMBUSTION; FLIGHT INSTRUMENTS; INFRARED INSTRUMENTS; INSPECTION; PROPULSION; SOLID PROPELLANT ROCKET ENGINES; SPACE SHUTTLES; SPACE TRANSPORTATION SYSTEM FLIGHTS; ANOMALIES; COUNTDOWN; DELETION; GENERAL OVERVIEWS; HEATING; INFRARED RADIATION; INSULATION; LAUNCHING; LOADS (FORCES); PARACHUTES; SKIRTS; SPECIFICATIONS; VIBRATION...