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  • Quality Assurance and Reliability  (2)
  • FLUID MECHANICS AND HEAT TRANSFER  (1)
  • 1
    Publication Date: 2019-06-27
    Description: A model is presented which can be used to study the loss of lift during hovering and horizontal flight of the VTOL aircraft. The model numerically predicts the pressure distribution induced by a round, turbulent, unheated, subsonic jet exhausting normally through a flat plate into a subsonic crossflow. The complete model assumes that the predominant features of the flow are jet entrainment and a pair of contrarotating vortices which form downstream of the jet. Experimentally determined vortex properties and a reasonable assumption concerning jet entrainment were used. Potential flow considerations were used except in the wake region, where a simple method for approximating the pressure distribution was suggested. The calculated pressure distribution, lift, and pitching moments on the flat plate are presented for a jet to crossflow velocity ratio of 8 and were compared with experimental results. A computer program is given which was used to calculate the pressure distribution across the flat plate.
    Keywords: FLUID MECHANICS AND HEAT TRANSFER
    Type: NASA-CR-146434
    Format: application/pdf
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  • 2
    Publication Date: 2019-08-15
    Description: The space shuttle utilizes several rocket engine systems, all of which must function with a high degree of reliability for successful mission completion. The space shuttle main engine (SSME) is by far the most complex of the rocket engine systems and is designed to be reusable. The reusability of spacecraft systems introduces many problems related to testing, reliability, and logistics. Components must be assembled from parts inventories in a manner which will most effectively utilize the available parts. Assembly must be scheduled to efficiently utilize available assembly benches while still maintaining flight schedules. Assembled components must be assigned to as many contiguous flights as possible, to minimize component changes. Each component must undergo a rigorous testing program prior to flight. In addition, testing and assembly of flight engines and components must be done in conjunction with the assembly and testing of developmental engines and components. The development, testing, manufacture, and flight assignments of the engine fleet involves the satisfaction of many logistical and operational requirements, subject to many constraints. The purpose of the SSME Component Assembly and Life Management Expert System (CALMES) is to assist the engine assembly and scheduling process, and to insure that these activities utilize available resources as efficiently as possible.
    Keywords: Quality Assurance and Reliability
    Type: Overview of the Center for Advanced Space Propulsion; NASA-CR-199690
    Format: text
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  • 3
    Publication Date: 2019-08-15
    Description: The Space Shuttle utilizes several rocket engine systems, all of which must function with a high degree of reliability for successful mission completion. The Space Shuttle Main Engine (SSME) is by far the most complex of the rocket engine systems. In earlier spacecraft, rocket systems (and, in fact, the entire spacecraft) were designed for use on only a single mission and were discarded after use. In a major departure from earlier practices, almost all systems on the Space Shuttle, including the rocket systems, are designed to be reusable; only the external tank is discarded during each mission.
    Keywords: Quality Assurance and Reliability
    Type: Center for Advanced Space Propulsion; 61-69; NASA-CR-199689
    Format: text
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