Author: S. A. LowryPublisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 144
Book Description
Space Shuttle Main Engine High Pressure Fuel Pump Aft Platform Seal Cavity Flow Analysis
Author: S. A. LowryPublisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 144
Book Description
Space Shuttle Main Engine High Pressure Fuel Pump Aft Platform Seal Cavity Flow Analysis
Author: S. A. LowryNASA Technical Paper
Author: NASA Scientific and Technical Publications
Author: Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 882
Book Description
Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1480
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1126
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Space Shuttle Main Engine Structural Analysis and Data Reduction/Evaluation. Volume 4
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722755317
Category :
Languages : en
Pages : 100
Book Description
The analysis performed on the Space Shuttle Main Engine (SSME) High Pressure Fuel Turbopump (HPFTP) inlet housings is summarized. Three DIAL finite element models were build to aid in assessing the structural life of the welds and fillets at the vanes. Complete results are given. Pool, Kirby V. Unspecified Center...
Fluid Flow Analysis of the Ssme High Pressure Fuel and Oxidizer Turbine Coolant Systems
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722403737
Category :
Languages : en
Pages : 68
Book Description
The objective is to provide improved analysis capability for the Space Shuttle Main Engine (SSME) high pressure fuel and oxidizer turbine coolant systems. Each of the systems was analyzed to determine fluid flow rate and thermodynamic and transport properties at all key points in the systems. Existing computer codes were used as a baseline for these analyses. These codes were modified to provide improved analysis capability. The major areas of improvement are listed. A review of the drawings was performed, and pertinent geometry changes were included in the models. Improvements were made in the calculation of thermodynamic and transport properties for a mixture of hydrogen and steam. A one-dimensional turbine model for each system is included as a subroutine to each code. This provides a closed loop analysis with a minimum of required boundary conditions as input. An improved labyrinth seal model is included in the high pressure fuel turbine coolant model. The modifications and the analysis results are presented in detail. Teal, G. A. Unspecified Center...
Author: Paul E. Allaire