Cover Image

The structural dynamics analysis of the main injector LOX inlet tee and its redesign /

Bibliographic Details
Main Author:	Romano, E.
Corporate Authors:	Rockwell International. Rocketdyne Division, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	[Canoga Park, Calif.] : [Washington, D.C.] : [Rockwell International, Rocketdyne Division?] ; [National Aeronautics and Space Administration?], [1989?]
Series:	NASA contractor report ; NASA CR-186764.
Subjects:	Design analysis. Dynamic response. Dynamic structural analysis. Injectors. Intake systems. Liquid oxygen. Space shuttle main engine. T shape. Vanes.
Online Access:	https://purl.fdlp.gov/GPO/LPS69840

Similar Items

SSME LOX post flow analysis/fluid structure interaction.
by: Burke, R. W.
Published: (1989)

LOX/hydrogen coaxial injector atomization test program /
by: Zaller, M.
Published: (1990)

Space Shuttle main engine (SSME) LOX turbopump pump-end bearing analysis : final report.
Published: (1986)

Low loss injector for space shuttle main engine : final report /
by: Von Pragenau, George L.
Published: (1984)

Atomization and mixing study : interim report /
by: Ferrenberg, A.
Published: (1983)

Current status of superheat spray modeling with NCC /
by: Raju, M. S.
Published: (2012)

Duct flow nonuniformities study for Space Shuttle main engine : technical report /
by: Thoenes, Jürgen
Published: (1985)

Combustion performance and heat transfer characterization of lox/hydrocarbon type propellants : final report, volume I.
Published: (1983)

The effects of nonlinearities on the dynamic response of a large shuttle payload /
by: Sullivan, Timothy L.
Published: (1987)

Nonlinear rotordynamics analysis /
by: Day, William B.
Published: (1985)

Fuel injector design optimization for an annular scramjet geometry /
by: Steffen, Christopher J.
Published: (2003)

Fuel injector design optimization for an annular scramjet geometry /
by: Steffen, Christopher J.
Published: (2003)

Photographic study of liquid-oxygen boiling and gas injection in the injector of a chugging rocket engine /
by: Conrad, E. William, et al.
Published: (1964)

LOX/GOX related failures during space shuttle main engine development /
by: Cataldo, C. E.
Published: (1981)

Development of a device to deploy fluid droplets in microgravity /
by: Robinson, David W., et al.
Published: (1997)

Combustion performance and heat transfer characterization of lox/hydrocarbon type propellants : final report, volume II.
Published: (1983)

Advanced research and technology programs for advanced high-pressure oxygen-hydrogen rocket propulsion /
by: Marsik, Stanley J.
Published: (1985)

Advanced research and technology programs for advanced high-pressure oxygen-hydrogen rocket propulsion /
by: Marsik, Stanley J.
Published: (1985)

Turbomachinery incipient failure detection indicators and analysis /
by: Faby, D. R.
Published: (1985)

SSME structural dynamic model development : phase II, final report /
by: Foley, M. J.
Published: (1985)

Analysis of heat-transfer tests of an impingement-convection-and film-cooled vane in a cascade /
by: Gladden, Herbert J., et al.
Published: (1971)

Axial and centrifugal compressor mean line flow analysis method /
by: Veres, Joseph P.
Published: (2009)

NPSS multidisciplinary integration and analysis /
Published: (2006)

A computational study of multiple jet and wall interaction /
by: Campbell, Warren
Published: (1986)

A computational study of multiple jet and wall interaction /
by: Campbell, Warren
Published: (1986)

Assessment of some atomization models used in spray calculations /
by: Raju, M. S.
Published: (2011)

Developing uncertainty models for robust flutter analysis using ground vibration test data.
by: Potter, Starr
Published: (2001)

Developing uncertainty models for robust flutter analysis using ground vibration test data /
by: Potter, Starr, et al.
Published: (2001)

Space shuttle main engine vibration data base /
by: Lewallen, Pat
Published: (1986)

Engineering evaluation of SSME dynamic data from engine tests and SSV flights : final report /
Published: (1986)

A data base and analysis program for shuttle main engine dynamic pressure measurements : final report /
by: Coffin, Thomas
Published: (1986)

Space station hydrogen/oxygen thruster technology /
by: Briley, G. L.
Published: (1988)

Risk assessment and scaling for the SLS LOx ET /
by: Osipov, Viatcheslav (Slava)
Published: (2012)

Structural Dynamics Division research and technology accomplishments for FY 1989 and plans for FY 1990 /
by: Smith, Jacqueline G.
Published: (1990)

Multishaker modal testing /
by: Craig, Roy R., 1934-
Published: (1983)

Flutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept /
by: Scott, Robert C.
Published: (2009)

Thermomechanical response of shape memory alloy hybrid composites /
by: Turner, Travis L.
Published: (2001)

Thermomechanical response of shape memory alloy hybrid composites /
by: Turner, Travis L.
Published: (2001)

Analysis of internal flows relative to the space shuttle main engine : final report.
Published: (1988)

Analysis of internal flows relative to the space shuttle main engine : final report.
Published: (1987)