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Combustion of lox with Hb2(sgb)s under subcritical, critical and supercritical conditions (task 1) a

University Park, PA : Propulsion Engineering Research Center, Pennsylvania State University ; Huntsville, Ala. : NASA Marshall Space Flight Center, [1992] 1992

NASA Flexible Screen Propellant Management Device (PMD) demonstration with cryogenic liquid

Wollen, Mark.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

Nonlinear rotordynamics analysis

Day, William B., author.
Marshall Space Flight Center, AL : George C. Marshall Space Flight Center, 1985. 1985

Orbital transfer vehicle oxygen turbopump technology. final report

[Washington, D.C.] : National Aeronautics and Space Administration, [1990] 1990

Pressure-volume-temperature (PVT) gauging of an isothermal cryogenic propellant tank pressurized wit

Van Dresar, Neil T., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2014. 2014-

Risk assessment and scaling for the SLS LOx ET

Osipov, Viatcheslav (Slava), author.
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, 2012. 2012

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

Huntsville, Ala. : SRS Technologies, Systems Technology Division ; Marshall Space Flight Center, Ala. : Materials and Processes Laboratory, Engineering Physics Division, George C. Marshall Space Flight Center, [1986] 1986

SSME LOX post flow analysis/fluid structure interaction final report.

Huntsville, AL : Lockheed Missiles & Space Co. ; [Washington, D.C. : National Aeronautics and Space Administration, 1989] 1989

SSME LOX post flow analysis/fluid structure interaction

Burke, R. W.
Huntsville, AL : Lockheed Missiles and Space Co., Huntsville Engineering Center ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfieldl, Va. : National Technical Information Service, distributor, 1989] 1989

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

Romano, E.
[Canoga Park, Calif. : Rockwell International, Rocketdyne Division? ; Washington, D.C. : National Aeronautics and Space Administration?. 1989?] 1989

A superconducing quenchgun for delivering lunar derived oxygen to lunar orbit

Nottke, Nathan.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990] 1990

Turbomachinery incipient failure detection indicators and analysis

Faby, D.R.
Latham, N.Y. : Shaker Research Corporation ; [Huntsville, Ala.] : National Aeronautics & Space Administration, George C. Marshall Space Flight Center, [1985] 1985