Results 111 to 120 of about 5,519 (211)

Turbomachinery shaft insert [PDF]

open access: yes
An insert is presented for a hollow rotatable shaft on the end of which an impeller is mounted, the insert having a first cylindrical portion receivable within the end of the shaft. The insert includes a radially extending portion adjacent the end of the
Vonpragenau, George L.
core   +1 more source

Steady-state attitude control propulsion systems computer program documentation and user's manual, volume 1 [PDF]

open access: yes
Computer program documentation and user manual for steady state attitude control propulsion system - vol.
Thompson, P. F., Turley, R. C.
core   +2 more sources

Advanced expander test bed engine [PDF]

open access: yes
The Advanced Expander Test Bed (AETB) is a key element in NASA's Space Chemical Engine Technology Program for development and demonstration of expander cycle oxygen/hydrogen engine and advanced component technologies applicable to space engines as well ...
Mitchell, J. P.
core   +1 more source

Investigation of cavitation damage of a mechanical pump impeller in high temperature potassium quarterly progress report no. 1, 7 dec. 1964 - 28 feb. 1965 [PDF]

open access: yes
Cavitation damage prediction from mixed flow centrifugal pump impeller in endurance testing in high temperature ...
Altieri, J. V., Kulp, R. S.
core   +1 more source

Hybrid bearings for LH2 and LO2 turbopumps [PDF]

open access: yes
Hybrid combinations of hydrostatic and ball bearings can improve bearing performance for liquid hydrogen and liquid oxygen turbopumps. Analytic studies were conducted to optimize hybrid bearing designs for the SSME-type turbopump conditions.
Butner, M. F., Lee, F. C.
core   +1 more source

Liquid rocket turbopump.

open access: yesJournal of the Japan Society for Aeronautical and Space Sciences, 1988
Kenjiro KAMIJO, Masataka NOSAKA
openaire   +2 more sources

Study of inducer load and stress Interim report, 15 Feb. 1968 - 15 Oct. 1968 [PDF]

open access: yes
Literature survey, analytic formulations, and test rig designs for cavitating inducers in rocket engine ...
Barten, H. J.   +2 more
core   +1 more source

Computational analysis of the SSME fuel preburner flow [PDF]

open access: yes
A computational fluid dynamics model which simulates the steady state operation of the SSME fuel preburner is developed. Specifically, the model will be used to quantify the flow factors which cause local hot spots in the fuel preburner in order to ...
Farmer, R. C., Wang, T. S.
core   +1 more source

Wetting state and mechanical property alteration for the Fe<sub>3</sub>Si films using rapid thermal annealing under various temperatures. [PDF]

open access: yesHeliyon, 2023
Borwornpornmetee N   +7 more
europepmc   +1 more source

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