Design of thrust balancer minimizes leakage bypass and obviates need for conventional thrust balancer. System allows operation at low flow rates and high thrust capacity at cryogenic temperatures and high pressures.
Turbopump radial and axial rotor support system
01.06.1972
Sonstige
Keine Angabe
Englisch
Spring Support for Turbopump Rotor Bearing
NTRS | 1982
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|Rotor support for the STME oxygen turbopump
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|