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
1972-06-01
Miscellaneous
No indication
English
Spring Support for Turbopump Rotor Bearing
NTRS | 1982
|Rotor support for the STME oxygen turbopump
AIAA | 1992
|Damping Seals Would Help Support Turbopump Rotor
NTRS | 1991
|Rotor support for the STME oxygen turbopump
Tema Archive | 1992
|Heat Shield And Axial Retainer For Turbopump Blade
NTRS | 1990
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