A set of test correlated mathematical models of the SSME High Pressure Oxygen Turbopump (HPOTP) housing and rotor assembly was produced. New analysis methods within the EISI/EAL and SPAR systems were investigated and runstreams for future use were developed. The LOX pump models have undergone extensive modification since the first phase of this effort was completed. The rotor assembly from the original model was abandoned and a new, more detailed model constructed. A description of the new rotor math model is presented. Also, the pump housing model was continually modified as additional test data have become available. This model is documented along with measured test results. Many of the more advanced features of the EAL/SPAR finite elemen...
A simulation study was conducted to examine the transient rotordynamics of the space shuttle main en...
Gasdynamic environments applied to the turbine blades and nozzles of the HPFTP and HPOTP were analyz...
The basic objectives of this contract were to perform detailed analysis and evaluation of dynamic da...
A mathematical model of the Space Shuttle Main Engine (SSME) as a complete assembly, with detailed e...
Rotational stability of turbopump components in the space shuttle main engine was studied via analys...
This structural dynamic analysis supports development of the SSME by evaluating components subjected...
A review is presented of various rotordynamic problems which have been encountered and eliminated in...
This volume summarizes the analysis used to assess the structural life of the Space Shuttle Main Eng...
To improve the Space Shuttle Main Engine (SSME) design and for future use in the development of gene...
The causes and remedies of vibration and subsynchronous whirl problems encountered in the Shuttle Ma...
The small, high pressure Mark 48 liquid hydrogen turbopump was analyzed and dynamically tested to de...
Full scale flow models with extensive instrumentation were designed and manufactured to provide data...
Integration issues involved with installing the alternate turbopump (ATP) High Pressure Oxygen Turbo...
The objective is to provide improved analysis capability for the Space Shuttle Main Engine (SSME) hi...
The analysis performed on the High Pressure Oxidizer Turbopump (HPOTP) preburner pump bearing assemb...
A simulation study was conducted to examine the transient rotordynamics of the space shuttle main en...
Gasdynamic environments applied to the turbine blades and nozzles of the HPFTP and HPOTP were analyz...
The basic objectives of this contract were to perform detailed analysis and evaluation of dynamic da...
A mathematical model of the Space Shuttle Main Engine (SSME) as a complete assembly, with detailed e...
Rotational stability of turbopump components in the space shuttle main engine was studied via analys...
This structural dynamic analysis supports development of the SSME by evaluating components subjected...
A review is presented of various rotordynamic problems which have been encountered and eliminated in...
This volume summarizes the analysis used to assess the structural life of the Space Shuttle Main Eng...
To improve the Space Shuttle Main Engine (SSME) design and for future use in the development of gene...
The causes and remedies of vibration and subsynchronous whirl problems encountered in the Shuttle Ma...
The small, high pressure Mark 48 liquid hydrogen turbopump was analyzed and dynamically tested to de...
Full scale flow models with extensive instrumentation were designed and manufactured to provide data...
Integration issues involved with installing the alternate turbopump (ATP) High Pressure Oxygen Turbo...
The objective is to provide improved analysis capability for the Space Shuttle Main Engine (SSME) hi...
The analysis performed on the High Pressure Oxidizer Turbopump (HPOTP) preburner pump bearing assemb...
A simulation study was conducted to examine the transient rotordynamics of the space shuttle main en...
Gasdynamic environments applied to the turbine blades and nozzles of the HPFTP and HPOTP were analyz...
The basic objectives of this contract were to perform detailed analysis and evaluation of dynamic da...