Add to ORKGTopics covered include: (1) pogo suppression for main propulsion subsystem operation; (2) application of quarter-scale low pressure oxidizer turbopump transfer functions; (3) pogo stability during orbital maneuvering subsystem operation; and (4) errors in frequency response measurements
Two dynamic pressure sources are described for the calibration of pogo pressure transducers used to ...
Abstract POGO instability is one of the most important dynamical problems of space vehicles. The mec...
Several accumulator designs and gas charge systems are considered in order to suppress POGO within t...
The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes...
An overview of more than 45 years of NASA human spaceflight experience is presented with respect to ...
The design guidelines were generated to support the selection of the baseline accumulator configurat...
The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes...
A dynamic (frequency response) analysis was made of a liquid oxygen feed system consisting of a low-...
Waterflow tests of a heritage Space Shuttle Main Engine pogo suppressor were performed to experiment...
Two methods of active pogo suppression (stabilization) for the space shuttle vehicle were studied an...
A frequency domain parameter optimization technique was used to design active pogo suppression contr...
The space shuttle introduced a new dimension in the complexity of the structural dynamics of a space...
Analytical model for use in design of pump inlet accumulators for prevention of liquid rocket longit...
Concept selection, design, fabrication, and testing of a Portable Subsystem (POS) for use in space s...
Pogo phenomenon is considered as low-frequency instability at system level in heavy satellite launch...
Two dynamic pressure sources are described for the calibration of pogo pressure transducers used to ...
Abstract POGO instability is one of the most important dynamical problems of space vehicles. The mec...
Several accumulator designs and gas charge systems are considered in order to suppress POGO within t...
The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes...
An overview of more than 45 years of NASA human spaceflight experience is presented with respect to ...
The design guidelines were generated to support the selection of the baseline accumulator configurat...
The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes...
A dynamic (frequency response) analysis was made of a liquid oxygen feed system consisting of a low-...
Waterflow tests of a heritage Space Shuttle Main Engine pogo suppressor were performed to experiment...
Two methods of active pogo suppression (stabilization) for the space shuttle vehicle were studied an...
A frequency domain parameter optimization technique was used to design active pogo suppression contr...
The space shuttle introduced a new dimension in the complexity of the structural dynamics of a space...
Analytical model for use in design of pump inlet accumulators for prevention of liquid rocket longit...
Concept selection, design, fabrication, and testing of a Portable Subsystem (POS) for use in space s...
Pogo phenomenon is considered as low-frequency instability at system level in heavy satellite launch...
Two dynamic pressure sources are described for the calibration of pogo pressure transducers used to ...
Abstract POGO instability is one of the most important dynamical problems of space vehicles. The mec...
Several accumulator designs and gas charge systems are considered in order to suppress POGO within t...