Add to ORKGAnalytical model for use in design of pump inlet accumulators for prevention of liquid rocket longitudal oscillatio
The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application
Linearized dynamic equations and mechanical model for propellant sloshing in Lunar Excursion Module ...
Analytical model for use in design of pump inlet accumulators for prevention of liquid rocket longit...
A modeling framework defined in the time-domain has been developed to characterize the steady state...
Several accumulator designs and gas charge systems are considered in order to suppress POGO within t...
Topics covered include: (1) pogo suppression for main propulsion subsystem operation; (2) applicati...
A dynamic (frequency response) analysis was made of a liquid oxygen feed system consisting of a low-...
This thesis has been carried out within the framework of the MIT-UNIPI Project funded by MISTI Globa...
Pogo phenomenon is considered as low-frequency instability at system level in heavy satellite launch...
Two methods of active pogo suppression (stabilization) for the space shuttle vehicle were studied an...
Stimulated by the pogo instability encountered in many liquid propellant rockets, the dynamic behavi...
When the propellants in a liquid rocket engine burn, the rocket not only launches and moves in space...
International audienceThe future developments of the Ariane rockets make it necessary to improve the...
AbstractProviding stability and dynamic quality of fuel systems is very important problem when devel...
The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application
Linearized dynamic equations and mechanical model for propellant sloshing in Lunar Excursion Module ...
Analytical model for use in design of pump inlet accumulators for prevention of liquid rocket longit...
A modeling framework defined in the time-domain has been developed to characterize the steady state...
Several accumulator designs and gas charge systems are considered in order to suppress POGO within t...
Topics covered include: (1) pogo suppression for main propulsion subsystem operation; (2) applicati...
A dynamic (frequency response) analysis was made of a liquid oxygen feed system consisting of a low-...
This thesis has been carried out within the framework of the MIT-UNIPI Project funded by MISTI Globa...
Pogo phenomenon is considered as low-frequency instability at system level in heavy satellite launch...
Two methods of active pogo suppression (stabilization) for the space shuttle vehicle were studied an...
Stimulated by the pogo instability encountered in many liquid propellant rockets, the dynamic behavi...
When the propellants in a liquid rocket engine burn, the rocket not only launches and moves in space...
International audienceThe future developments of the Ariane rockets make it necessary to improve the...
AbstractProviding stability and dynamic quality of fuel systems is very important problem when devel...
The asymmetric configuration of the space shuttle results in coupled pitch and axial vibration modes...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application
Linearized dynamic equations and mechanical model for propellant sloshing in Lunar Excursion Module ...