Add to ORKGRecommended procedures for stability, control, and structural loading analysis of large liquid fueled rocket booster sloshing parameter
Orbital investigation of liquid hydrogen dynamics in propellant tank of S-IVB stag
Study of resonant oscillations of an ideal fluid in a cylindrical tank is used to obtain a better un...
Mathematical models for determining longitudinal vibration modes of multistage liquid and solid prop...
Analytical methods for dynamic stability analyses of large launch vehicles during flight through and...
One of the challenges of developing flight control systems for liquid-propelled space vehicles is en...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application
A summary review of some of the technical issues which surround the design of the propulsion systems...
Liquid propellant behavior under space flight conditions and predicting Apollo spacecraft liquid sta...
Control and stability aspects prior to spacecraft landing, and propulsive assist to landing spacecra...
Ever since the launch of the early high-efficiency rockets, controlling liquid fuel slosh within a l...
Effect of propellant sloshing on stability of accelerometer controlled rigid space vehicl
Liquid sloshing and dynamics in rocket propellant tanks annotated bibliography with abstract
Issued as Monthly progress report, no.1-13, and Final report, Project no. A-767Contract no. NAS8-111...
The slosh dynamics of propellant tanks can be represented by an equivalent pendulum-mass mechanical ...
Ground tests of solid propellant rocket motors have shown that metal-containing propellants produce ...
Orbital investigation of liquid hydrogen dynamics in propellant tank of S-IVB stag
Study of resonant oscillations of an ideal fluid in a cylindrical tank is used to obtain a better un...
Mathematical models for determining longitudinal vibration modes of multistage liquid and solid prop...
Analytical methods for dynamic stability analyses of large launch vehicles during flight through and...
One of the challenges of developing flight control systems for liquid-propelled space vehicles is en...
Liquid propellant sloshing in tilted axisymmetric cylindrical tanks for space shuttle application
A summary review of some of the technical issues which surround the design of the propulsion systems...
Liquid propellant behavior under space flight conditions and predicting Apollo spacecraft liquid sta...
Control and stability aspects prior to spacecraft landing, and propulsive assist to landing spacecra...
Ever since the launch of the early high-efficiency rockets, controlling liquid fuel slosh within a l...
Effect of propellant sloshing on stability of accelerometer controlled rigid space vehicl
Liquid sloshing and dynamics in rocket propellant tanks annotated bibliography with abstract
Issued as Monthly progress report, no.1-13, and Final report, Project no. A-767Contract no. NAS8-111...
The slosh dynamics of propellant tanks can be represented by an equivalent pendulum-mass mechanical ...
Ground tests of solid propellant rocket motors have shown that metal-containing propellants produce ...
Orbital investigation of liquid hydrogen dynamics in propellant tank of S-IVB stag
Study of resonant oscillations of an ideal fluid in a cylindrical tank is used to obtain a better un...
Mathematical models for determining longitudinal vibration modes of multistage liquid and solid prop...