Download or read book Propellant Slosh Loads written by United States. National Aeronautics and Space Administration and published by . This book was released on 1968 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Propellant Slosh Loads written by and published by . This book was released on 2000 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Propellant Slosh Loads written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Space Vehicle Design Criteria structures Propellant Slosh Loads written by and published by . This book was released on 1968 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Propellant slosh loads written by and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Space Vehicle Design Criteria structures written by and published by . This book was released on 1968 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Comparison of Propellant Sloshing Parameters Obtained from Model and Full size Centaur Liquid oxygen Tanks written by Andrew J. Stofan and published by . This book was released on 1966 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Dynamic Effects of Propellant Slosh on a Planetary Lander with Transient Mass Properties written by Thomas William Carlson and published by . This book was released on 2012 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt: NASA is currently in development of a vertical test bed vehicle demonstrating new green propellant propulsion systems and autonomous landing and hazard detection technology. The vehicle is required to land on the Earth's surface without the aid of parachutes using a single gimbaled LOX/Methane engine to control its descent. One of the many challenges of this system is the ability to control the descent while the vehicle is exposed to external and internal disturbances, and under changing mass properties (propellant consumption). In order to develop a suitable control system, the maximum expected magnitude of the disturbance inputs must be predicted. One such disturbance is the propellant slosh created during vehicle accelerations. This paper analyzes the effects of propellant slosh on the rigid body motion of the vehicle for both liquid methane (fuel) and liquid oxygen (oxidizer) residing in spherical propellant tanks containing cruciform and rigid ring baffles. This was accomplished by analysis and software simulation. The results are compared with the NASA models as well as existing historical data. With a validated analysis model, the software can be used to run multiple scenarios to gain information on vehicle response prior to testing using expensive vehicle hardware. The software used for the simulation is SimWise 4D by Design Simulation Technologies, Inc. Modeling of the rigid body vehicle was done using Pro ENGINEER and Siemens NX8 CAD software. Simulation in SimWise 4D showed that the induced vehicle rotation rates due to propellant slosh in the spherical tanks are dependent on the propellant fuel height, slosh frequency, slosh amplitude, and propellant mass. Induced angular rates and accelerations decreased with a decrease of propellant loading beginning at the 2000 lb load case. Higher load cases (at 4000 lb for example) exhibited decreased induced velocity due to decreased sloshing as the liquid free surface decreased within the spherical tank.

Download or read book Liquid Sloshing Dynamics written by Raouf A. Ibrahim and published by . This book was released on 2005-09 with total page 972 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book deals with almost every aspect of liquid sloshing dynamics.

Download or read book Slosh Suppression NASA Space Vehicle Design Criteria structures written by and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Theory of the Fluid Oscillations in a Circular Cylindrical Ring Tank Partially Filled with Liquid written by Helmut F. Bauer and published by . This book was released on 1960 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid Propellant Processing Factors in Rocket Motor Design written by Carlton L. Horine and published by . This book was released on 1971 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Study on In orbit Assessment of Propellant Slosh Dynamics written by C. Philippe and published by . This book was released on 1990 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Liquid Sloshing Dynamics written by Raouf A. Ibrahim and published by Cambridge University Press. This book was released on 2005-05-19 with total page 986 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of liquid sloshing in moving or stationary containers remains of great concern to aerospace, civil, and nuclear engineers; physicists; designers of road tankers and ship tankers; and mathematicians. Beginning with the fundamentals of liquid sloshing theory, this book takes the reader systematically from basic theory to advanced analytical and experimental results in a self-contained and coherent format. The book is divided into four sections. Part I deals with the theory of linear liquid sloshing dynamics; Part II addresses the nonlinear theory of liquid sloshing dynamics, Faraday waves, and sloshing impacts; Part III presents the problem of linear and nonlinear interaction of liquid sloshing dynamics with elastic containers and supported structures; and Part IV considers the fluid dynamics in spinning containers and microgravity sloshing. This book will be invaluable to researchers and graduate students in mechanical and aeronautical engineering, designers of liquid containers, and applied mathematicians.

Download or read book Dynamic Stability of Space Vehicles Testing for booster propellant sloshign parameters by D M Eggleston written by General Dynamics Corporation and published by . This book was released on 1968 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Solid Propellant Grain Structural Integrity Analysis written by James S. Noel and published by . This book was released on 1973 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Principles of Design of Dynamically Similar Models for Large Propellant Tanks written by Paul Edwin Sandorff and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: