Add to ORKGPropellant characteristics for solid rocket motors were not completely determined for its use as a processing variable in today's production facilities. A major effort to determine propellant characteristics obtainable through ultrasonic measurement techniques was performed in this task. The information obtained was then used to determine the uniformity of manufacturing methods and/or the ability to determine non-uniformity in processes
The ability to accurately characterize propellant in a finite element model is a concern of engineer...
Mechanical characterization of solid fuel propellants - stress-strain behavior of inert composite pr...
Solid composite propellants are used widely in the aerospace industry due to their desirable mechani...
Efforts to determine whether rocket propellant density and modulus can be reliably measured using no...
Previous reports of this series have attempted to define some of the important parameters affecting ...
With age and storage, the mechanical properties of solid rocket propellants change due to oxidizer p...
Maxwell fluid model consisting of a spring and a dashpot in series is applied for viscoelastic chara...
Previous reports of this series have attempted to define some of the important parameters affecting...
The USAF MINUTEMAN ICBM Transportation and Handling Test Program involves vibration testing of full ...
The design and qualification tests of rocket motors require knowledge of the mechanical behavior of ...
This report presents the results obtained during the past year in a research program on Solid Propel...
In this report the groundwork is laid for the proposed work scope which stressed the need for a grea...
The University of Arizona program is aimed at introducing scientific rigor to the predictability and...
The ways are described by which propellant processing is affected by choices made in designing rocke...
Technique computes stresses resulting from axisymmetric transient thermal loading in circular solid-...
The ability to accurately characterize propellant in a finite element model is a concern of engineer...
Mechanical characterization of solid fuel propellants - stress-strain behavior of inert composite pr...
Solid composite propellants are used widely in the aerospace industry due to their desirable mechani...
Efforts to determine whether rocket propellant density and modulus can be reliably measured using no...
Previous reports of this series have attempted to define some of the important parameters affecting ...
With age and storage, the mechanical properties of solid rocket propellants change due to oxidizer p...
Maxwell fluid model consisting of a spring and a dashpot in series is applied for viscoelastic chara...
Previous reports of this series have attempted to define some of the important parameters affecting...
The USAF MINUTEMAN ICBM Transportation and Handling Test Program involves vibration testing of full ...
The design and qualification tests of rocket motors require knowledge of the mechanical behavior of ...
This report presents the results obtained during the past year in a research program on Solid Propel...
In this report the groundwork is laid for the proposed work scope which stressed the need for a grea...
The University of Arizona program is aimed at introducing scientific rigor to the predictability and...
The ways are described by which propellant processing is affected by choices made in designing rocke...
Technique computes stresses resulting from axisymmetric transient thermal loading in circular solid-...
The ability to accurately characterize propellant in a finite element model is a concern of engineer...
Mechanical characterization of solid fuel propellants - stress-strain behavior of inert composite pr...
Solid composite propellants are used widely in the aerospace industry due to their desirable mechani...