Add to ORKGThis report contains a restatement of the equations governing the exterior ballistics of a free flight rocket in a form suitable for solution by high speed digital computers. Neither the notation nor the definitions conform to any particular reference, hence they are clearly stated in the development of the equations of motion. The equations, along with the necessary notation are collected at the end of the report for easy reference.Department of the Army, Contract No. 57-4341, DA-11-070-508-ORD. -593, ORD. Proj. No. Tu2-7D (TW-205
This report provides a general analysis of the flight dynamics of several surface-to-air and two air...
This report contains an analysis of the single degree of freedom model originally studied in Part A ...
A numerical investigation of the behavior of stages or parts of launchers as a function of fundament...
This report contains a general formulation of the equations of motion for a rocket consisting of two...
In recent years, the science of flight mechanics as applied to long range ballistic missiles has bec...
The initial phases of this contract examined some very elementary models of launching systems. In t...
International Series of Monographs on Aeronautics and Astronautics, Division VII, Volume 5: The Flig...
This report contains an analysis of a four degree of freedom model multiple lauching system. The lau...
The ballistics equations for spherical pellets in free flight are simplified through appropriate sca...
This report is a sequel to Technical Report No. 139. The analysis of the straight rail launcher mode...
It consists of a statement of the original goals of the contract in addition to a list of the nine p...
This papers introduces an analytic method to define multistage launcher trajectories to determine th...
This thesis studies the equations of an uncontrolled unguided anti-tank missile with six-degree-of-f...
The work shows computational results of the effect of a simplified mathematical model of the flight ...
The closed-form analytic solution to the equations of motion for ballistic entry developed by Allen ...
This report provides a general analysis of the flight dynamics of several surface-to-air and two air...
This report contains an analysis of the single degree of freedom model originally studied in Part A ...
A numerical investigation of the behavior of stages or parts of launchers as a function of fundament...
This report contains a general formulation of the equations of motion for a rocket consisting of two...
In recent years, the science of flight mechanics as applied to long range ballistic missiles has bec...
The initial phases of this contract examined some very elementary models of launching systems. In t...
International Series of Monographs on Aeronautics and Astronautics, Division VII, Volume 5: The Flig...
This report contains an analysis of a four degree of freedom model multiple lauching system. The lau...
The ballistics equations for spherical pellets in free flight are simplified through appropriate sca...
This report is a sequel to Technical Report No. 139. The analysis of the straight rail launcher mode...
It consists of a statement of the original goals of the contract in addition to a list of the nine p...
This papers introduces an analytic method to define multistage launcher trajectories to determine th...
This thesis studies the equations of an uncontrolled unguided anti-tank missile with six-degree-of-f...
The work shows computational results of the effect of a simplified mathematical model of the flight ...
The closed-form analytic solution to the equations of motion for ballistic entry developed by Allen ...
This report provides a general analysis of the flight dynamics of several surface-to-air and two air...
This report contains an analysis of the single degree of freedom model originally studied in Part A ...
A numerical investigation of the behavior of stages or parts of launchers as a function of fundament...