Method for calculating propellant grains with a cylindrical or cylindrical and conical section.

by Gismondi, E
[Place of publication not identified] : [publisher not identified], 1967

Method for calculating the performance and behavior of a propulsion system driven by a solid propellant with radial combustion and a cylindrical or conical section.

by Gismondi, E
[Place of publication not identified] : [publisher not identified], 1967

A new method for measuring the thrust of a rocket engine.

by Gismondi, E
[Place of publication not identified] : [publisher not identified], 1966

Method for the theoretical and experimental determination of the combustion efficiency of solid-propellant propulsion systems of any form and of liquid-propellant propulsion system...

by Gismondi, E
[Place of publication not identified] : [publisher not identified], 1967

Computational method for the cooling system of liquid-propellant rockets.

by Gismondi, E
[Place of publication not identified] : [publisher not identified], 1967

Method for measuring rocket thrust by means of an accelerometric system.

by Gismondi, E
[Place of publication not identified] : [publisher not identified], 1967

Method for determining the effect of combustion time of the apogee engine of a satellite in circular orbit on the difference between real and ideal apogee distance.

by Gismondi, E
[Place of publication not identified] : [publisher not identified], 1967