Add to ORKGA lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain...
Method for igniting solid propellant rocket motors by injecting hypergolic fluid
This paper presents the design, fabrication and testing of a bi - propellant rocket engine with a th...
A high number of liquid oxygen and gaseous hydrogen orifices per unit area are provided in an inject...
Improved injector for oxygen difluoride and diborane has better mixing characteristics and is able t...
A rocket injector is provided with multiple sets of manifolds for supplying propellants to injector ...
An injector for liquid fueled rocket engines wherein a generally flat core having a frustoconical do...
A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy tu...
A low pressure loss injector element is disclosed for the main combustion chamber of a rocket engine...
Solid propellant ignition with hypergolic fluid injected to predetermined portions of propellan
Propellants flow through specialized mechanical hardware that is designed for effective and safe ign...
The characteristics of a solid propellant rocket engine with a controlled rate of thrust buildup to ...
Provided herein are various improvements to rocket engine components and rocket engine operational t...
Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxid...
This invention relates to rocket apparatus of the magazine type in which separate charges of explosi...
A lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain...
Method for igniting solid propellant rocket motors by injecting hypergolic fluid
This paper presents the design, fabrication and testing of a bi - propellant rocket engine with a th...
A high number of liquid oxygen and gaseous hydrogen orifices per unit area are provided in an inject...
Improved injector for oxygen difluoride and diborane has better mixing characteristics and is able t...
A rocket injector is provided with multiple sets of manifolds for supplying propellants to injector ...
An injector for liquid fueled rocket engines wherein a generally flat core having a frustoconical do...
A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy tu...
A low pressure loss injector element is disclosed for the main combustion chamber of a rocket engine...
Solid propellant ignition with hypergolic fluid injected to predetermined portions of propellan
Propellants flow through specialized mechanical hardware that is designed for effective and safe ign...
The characteristics of a solid propellant rocket engine with a controlled rate of thrust buildup to ...
Provided herein are various improvements to rocket engine components and rocket engine operational t...
Control over drop size distributions, injection rates, and geometrical distribution of fuel and oxid...
This invention relates to rocket apparatus of the magazine type in which separate charges of explosi...
A lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain...
Method for igniting solid propellant rocket motors by injecting hypergolic fluid
This paper presents the design, fabrication and testing of a bi - propellant rocket engine with a th...