Add to ORKGA rocket engine igniter has been created that uses a pneumatically driven hammer that, by specialize...
A laser ignition/ablation propulsion system that captures the advantages of both liquid and solid pr...
This thesis document was issued under the authority of another institution, not NPS. At the time it...
Method for igniting solid propellant rocket motors by injecting hypergolic fluid
The characteristics of a solid propellant rocket engine with a controlled rate of thrust buildup to ...
Propellants flow through specialized mechanical hardware that is designed for effective and safe ign...
An ignitor for use with the MC-1 rocket engine has a cartridge bounded by two end caps with rupture ...
A lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain...
Flame propagation and ignition in axial head-end, canted head-end, and aft-end solid propellant igni...
A solid rocket motor includes a combustion chamber bounded by an outer casing, a propellant grain wi...
A rocket injector is provided with multiple sets of manifolds for supplying propellants to injector ...
Steerable solid propellant rocket motor adapted to effect payload orientation as multistage rocket s...
A high number of liquid oxygen and gaseous hydrogen orifices per unit area are provided in an inject...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Performance evaluation of solid propellant rocket motor ignition to determine igniter design and par...
A rocket engine igniter has been created that uses a pneumatically driven hammer that, by specialize...
A laser ignition/ablation propulsion system that captures the advantages of both liquid and solid pr...
This thesis document was issued under the authority of another institution, not NPS. At the time it...
Method for igniting solid propellant rocket motors by injecting hypergolic fluid
The characteristics of a solid propellant rocket engine with a controlled rate of thrust buildup to ...
Propellants flow through specialized mechanical hardware that is designed for effective and safe ign...
An ignitor for use with the MC-1 rocket engine has a cartridge bounded by two end caps with rupture ...
A lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain...
Flame propagation and ignition in axial head-end, canted head-end, and aft-end solid propellant igni...
A solid rocket motor includes a combustion chamber bounded by an outer casing, a propellant grain wi...
A rocket injector is provided with multiple sets of manifolds for supplying propellants to injector ...
Steerable solid propellant rocket motor adapted to effect payload orientation as multistage rocket s...
A high number of liquid oxygen and gaseous hydrogen orifices per unit area are provided in an inject...
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction produc...
Performance evaluation of solid propellant rocket motor ignition to determine igniter design and par...
A rocket engine igniter has been created that uses a pneumatically driven hammer that, by specialize...
A laser ignition/ablation propulsion system that captures the advantages of both liquid and solid pr...
This thesis document was issued under the authority of another institution, not NPS. At the time it...