Add to ORKGSterile solid propellant motor for planetary and lunar landings - chemical sterilization, heat steri...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Development of thermal insulation system for wing and control surfaces of hypersonic aircraft and re...
Solid propellant ignition with hypergolic fluid injected to predetermined portions of propellan
The characteristics of a solid propellant rocket engine with a controlled rate of thrust buildup to ...
A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy tu...
A rocket injector is provided with multiple sets of manifolds for supplying propellants to injector ...
A lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain...
Performance evaluation of solid propellant rocket motor ignition to determine igniter design and par...
Demonstration of solid propellant rocket engine for unmanned planetary landers to withstand dry heat...
Flame propagation and ignition in axial head-end, canted head-end, and aft-end solid propellant igni...
A solid propellant rocket motor containing 60.9 Kg (134-lb) of propellant was successfully static fi...
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...
Determining postignition interactions between igniter and main motor flow by aft-end heated air simu...
Sterile solid propellant motor for planetary and lunar landings - chemical sterilization, heat steri...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Development of thermal insulation system for wing and control surfaces of hypersonic aircraft and re...
Solid propellant ignition with hypergolic fluid injected to predetermined portions of propellan
The characteristics of a solid propellant rocket engine with a controlled rate of thrust buildup to ...
A supersonic combustion rocket is provided in which a small rocket motor is substituted for heavy tu...
A rocket injector is provided with multiple sets of manifolds for supplying propellants to injector ...
A lightweight pyrogen igniter assembly including an elongated molded plastic tube adapted to contain...
Performance evaluation of solid propellant rocket motor ignition to determine igniter design and par...
Demonstration of solid propellant rocket engine for unmanned planetary landers to withstand dry heat...
Flame propagation and ignition in axial head-end, canted head-end, and aft-end solid propellant igni...
A solid propellant rocket motor containing 60.9 Kg (134-lb) of propellant was successfully static fi...
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...
Determining postignition interactions between igniter and main motor flow by aft-end heated air simu...
Sterile solid propellant motor for planetary and lunar landings - chemical sterilization, heat steri...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Development of thermal insulation system for wing and control surfaces of hypersonic aircraft and re...