Add to ORKGJet-stream interaction effects on rocket engine studied with simulated ballistic missile using liquid oxygen and JP-4 fuel mixtur
A small laboratory diagnostic thruster was developed to augment present low thrust chemical rocket o...
An investigation at a Reynolds number per foot of 14.4 x 10(exp 6) was made to determine the pressur...
The results of experimental researches of the structure and of the basic parameters of the air when ...
A rocket of the 1000-pound-thrust class using liquid oxygen and JP-4 fuel as propellant was installe...
A generalized study of base flow phenomena has been conducted with four 500-pound-thrust JP-4 fuel-l...
A rocket of the 1000-pound-thrust class using liquid oxygen and JP-4 fuel as propellant was installe...
Despite efforts in the search for alternative means of energy, combustion still remains the key sour...
In this work CFD investigation of weight and temperature for a rocket spout with four channels at Ma...
A gaseous H2/O2 rocket engine was constructed at the NASA-Lewis to provide a high heat flux source r...
Characteristic exhaust velocity of a 200-pound-thrust rocket engine was evaluated for fuel temperatu...
Heat-transfer measurements were made on a simulated glide-rocket shape in free flight at Mach number...
Aerodynamic hinge moments for scale model boost stage nozzle of Saturn V launch vehicle during cold ...
NASA's Space Launch System (SLS) uses four clustered liquid rocket engines along with two solid rock...
The application of laser-based diagnostic techniques has become commonplace to a wide variety of com...
The results of experimental researches of the structure and of the basic parameters of the air when ...
A small laboratory diagnostic thruster was developed to augment present low thrust chemical rocket o...
An investigation at a Reynolds number per foot of 14.4 x 10(exp 6) was made to determine the pressur...
The results of experimental researches of the structure and of the basic parameters of the air when ...
A rocket of the 1000-pound-thrust class using liquid oxygen and JP-4 fuel as propellant was installe...
A generalized study of base flow phenomena has been conducted with four 500-pound-thrust JP-4 fuel-l...
A rocket of the 1000-pound-thrust class using liquid oxygen and JP-4 fuel as propellant was installe...
Despite efforts in the search for alternative means of energy, combustion still remains the key sour...
In this work CFD investigation of weight and temperature for a rocket spout with four channels at Ma...
A gaseous H2/O2 rocket engine was constructed at the NASA-Lewis to provide a high heat flux source r...
Characteristic exhaust velocity of a 200-pound-thrust rocket engine was evaluated for fuel temperatu...
Heat-transfer measurements were made on a simulated glide-rocket shape in free flight at Mach number...
Aerodynamic hinge moments for scale model boost stage nozzle of Saturn V launch vehicle during cold ...
NASA's Space Launch System (SLS) uses four clustered liquid rocket engines along with two solid rock...
The application of laser-based diagnostic techniques has become commonplace to a wide variety of com...
The results of experimental researches of the structure and of the basic parameters of the air when ...
A small laboratory diagnostic thruster was developed to augment present low thrust chemical rocket o...
An investigation at a Reynolds number per foot of 14.4 x 10(exp 6) was made to determine the pressur...
The results of experimental researches of the structure and of the basic parameters of the air when ...