Add to ORKGPhotoelastic investigation on scaled models of Algol rocket engine nozzles to determine pressure and thermal stresse
Numerical analysis of techniques for separating space shuttles by separation rockets, spring loaded ...
A program is described for obtaining a reliable, parametric set of measurements in the exhaust plume...
Stress analysis and friction coefficient determination for expandable tube type shock absorbe
Samples of aluminum slag were investigated to aid the Earth Science and Applications Division at the...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Reaction kinetics ablation program to predict ablation performance of rocket nozzle heat protection ...
Cost estimates and feasibility of compression molded plastic motor cases and nozzles for solid rocke...
Structural reliability tests on pyrolytic graphite and pyrolytic graphite alloys for use in liquid p...
Evaluating low cost ablative materials for use in large solid propellant rocket motor
On April 5, 1983, an Inertial Upper Stage (IUS) spacecraft experienced loss of control during the bu...
The recent fusion of decades of advancements in mathematical models, numerical algorithms and curve ...
Comparison of experimental heat transfer coefficients in a nozzle with analytical predictions for va...
Solid propellant combustion model modification to contain two heat release zones in gas phas
Computerized prediction analyses of radial spin acceleration effects on solid propellant rocket moto...
Static tests of 65 inch diameter subscale rocket engines to evaluate nozzle fabrication methods, noz...
Numerical analysis of techniques for separating space shuttles by separation rockets, spring loaded ...
A program is described for obtaining a reliable, parametric set of measurements in the exhaust plume...
Stress analysis and friction coefficient determination for expandable tube type shock absorbe
Samples of aluminum slag were investigated to aid the Earth Science and Applications Division at the...
A miniature solid propellant rocket motor has been developed to be used in a program to determine th...
Reaction kinetics ablation program to predict ablation performance of rocket nozzle heat protection ...
Cost estimates and feasibility of compression molded plastic motor cases and nozzles for solid rocke...
Structural reliability tests on pyrolytic graphite and pyrolytic graphite alloys for use in liquid p...
Evaluating low cost ablative materials for use in large solid propellant rocket motor
On April 5, 1983, an Inertial Upper Stage (IUS) spacecraft experienced loss of control during the bu...
The recent fusion of decades of advancements in mathematical models, numerical algorithms and curve ...
Comparison of experimental heat transfer coefficients in a nozzle with analytical predictions for va...
Solid propellant combustion model modification to contain two heat release zones in gas phas
Computerized prediction analyses of radial spin acceleration effects on solid propellant rocket moto...
Static tests of 65 inch diameter subscale rocket engines to evaluate nozzle fabrication methods, noz...
Numerical analysis of techniques for separating space shuttles by separation rockets, spring loaded ...
A program is described for obtaining a reliable, parametric set of measurements in the exhaust plume...
Stress analysis and friction coefficient determination for expandable tube type shock absorbe