Ascent performance characteristics were studied for a vertical-take-off, horizontal-landing, single-...
A research effort has been undertaken to investigate critical aspects of launch vehicle performance ...
Compactness, reliability, readiness, and construction simplicity of solid rocket motors make them ve...
5th AIAA/USAF/NASA/ISSMO; Symposium on Multidisciplinary Analysis and Optimization Panama City, Fl,...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Booster parametric design method for performance and trajectory analysis - propulsio
The purpose of this research is to investigate the effects of staging variables on Two-Stage-To-Orbi...
Small rocket engine tests were conducted for the purpose of obtaining pulse performance data to aid ...
A parametric pretest uncertainty analysis has been performed for a chemical rocket engine test at a ...
A technique is described for theoretical, statistical evaluation of the thrust imbalance of pairs of...
This paper presents the results of statistical analyses performed to predict the thrust imbalance be...
The all rocket mode of operation is a critical factor in the overall performance of a rocket based c...
International audienceSpace launcher complexity arises, on the one hand, from the coupling between s...
A preliminary uncertainty analysis has been performed for the High Area Ratio Rocket Nozzle test pro...
Propulsion systems dispersion analysis and propellant optimization method for Apollo subsystem
Ascent performance characteristics were studied for a vertical-take-off, horizontal-landing, single-...
A research effort has been undertaken to investigate critical aspects of launch vehicle performance ...
Compactness, reliability, readiness, and construction simplicity of solid rocket motors make them ve...
5th AIAA/USAF/NASA/ISSMO; Symposium on Multidisciplinary Analysis and Optimization Panama City, Fl,...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1994.In...
Booster parametric design method for performance and trajectory analysis - propulsio
The purpose of this research is to investigate the effects of staging variables on Two-Stage-To-Orbi...
Small rocket engine tests were conducted for the purpose of obtaining pulse performance data to aid ...
A parametric pretest uncertainty analysis has been performed for a chemical rocket engine test at a ...
A technique is described for theoretical, statistical evaluation of the thrust imbalance of pairs of...
This paper presents the results of statistical analyses performed to predict the thrust imbalance be...
The all rocket mode of operation is a critical factor in the overall performance of a rocket based c...
International audienceSpace launcher complexity arises, on the one hand, from the coupling between s...
A preliminary uncertainty analysis has been performed for the High Area Ratio Rocket Nozzle test pro...
Propulsion systems dispersion analysis and propellant optimization method for Apollo subsystem
Ascent performance characteristics were studied for a vertical-take-off, horizontal-landing, single-...
A research effort has been undertaken to investigate critical aspects of launch vehicle performance ...
Compactness, reliability, readiness, and construction simplicity of solid rocket motors make them ve...