Weight estimating relationships (WERs) and recurring production cost estimating relationships (CERs) were developed for helicopters at the system level. The WERs estimate system level weight based on performance or design characteristics which are available during concept formulation or the preliminary design phase. The CER (or CERs in some cases) for each system utilize weight (either actual or estimated using the appropriate WER) and production quantity as the key parameters
Telemetry calibration curves for the LANDSAT-4 subsystems are defined by nth order polynomial equati...
A method by which modern and classical theory techniques may be integrated in a synergistic fashion ...
A computer program was developed to integrate avionics research in navigation, guidance, controls, a...
The results of a NASA study to develop production cost estimating relationships (CERs) and weight es...
The fundamentals of the cost/performance management system used in the procurement of two tilt rotor...
Formulas relating overall sound pressure level (OASPL) to parameters such as horsepower required, ti...
The equilibrium characteristics of a dual-lift helicopter system are examined. The system consists o...
A structured methodology was developed that allows the generation, analysis, and rank-ordering of sy...
The feasibility was studied of predicting rotary wing operation maintenance costs by using several ...
In todays cost-constrained environment, NASA needs an X-Plane database and parametric cost model tha...
An analysis of the flight dynamics and piloted control characteristics of the Helistat, a quadrotor ...
In order to facilitate solutions of the general problem of helicopter selection, the aerodynamic per...
Critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculation...
The airplane shown below is the Beech Super King Air, an executive transport built by Beech Aircraft...
The key variables accounting for the nature, timing and magnitude of the equipment and re-equipment ...
Telemetry calibration curves for the LANDSAT-4 subsystems are defined by nth order polynomial equati...
A method by which modern and classical theory techniques may be integrated in a synergistic fashion ...
A computer program was developed to integrate avionics research in navigation, guidance, controls, a...
The results of a NASA study to develop production cost estimating relationships (CERs) and weight es...
The fundamentals of the cost/performance management system used in the procurement of two tilt rotor...
Formulas relating overall sound pressure level (OASPL) to parameters such as horsepower required, ti...
The equilibrium characteristics of a dual-lift helicopter system are examined. The system consists o...
A structured methodology was developed that allows the generation, analysis, and rank-ordering of sy...
The feasibility was studied of predicting rotary wing operation maintenance costs by using several ...
In todays cost-constrained environment, NASA needs an X-Plane database and parametric cost model tha...
An analysis of the flight dynamics and piloted control characteristics of the Helistat, a quadrotor ...
In order to facilitate solutions of the general problem of helicopter selection, the aerodynamic per...
Critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculation...
The airplane shown below is the Beech Super King Air, an executive transport built by Beech Aircraft...
The key variables accounting for the nature, timing and magnitude of the equipment and re-equipment ...
Telemetry calibration curves for the LANDSAT-4 subsystems are defined by nth order polynomial equati...
A method by which modern and classical theory techniques may be integrated in a synergistic fashion ...
A computer program was developed to integrate avionics research in navigation, guidance, controls, a...