An Improved Procedure for Combining Day-of-Launch Atmospheric Flight Loads
An improved procedure for combining launch vehicle atmospheric flight load contributors is presented. This new procedure produces load-to-allowable value ratios with lower bias and less variance than previously used procedures. It is expected that the new procedure will increase launch availability...
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| creator | Binkley, J F Clark, J B Spiekermann, C E |
| description | An improved procedure for combining launch vehicle atmospheric flight load contributors is presented. This new procedure produces load-to-allowable value ratios with lower bias and less variance than previously used procedures. It is expected that the new procedure will increase launch availability without reducing launch reliability. |
| format | Report |
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| subjects | ACCELERATION Aerodynamics AEROELASTICITY ANGLE OF ATTACK ATMOSPHERICS CAPABILITY RATIO CENTRAL LIMIT THEORY DYNAMIC PRESSURE FLIGHT LOADS GIMBALS LAUNCH VEHICLES LOADS COMBINATION EQUATION MONTE CARLO METHOD RELIABILITY RIGID BODY STATIC LOADS STATISTICS STRUCTURAL PROPERTIES Unmanned Spacecraft WINGS |
| title | An Improved Procedure for Combining Day-of-Launch Atmospheric Flight Loads |
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