An Improved Procedure for Combining Day-of-Launch Atmospheric Flight Loads

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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Binkley, J F, Clark, J B, Spiekermann, C E
Format: Report
Sprache:eng
Schlagworte:
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
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Beschreibung
Zusammenfassung: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.