SLS Trade Study 0058: Day of Launch (DOL) Wind Biasing

SLS heritage hardware and legacy designs have shown load exceedances at several locations during Design Analysis Cycles (DAC): MPCV Z bending moments; ICPS Electro-Mechanical Actuator (EMA) loads; Core Stage loads just downstream of Booster forward interface. SLS Buffet Loads Mitigation Task Team (B...

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Bibliographische Detailangaben

Hauptverfasser:	Decker, Ryan K., Duffin, Paul, Hill, Ashley, Beck, Roger, Dukeman, Greg
Format:	Other
Sprache:	eng
Schlagworte:	Launch Vehicles And Launch Operations Spacecraft Design, Testing And Performance
Online-Zugang:	Volltext bestellen
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