A statistical technique for combining launch vehicle loads during atmospheric flight

Details A statistical technique for combining launch vehicle loads during atmospheric flight A statistical technique for combining launch vehicle loads during atmospheric flight

Jan 1993

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1993aiaa.meetqz...m&link_type=abstract

AIAA, Aerospace Sciences Meeting and Exhibit, 31st, Reno, NV, Jan. 11-14, 1993, 8 p.

Computer Science

Aerodynamic Loads, Gust Loads, Statistical Analysis, Titan 4 Launch Vehicle, Aeroelasticity, Meteorology, Monte Carlo Method, Static Loads

Scientific paper

The load a launch vehicle will experience during atmospheric flight is made up of various components, which may or may not occur simultaneously. A significant portion of the load is dependent on atmospheric conditions on the day of launch. Due to time constraints on the day of launch, the load contributors are often combined in what is referred to as a loads combination equation. To verify the adequacy of a loads combination equation, a Monte Carlo statistical technique for combining atmospheric flight loads has been developed and implemented. The technique was used to verify the loads combination equation currently in use for the Air Force Titan IV launch vehicle.

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