Refined Day-of-Launch Atmospheric Flight Loads Analysis Approach

A day-of-launch atmospheric flight loads analysis approach that reduces conservatism by better defining the components of flight loads that have to be treated statistically and those that can be established with measured wind profiles just prior to launch is described. The approach introduces the co...

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Veröffentlicht in:Journal of spacecraft and rockets 2000-07, Vol.37 (4), p.453-458
Hauptverfasser: Kabe, A. M, Spiekermann, C. E, Kim, M. C, Lee, S. S
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container_end_page 458
container_issue 4
container_start_page 453
container_title Journal of spacecraft and rockets
container_volume 37
creator Kabe, A. M
Spiekermann, C. E
Kim, M. C
Lee, S. S
description A day-of-launch atmospheric flight loads analysis approach that reduces conservatism by better defining the components of flight loads that have to be treated statistically and those that can be established with measured wind profiles just prior to launch is described. The approach introduces the concept of removing from measured day-of-launch winds the rapidly varying features and only using the more slowly changing components in the load calculations performed just prior to launch. The proposed approach takes advantage of two recent developments. The first development defines the spectral boundary, as a function of time, between wind components that can be considered slowly varying and those that change rapidly and, hence, have to be addressed statistically. The second development provides an approach for calculating gust loads caused only by the turbulent components of the winds and thus eliminates the need to include these wind components in the load calculations performed just prior to launch. (Author)
doi_str_mv 10.2514/2.3604
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The second development provides an approach for calculating gust loads caused only by the turbulent components of the winds and thus eliminates the need to include these wind components in the load calculations performed just prior to launch. 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subjects Atmospheric flight
ATMOSPHERIC TURBULENCE
Boundaries
Calculations
Flight dynamics
Gusts
LAUNCH VEHICLES
LOAD DISTRIBUTION (FORCES)
Mathematical analysis
PAYLOADS
Rockets
Spacecraft
Spectra
STATISTICAL ANALYSIS
Statistical methods
Wind effects
WIND PROFILES
title Refined Day-of-Launch Atmospheric Flight Loads Analysis Approach
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