The Wind Environment Interactions Relative to Launch Vehicle Design

Author:

L. Johnson Dale1,W. Vaughan William2ORCID

Affiliation:

1. National Aeronautics and Space Administration - Marshall Space Flight Center (retired) - Huntsville/AL - USA

2. National Aeronautics and Space Administration - Marshall Space Flight Center (emeritus) - Huntsville/AL - USA

Abstract

Since atmospheric winds play the most critical natural enviroment (NE) role as input into the design and development of an aerospace launch vehicle, this paper provides a more detailed description of the wind environment and its interaction with engineering design in launch and space vehicle development applications at Kennedy Space Center (KSC).

Publisher

FapUNIFESP (SciELO)

Subject

Aerospace Engineering

Reference14 articles.

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2. Adelfang SI, Smith OE, Batts GW (1994) Ascent wind model for launch vehicle design. J Spacecraft and Rockets 31(3):502-508. https://doi.org/10.2514/3.26467 [ Links ]

3. Bowman BR, Tobiska WK, Marcos FA, Valladares C (2008) The JB2006 empirical thermosphere density model. Journal of Atmospheric and Solar-Terrestrial Physics 70(5):774-793. https://doi.org/10.1016/j.jastp.2007.10.002 [ Links ]

4. Department of Defense (1969) Military Specification Flying Qualities of Piloted Airplanes. (MILF-8785B). US Airforce Technical Report. [ Links ]

5. Geissler ED (1970) Wind effects on launch vehicles. Slough: Technivision Services. [ Links ]

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