The Wind Environment Interactions Relative to Launch Vehicle Design
Author:
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
Publisher
FapUNIFESP (SciELO)
Subject
Aerospace Engineering
Link
http://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e0220.pdf
Reference14 articles.
1. Adelfang SI (1999) User’s guide for monthly vector wind profile model. (CR-1999-209759). NASA Technical Report. [ Links ]
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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