NASA NTRS · 19660015200
Engineering method to predict Saturn V vehicle and launch complex environments due to rocket jet impingement Quarterly progress report no. 3, 1 Jan. - 31 Mar. 1965
Abstract
Prediction of forces and heat loads of Saturn V vehicle and launch complex environments due to rocket jet plume impingement
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Africano, A.. 1965-04-15. Engineering method to predict Saturn V vehicle and launch complex environments due to rocket jet impingement Quarterly progress report no. 3, 1 Jan. - 31 Mar. 1965. https://ntrs.nasa.gov/citations/19660015200
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