NASA NTRS · 19660020050
Engineering Method to Predict Saturn V Vehicle and Launch Complex Environments Due to Rocket Jet Impingement Quarterly Progress Report No. 2, 1 Oct. - 31 Dec. 1964
Abstract
Prediction of Saturn V vehicle and launch complex force and heat load environments due to rocket jet impingement - impact pressure and radiation and convective heat transfer
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Africano, A.. 1965-01-15. Engineering Method to Predict Saturn V Vehicle and Launch Complex Environments Due to Rocket Jet Impingement Quarterly Progress Report No. 2, 1 Oct. - 31 Dec. 1964. https://ntrs.nasa.gov/citations/19660020050
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