TY  - RPRT
TI  - 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
AU  - Africano, A.
PY  - 1965
UR  - https://ntrs.nasa.gov/citations/19660020050
ID  - 19660020050
ER  -