TY  - RPRT
TI  - 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
AU  - Africano, A.
PY  - 1965
UR  - https://ntrs.nasa.gov/citations/19660015200
ID  - 19660015200
ER  -