TY  - RPRT
TI  - Injection Principles from Combustion Studies in a 200-Pound-Thrust Rocket Engine Using Liquid Oxygen and Heptane
AU  - Heidmann, M. F.
AU  - Auble, C. M.
PY  - 1955
UR  - https://ntrs.nasa.gov/citations/20050019330
ID  - 20050019330
ER  -