TY  - RPRT
TI  - A fluidic sounding rocket motor ignition system.
AU  - Marchese, V. P.
AU  - Rakowsky, E. L.
AU  - Bement, L. J.
PY  - 1972
UR  - https://ntrs.nasa.gov/citations/19730028684
ID  - 19730028684
ER  -