TY  - RPRT
TI  - Thrust transient prediction and control of solid rocket engines.
AU  - Macdonald, B. W.
AU  - Most, W. J.
AU  - Stang, P. L.
AU  - Summerfield, M.
PY  - 1968
UR  - https://ntrs.nasa.gov/citations/19690040376
ID  - 19690040376
ER  -