TY  - RPRT
TI  - Spacecraft boost and abort guidance and control systems requirement study, boost dynamics and control analysis study. Exhibit A: Boost dynamics and control anlaysis
AU  - Williams, F. E.
AU  - Price, J. B.
AU  - Lemon, R. S.
PY  - 1972
UR  - https://ntrs.nasa.gov/citations/19730002163
ID  - 19730002163
ER  -