TY  - RPRT
TI  - Optimization problems caused by interaction of guidance and propellant systems.
AU  - Chandler, D. C.
AU  - Horn, H. J.
AU  - Ryan, R. S.
PY  - 1967
UR  - https://ntrs.nasa.gov/citations/19670048803
ID  - 19670048803
ER  -