TY  - RPRT
TI  - Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
AU  - Bryson, A. E., Jr.
AU  - Winfield, D. H.
PY  - 1966
UR  - https://ntrs.nasa.gov/citations/19670007468
ID  - 19670007468
ER  -