TY  - RPRT
TI  - Closed-Form and Numerically-Stable Solutions to Problems Related to the Optimal Two-Impulse Transfer Between Specified Terminal States of Keplerian Orbits
AU  - Senent, Juan
PY  - 2011
UR  - https://ntrs.nasa.gov/citations/20110014083
ID  - 20110014083
ER  -