TY  - RPRT
TI  - Finite burn maneuver modeling for a generalized spacecraft trajectory design and optimization system.
AU  - Cesar Ocampo
PY  - 2004
DO  - 10.1196/annals.1311.013
UR  - https://pubmed.ncbi.nlm.nih.gov/15220149/
ID  - 15220149
ER  -