TY  - RPRT
TI  - Gradient Field Imploding Liner Fusion Propulsion System: NASA Innovative Advanced Concepts Phase I Final Report
AU  - Lapointe, M. R.
AU  - Adams, R. B.
AU  - Cassibry, J.
AU  - Zweiner, M.
AU  - Gilland, J. H.
PY  - 2018
UR  - https://ntrs.nasa.gov/citations/20180006825
ID  - 20180006825
ER  -