TY  - RPRT
TI  - A Preliminary Model for Spacecraft Propulsion Performance Analysis Based on Nuclear Gain and Subsystem Mass-Power Balances
AU  - Chakrabarti, S.
AU  - Schmidt, G. R.
AU  - Thio, Y. C.
AU  - Hurst, C. M.
PY  - 1999
UR  - https://ntrs.nasa.gov/citations/19990080929
ID  - 19990080929
ER  -