TY  - RPRT
TI  - Flight Performance Feasibility Studies for the Max Launch Abort System
AU  - Tarabini, Paul V.
AU  - Gilbert, Michael G.
AU  - Beaty, James R.
PY  - 2013
UR  - https://ntrs.nasa.gov/citations/20140002406
ID  - 20140002406
ER  -