TY  - RPRT
TI  - Hot Fire Ignition Test with Densified Liquid Hydrogen using a RL10B-2 Cryogenic H2/O2 Rocket Engine
AU  - McNelis, Nancy B.
AU  - Haberbusch, Mark S.
PY  - 1997
UR  - https://ntrs.nasa.gov/citations/19970026009
ID  - 19970026009
ER  -