TY  - RPRT
TI  - Performance and Stability Analyses of Rocket Combustion Devices Using Liquid Oxygen/Liquid Methane Propellants
AU  - Hulka, James R.
AU  - Jones, G. W.
PY  - 2010
UR  - https://ntrs.nasa.gov/citations/20100032021
ID  - 20100032021
ER  -