RL-10 and J-2 hydrogen oxygen engine design and development for Saturn Apollo launch vehicles, noting performance parameters from ground and flight tests
Development of LOX-hydrogen engines for the Saturn Apollo launch vehicles.
PROPULSION JOINT SPECIALIST CONFERENCE ; 1968 ; CLEVELAND, OH
1968-06-01
Conference paper
No indication
English
Apollo/Saturn V launch operations.
NTRS | 1966
|Apollo/Saturn V launch operations
AIAA | 1966
|