Publication Date:
2019-07-13
Description:
Liquid rocket engine injector elements design criteria, using noncircular orifice geometry to predict efficiency
Keywords:
PROPULSION SYSTEMS
Type:
AIAA PAPER 70-704
,
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH; Jun 15, 1970 - Jun 19, 1970; SAN DIEGO, CA
Format:
text
Permalink