Modeling RL10 Thrust Increase with Densified LH~2 and LOX Propellants
39th, Joint propulsion conference; 39th AIAA/ASME/SAE/ASEE joint propulsion conference ; 2003 ; Huntsville, AL
2003-01-01
4485 pages
Nos 2003-4404 to 2003-9731 with gaps
Conference paper
English
AIAA , ASME , SAE , ASEE , propulsion
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Modified RL10 rocket engine demonstrates combustion stability over an expanded thrust range
Online Contents | 2009