Development of a Low Cost 650,000 LBF Thrust H2/O2 Booster Engine Injector
33rd, Joint propulsion conference ; 1997 ; Seattle; WA
1997-01-01
ALL
Nos 97-2914 to 97-3388 with gaps
Conference paper
English
AIAA , ASME , SAE , ASEE , propulsion
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Thrust augmentation nozzle (TAN) concept for rocket engine booster applications
British Library Conference Proceedings | 2006
|Thrust augmentation nozzle (TAN) concept for rocket engine booster applications
Online Contents | 2006
|