Simulation of the working process of launch vehicle pressurization system in random vibration condition
JOURNAL- BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS ; 39 , 10 ; 1314-1318
01.01.2013
5 pages
Aufsatz (Zeitschrift)
Unbekannt
DDC: | 629.4 |
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Multiple On-Off Solenoid Valve Control for a Launch Vehicle Propellant Tank Pressurization System
British Library Conference Proceedings | 1999
|PROPELLANT TANK AMMONIAC PRESSURIZATION SYSTEM OF LAUNCH VEHICLES PROPULSION SYSTEMS
DOAJ | 2018
|