Use of capacitative manometers for sensing correct ratio of oxidizer-fuel weight in missile tanks during flight.
Rocket propellant manometer system
ISA -- J
Instrument Society of America -- Journal ; 9 , n 10
1962
2 pages
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
NTIS | 1973
|Solid-liquid rocket propellant system
Engineering Index Backfile | 1956
|Engineering Index Backfile | 1961
|Solid-Propellant Ballistic Rocket
NTIS | 1974
|NTIS | 1971
|