Application of the Saha equation to high temperature (above 6000 K) rocket exhaust
29th Joint Propulsion Conference and Exhibit ; 1993 ; Monterey , CA , U.S.A.
01.01.1993
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Two-temperature Saha equation - A misunderstood problem
AIAA | 1995
|Rocket exhaust plume dimensions
AIAA | 1969
|