Flow of chemically reacting propellant exhaust mixture in barrier cooled axisymmetric rocket nozzle
Kinetic performance of barrier-cooled rocket nozzles.
01.10.1968
Sonstige
Keine Angabe
Englisch
Kinetic performance of barrier-cooled rocket nozzles.
AIAA | 1968
|Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|