Thermal barrier coating for use on water cooled nozzle of solid propellant rocket engine
Development of a thermal barrier coating for use on a water-cooled nozzle of a solid propellant rocket motor Final report
03.05.1969
Report
Keine Angabe
Englisch
Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|