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
1969-05-03
Report
No indication
English
Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|