Design optimum zinc infiltrated self cooled nozzle inserts for hybrid propellant rocket motors
Design and application of self-cooled rocket nozzles Final report, 5 Jan. 1968 - 31 Oct. 1969
1969-10-01
Report
No indication
English
Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|Cooled Solid Propellant Rocket Nozzles
NTIS | 1964
|Kinetic performance of barrier-cooled rocket nozzles.
AIAA | 1968
|