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Rocket engine nozzle photographic system
- Publication Year :
- 1968
- Publisher :
- United States: NASA Center for Aerospace Information (CASI), 1968.
-
Abstract
- Protective enclosure for a camera, located on the exhaust stream of a rocket engine, permits continuous recording of erosion processes of materials used in nozzle throat structures. The system uses a standard camera in a water-cooled, pressurized enclosure having a unique, inert gas-swept viewing duct.
- Subjects :
- Physical Sciences
Subjects
Details
- Language :
- English
- Database :
- NASA Technical Reports
- Publication Type :
- Report
- Accession number :
- edsnas.19680000113
- Document Type :
- Report