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.
Rocket engine nozzle photographic system
01.04.1968
Sonstige
Keine Angabe
Englisch
British Library Conference Proceedings | 2004
|AIAA | 2004
|NTIS | 1977
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