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1 March 1983 High Speed Photographic Studies Of Rocket Engine Combustion
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Proceedings Volume 0348, 15th Intl Congress on High Speed Photography and Photonics; (1983) https://doi.org/10.1117/12.967723
Event: 15th International Congress on High Speed Photography and Photonics, 1982, San Diego, United States
Abstract
The high speed cameras were used to develop the new sounding rocket motor and to check the safety operation system. The new rocket motor was designed as a single stage rocket and its power was greater than the multi-stage K-9M rocket motor. The test combustion of this new type rocket engine was photographed by the high speed cameras to analyze the burning process. At the outside of rocket chamber, the cable which connect the detector of an engine nozzle with the telemeter system was fixed. To check the thero.,a1 influences of combustion flame to the cable, the thermo-tapes and high speed cameras were used Safety operation system was tested and photographed with high speed cameras using a S0-1510 model rocket.
© (1983) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Tsuneyoshi Uyemura, Shigeo Ozono, Toshio Mizunuma, Yoshitaka Yamamoto, Yutaka Kikusato, Masamitsu Eiraku, and Yubu Uchida "High Speed Photographic Studies Of Rocket Engine Combustion", Proc. SPIE 0348, 15th Intl Congress on High Speed Photography and Photonics, (1 March 1983); https://doi.org/10.1117/12.967723
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