Reviewing of photographic technique for determining temperatures in luminous rocket exhaust gases; recent refinements in reduction and analysis of film records; values of temperatures measured at nozzle exit of small rocket motor are compared with theoretical values based on measurement of pressure in chamber, propellant mixture ratio, and dimensions of motor; applicability to studies of expansion process in rocket nozzles. (See also Optical Soc America -- J v 48 n 10 Oct 1958 p 717-21)
Photographic technique for measuring temperatures in luminous rocket exhaust flames
Aircraft Eng
Aircraft Engineering ; 31 , n 363
1959
3 pages
Aufsatz (Zeitschrift)
Englisch
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