It was found that reduction in thermal radiation from an oxygen-hydrocarbon rocket exhaust flame of 50% or greater might be achieved with the addition of approximately 10% water, by weight, to propellants, with an attendant performance loss on the order of only 2%. (Author)
The Effect of Water Injection on the Thermal Radiation from Oxygen-Hydrocarbon Rocket Exhaust Flames
1959
5 pages
Report
Keine Angabe
Englisch
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