NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Effect of Ozone Addition on Combustion Efficiency of Hydrogen: Liquid-Oxygen Propellant in Small RocketsAn experimental study shows that 2 percent by weight ozone in oxygen has little effect on overall reactivity for a range of oxidant-fuel weight ratios from 1 to 6. This conclusion is based on characteristic-velocity measurements in 200-pound-thrust chambers at a pressure of 300 pounds per square inch absolute with low-efficiency injectors. The presence of 9 percent ozone in oxygen also did not affect performance in an efficient chamber. Explosions were encountered when equipment or procedure permitted ozone to concentrate locally. These experiments indicate that even small amounts of ozone in oxygen can cause operational problems.
Document ID
19980228133
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Miller, Riley O.
(NASA Lewis Research Center Cleveland, OH United States)
Brown, Dwight D.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1959
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-327
NASA-MEMO-5-26-59E
Report Number: E-327
Report Number: NASA-MEMO-5-26-59E
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available