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Figure5:PhotograopfhElectrolysPisropulsion BreadboaInrdstalleIdnsideHighAltitude Chamber Rate: 18.7 seem IIIII 3.36 3.35 a 18.10 18.05 C A A A A A /'dT)TY)TY',_ t._ O 3: O = 3.34 D. m / '/)z/¢)z//_ Z_3 O. A A A Oxycjen Rate: 37.5 SCORn 3.33 I 1 I I I NASA TM-113157 14 0.6 Oxygen 0.7 0.8 Pressure 0.9 1.0 (MPa) Oxygen Generation Rate: 7.5 sccm A I I I I I 0.6 0.7 0.8 0.9 1.0 Oxygen Pressure (MPa) Electric Power Required to Propellant Generation Rate at 8.70 8.68 8.66 - c 8.64 - Q. m _A A A AA A A =,- 17.95 17.90 A -A A _b /v_ A A -A A A A A 8.62 -A 0.6 0.7 0.8 0.9 1.0 Figure 6: Maintain Increasing a) 7.5 sccm; b) 18.7 sccm; c) 37.5 sccm. Average Constant Pressures. 02 Generation Rates: A Oxygen Generation Oxygen Pressure (MPa)PDF Image | Electrolysis Spacecraft Propulsion Applications
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