29th Joint Propulsion Conference and Exhibit 1993
DOI: 10.2514/6.1993-2222
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An approach to system optimization for solar electric orbital transfer vehicles

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“…For the LEO-to-GEO transfer, likely propellants include hydrogen and ammonia. 4,5,6 Helium has also been considered as a propellant for this application because of the potential for much higher efficiency with arcjets operating on helium.…”
Section: Introductionmentioning
confidence: 99%
“…For the LEO-to-GEO transfer, likely propellants include hydrogen and ammonia. 4,5,6 Helium has also been considered as a propellant for this application because of the potential for much higher efficiency with arcjets operating on helium.…”
Section: Introductionmentioning
confidence: 99%