2.5.4.6 Primary Structure This structure is identical to that for the Brayton SPS. Aluminum was assumed for this component. Potassium Rankine High Temperature Cycle: Total Mass-4.5xlOE6 Kg Non-Lunar Mass=O Potassium Rankine Low Temperature Cycle: Total Mass»5.13xlOE6 Kg Non-Lunar Mass-0 Steam Rankine High Temperature Cycle: Total Mass-3.33xlOE6 Kg Non-Lunar Mass-0 Steam Rankine Low Temperature Cycle: Total Mass-4.14xlOE6 Kg Non-Lunar Mass-0 2.5.4 Rankine Cycle References 1. "Space Based Power Conversion and Relay Systems: Preliminary Analysis of Alternative Systems", 26 May, 1976, NASA MSFC Contract NAS8-31682, Boeing Aerospace Co., NASA-CR-15O171.
RkJQdWJsaXNoZXIy MTU5NjU0Mg==