[10] Boeing Aerospace Corporation, High Power Spacecraft Thermal Management, AFWAL Contract AF33615-85-C-2540. [11] Thermacore Proposal P12-1555, Space Designed 10 kW,h Heat Pump Heat Rejection System Critical Component Demonstration. [12] Thermacore Proposal P12-1552, Development of Low-mass Self-deploying Radiators for Spacecraft. [13] Thermacore Proposal P12-1543, Low Mass Intrinsically Hard High Temperature Radiators. [14] Final Report, NAS3-24634.
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