PIONEER ASTRONAUTICS — National Aeronautics and Space Administration SBIR Phase I: Z1

Description

The Radiator Free Engine (RFE) is a new technology enabling very high power to mass ratio nuclear electric propulsion. In the RFE, cold water propellant or hydrogen used as the heat rejection dump for a dynamic cycle heated by a nuclear reactor, enabling Carnot efficiencies as high as 0.79 for water or 0.99 for hydrogen. Some of the propellant that is boiled or sublimated off is then sent to an electric propulsion system, which ejects it from the spacecraft at high velocities to produce thrust. Potential RFE conversion systems include Brayton, Rankine, and Stirling cycles. The RFE can be operated in either steady state or in pulsed modes, with the later enabling very high thrust/mass ratios. Potential alternative RFE propellants include nitrogen, methane, CO2, and ammonia stored in either liquid or frozen phases. Because its thermal to electric conversion efficiency is about a factor of 3 higher than conventional NEP systems, and it does not require radiators for heat rejection, the RFE can achieve power to mass ratios an order of magnitude higher than conventional multi megawatt power systems.nbsp; Other advantages of the RFE include its ability to use cheap, dense propellants that are plentiful or producible in space. In the proposed program, the potential performance of the RFE will be analyzed, design options compared, technical concerns addressed, and the concept validated by means of computer analysis and laboratory tests.