NASA SBIR 2021-I Solicitation

Proposal Summary


   
Proposal Number:          21-1- Z1.07-1116
          
          
   
Subtopic Title:
      Dynamic Energy Conversion for Space Nuclear Power and Propulsion
          
          
   
Proposal Title:
      Radiator Free Engine
          
          

Small Business Concern

   
Firm:
          
Pioneer Astronautics
          
   
Address:
          
11111 West 8th Avenue, Unit A, Lakewood, CO 80215
          
   
Phone:
          
(303) 984-9346                                                                                                                                                                                
          

Principal Investigator:

   
Name:
          
Robert Zubrin
          
   
E-mail:
          
zubrin@aol.com
          
   
Address:
          
11111 West 8th Avenue, Unit A, CO 80215 - 5516
          
   
Phone:
          
(303) 984-9346                                                                                                                                                                                
          

Business Official:

   
Name:
          
Robert Zubrin
          
   
E-mail:
          
zubrin@aol.com
          
   
Address:
          
11111 West 8th Avenue, Unit A, CO 80215 - 5516
          
   
Phone:
          
(303) 984-9346                                                                                                                                                                                
          

Summary Details:

   
Estimated Technology Readiness Level (TRL) :                                                                                                                                                          
Begin: 2
End: 4
          
          
     
Technical Abstract (Limit 2000 characters, approximately 200 words):

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.  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.

          
          
     
Potential NASA Applications (Limit 1500 characters, approximately 150 words):

The Radiator Free Engine (RFE) enables very high power to mass ratio NEP and solar thermal electric propulsion. RFE systems could be used to transport payloads from LEO to the Deep Space Gateway. RFE systems could use water as propellant, enabling the Artemis Moonbase to support both cis-lunar and interplanetary transportation. RFEs could enable fast trips between Earth and Mars. RFE reactor systems could also be used to supply power on surface of the Moon, Mars, and Titan. RFE lunar surface vehicles could go into shadowed craters to mine ice.

          
          
     
Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words):

Solar thermal RFE space transfer vehicles could support LEO to GEO transfer of commercial satellites, and cis-lunar transportation. RFE propulsion would be extremely attractive for asteroid development, since water ice is present on many asteroids.  RFE technology could also be used to support high efficiency power generation on Earth.

          
          
     
Duration:     6
          
          

Form Generated on 04/06/2021 12:07:05