AAWSAP DIRD, MHD Air Breathing Propulsion and Power for Aerospace Applications, November 2010
DOW-UAP-D149 · page 28 of 32
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UNCLASSIFIED//EAR QFFl&IAk l!ISl!!! er•t I Another operational option enabled with electric systems is to fly at much lower obits where drag forces would normally cause the spacecraft to reenter in a short period of time. An air-breathing electric thruster can be used for drag make-up without the need for additional propellant. 51 Nuclear fission power systems coupled with electric thrusters enable new capabilities. Nuclear space reactors have been flown in space (SNAP-10A by the United States and TOPAZ reactors by the former Soviet Union).52 The SP-100 system shown in Figure 1253 was being developed in the 1990s as a tug to move spacecraft from LEO to GEO orbits. Even higher powered systems have been proposed to planetary CUTAWAY VIEW OFTHESP-IOOSPACE NUCLEAR POWER SYSTEM Figure 12. SP-100 Space Nuclear Power System. Illustration of the 100 kWe SP-100 nuclear reactor. missions such as those shown in Figure 13. 54• 55 Having a nuclear vehicle in orbit also enables the beaming of power to air or ground vehicles from orbit or the use of laser and microwave weapons. Figure 13. Nuclear Electric Propulsion (NEP) Concept Vehicles. Left is the 100-kWe Jupiter Icy Moons (JIMO) planetary spacecraft. Right is a 100-MWe-class piloted Mars vehicle. UNCLASSIFIED/FOR OEFICllk W61i 8HLY 24