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24 Φεβ 2009 · SP-100_Reactor_Drawing.png (524 × 303 pixels, file size: 64 KB, MIME type: image/png)
An update on the SP-100 reactor subsystem design and performance is provided. Several key requirements have influenced the design substantially as the more deta.
SP-100 (Space reactor Prototype [1]) was a U.S. research program for nuclear fission reactors usable as small fission power systems for spacecraft. [2] It was started in 1983 by NASA , the US Department of Energy and other agencies.
1 Απρ 2003 · The SP100 space nuclear reactor was designed for use as an orbital power supply, lunar or Martian surface power station, and power supply for nuclear electric propulsion, with a scaleable power range of 10's kWe to 100's kWe.
The SP-100 program develops, validates, and demonstrates the technology for space nuclear power systems in the range of 10 to 1000 kilowatts electric for use in future military and civilian space missions.
SP-100, THE U.S. SPACE NUCLEAR REACTOR POWER PROGRAM* By: Vincent C. Truscello ' Abstract—DARPA. in conjunction with DOE's Office of Nuclear Energy, and NASA's Office of Aeronautics and Space Technology are jointly sponsoring a space nuclear reactor power system program known as the Space Power-100 (SP-100) Development Project.
Reactor. s the mass of SP-100's nuclear heat source is3049 kg, specific mass of that 100-kWe powerplant mnst exceed 30 kg/kWe even if the ther. oelectric power generator had no mass at all. In exploiting this reactor and its large investment of time and money, the key to reduced specific mass is, of course, to.
