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  1. 24 Φεβ 2009 · SP-100_Reactor_Drawing.png ‎ (524 × 303 pixels, file size: 64 KB, MIME type: image/png)

  2. 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.

  3. en.wikipedia.org › wiki › SP-100SP-100 - Wikipedia

    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.

  4. The NASA, DOD, and DOE triagency SP-100 Pro- gram has recently embarked on a major effort to demonstrate the technology readiness of nuclear reactor space power systems for space applications by 1992. This program is termed the SP-100 ground engineerin system (GES) in which system safety and typica? reactor and aerospace (conversion,

  5. 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.

  6. The ORNL reactor study assumed a thermal power of 10 MWt, coolant outlet temperature of 1200 K, and operational life of two years at full power. The results showed the SP-100 HEU option to be the lightest mass reactor at approximately 2400 kg including fuel, vessel, reflector, instrumentation & control, and Li primary loop.

  7. 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.

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