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SP-100 reactor for lunar surface power system applications. Two designs were characterized and modeled. The first design integrates a 100-kWe SP-100 Brayton power system with a lunar lan-der. This system is intended to meet early lunar mission power needs while minimizing on-site installation requirements.
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.
A significant portion of the SP-100 Project is aimed at identifying plausible missions, determining their requirements, and identifying space nuclear reactor systems that would be capable of meeting these requirements. These system identification activities are being closely followed by the development of enabling technology. To insure that the
1 Ιαν 1991 · The SP-100 Program is developing a nuclear reactor power system that can enhance and/or enable future civilian and military space missions. The program is directed to develop space reactor technology to provide electrical power in the range of tens to hundreds of kilowatts.
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.
The goal of the triagency SP-100 Program is to develop long-lived, compact, lightweight, survivable nuclear reactor space power systems for application to the power range 50 kWe to 1 MWe.
A 100 kW/sub e/ Generic Flight System (GFS) design was established in response to comprehensive specifications which provided bounding requirements that envelope a range of missions from earth orbiting satellites to planetary probes.
